24 Fracture Mechanics Jobs

Job Requirements Conduct static, transient, linear, nonlinear, fatigue (LCF/HCF), thermal, and structural analyses of wind turbine components using ANSYS Workbench. Evaluate the structural integrity of components by analyzing stress, strain, displacement, and other relevant parameters under various load conditions. Interpret FEA results, identify potential areas for improvement, and propose design modifications to optimize component performance and reliability. Drive technical solutions and reviews with a design team and multiple sub-suppliers and solution providers. Investigate failures, conduct root cause analysis, and implement solutions to prevent recurring issues in wind turbine components. Identify opportunities to improve FEA processes, documentation, and design methodologies. Prepare and document detailed reports summarizing the FEA analysis, results, and recommendations. Participate in hiring, training, mentoring, and reviewing junior engineers. Embrace a proactive approach to quality by adhering to best practices and QMS processes. Work Experience Postgraduate degree holder in Mechanical engineering with over 10 years of professional experience. Proficiency in Finite Element (FE) tools such as ANSYS (Classic/workbench) is essential. Understanding of the structural design principles for large castings, welded structures, and forged components. Solid grasp of High Cycle Fatigue/Low Cycle Fatigue and fracture mechanics. Hands-on experience in performing analytical calculations for bolted/welded assemblies. Proficient in defining contacts, conducting Nonlinear analysis, and performing Buckling Analysis. Familiarity with certification requirements for components used in Wind Turbine Generators (WTG) or similar applications. Knowledge of International safety and mechanical design standards.

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NA Minimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Independently execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Perform the static FEA independently for fatigue loading to facilitate the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Follow the meshing and analysis guidelines for static and fatigue analysis and ensure the FE models created by team for F&DT justifications are compiled to the guidelines and are of high quality. Perform the FEA V&V checks and prepare the V&V documents capture the required checks for the FE models. Also ensure the specific considerations for the fatigue evaluation is correctly captured and simulated in the FE models and if required use your expertise and guidance to align with the requirements. Independently develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Prepare detailed output which will help to Identify the fatigue critical locations based on highly stressed areas from static analysis results, safety critical parts and the standard features which irrespective of stress value need to be checked. Perform the low RF/MOS mitigation, Alternative concepts analyses, compilation of inputs for the review and certification reports. Down select the number of calculation points and align with the client on this in alignment with SME/Team leads. Perform the required analyses checks to enable decision basis for selection of reliable concepts out of multiple concepts based on the static and F&DT justification validations compliance including future operational and maintenance and repair considerations. Enable F&DT team with required inputs for generation of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Review the outputs. Peer checker for F&DT analysis certification task. Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Perform the mitigation task for the low fatigue, crack growth life and F&DT performance non-compliance issues based on your expertise and experience. Align these methods with SMEs team leaders and document it as reference documents. Perform tasks as required based on the outcomes of Collaboration with cross-functional discussions with design manufacturing quality, and systems teams; actively support with relevant detailed results and observations to engage in design reviews, issue resolution, and integration discussions. Assisting customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Enable aligning customer expectations with engineering deliverables and strategic goals. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from F&DT point of view. Experience of static and F&DT analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization, fatigue and damage tolerance analysis for helicopter/aircraft certification and testing activities. Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of F&DT test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistrucut. or similar tools is a strong plus. Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. Expertise for structural sizing of aerospace structural parts meeting certification, testing and manufacturability requirements. Sound work experience related to aircraft materials, fatigue phenomenon, fracture mechanics concepts, fatigue spectrum derivation, probabilistic fatigue and crack growth assessments. Must have knowledge of structural classification, primary and secondary structure design requirements, load path and structural response. Perform the low RF/MOS mitigation, Alternative concepts analyses, compilation of inputs for the review and certification reports. Expertise in structural classification, related F&DT compliance, calculation points and their down selection, selection of scatter factors. FEA considerations and their incorporation in the meshing requirements for F&DT Analysis. In-depth understanding of helicopter/aircraft load-bearing structures, structural response with focus on structural integrity, stiffness, and load path optimization under both static and Fatigue conditions. Knowledge of failure modes relevant to metallic and composite airframe components. Proven experience for low cycles and high cycle fatigue analysis for fixed wing or rotary wing aircrafts. Exposure to functional considerations like telescopic, foldability swivel and reversal of structure. Additional Information:- The candidate should have 5 to 8 years of practical experience in the Aerostructures fatigue and damage tolerance analysis domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Minimum 12 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Lead strategic aerospace engineering engagements for rotary wing platforms, driving technical delivery, innovation, and client satisfaction. Play a key role in shaping engineering processes, delivery governance, and team capability development. Engage directly with aerospace OEMs, Tier-1 suppliers and regulatory bodies, influencing design decisions, compliance strategies, and product lifecycle outcomes. Drive digital engineering transformation, championing initiatives around MBSE, MBD, and digital continuity. Lead and oversee the execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Guide the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Establish and govern engineering F&DT analysis best practices, design review frameworks, and technical quality gates across the program lifecycle. Provide technical oversight related to F&DT across multiple concept development, structural architecture, F&DT requirement compliance for detailed design, integration, certification and certification test support. Support in generation and review of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Level II and level III checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Lead root cause investigations, risk assessments, and resolution strategies for stress/F&DT related issues, non-conformances, schedule variance and airworthiness deviations. Finalize the F&DT technical requirements, limitations and associated tasks within defined timelines, ensuring high-quality output with minimal errors. Analyse complex design challenges and propose optimal engineering solutions aligned with project goals and constraints. Provide high level competency for the fatigue spectrum derivation for analysis and the subsequent service load and the test load spectrum derivation. Document the procedure as a signed document for reference. Supervision and approval of method register, F&DT method document, Analysis tools alignment, F&DT certification analysis check lists, certification test report templates and SLA in alignment with client during the initial execution phase. Act as the technical voice of the program, aligning customer expectations with engineering deliverables and strategic goals. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Lead effective engineering change management by proactively tracking evolving inputs and shifting requirements. Evaluate and mitigate the impact of delays on schedule variance, resource planning, costs, and milestone achievement through a structured change control process aligned with client approvals and established governance protocols. Represent engineering during customer technical audits, program quality gate reviews, and change control reviews. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Act as the primary technical/program level interface with the client, ensuring alignment on F&DT compliance objectives and deliverables. Professional & Technical Skills:Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have minimum 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NA Minimum 12 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Lead strategic aerospace engineering engagements for rotary wing platforms, driving technical delivery, innovation, and client satisfaction. Play a key role in shaping engineering processes, delivery governance, and team capability development. Engage directly with aerospace OEMs, Tier-1 suppliers and regulatory bodies, influencing design decisions, compliance strategies, and product lifecycle outcomes. Drive digital engineering transformation, championing initiatives around MBSE, MBD, and digital continuity. Lead and oversee the execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Guide the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Establish and govern engineering F&DT analysis best practices, design review frameworks, and technical quality gates across the program lifecycle. Provide technical oversight related to F&DT across multiple concept development, structural architecture, F&DT requirement compliance for detailed design, integration, certification and certification test support. Support in generation and review of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Level II and level III checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Lead root cause investigations, risk assessments, and resolution strategies for stress/F&DT related issues, non-conformances, schedule variance and airworthiness deviations. Finalize the F&DT technical requirements, limitations and associated tasks within defined timelines, ensuring high-quality output with minimal errors. Analyse complex design challenges and propose optimal engineering solutions aligned with project goals and constraints. Provide high level competency for the fatigue spectrum derivation for analysis and the subsequent service load and the test load spectrum derivation. Document the procedure as a signed document for reference. Supervision and approval of method register, F&DT method document, Analysis tools alignment, F&DT certification analysis check lists, certification test report templates and SLA in alignment with client during the initial execution phase. Act as the technical voice of the program, aligning customer expectations with engineering deliverables and strategic goals. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Lead effective engineering change management by proactively tracking evolving inputs and shifting requirements. Evaluate and mitigate the impact of delays on schedule variance, resource planning, costs, and milestone achievement through a structured change control process aligned with client approvals and established governance protocols. Represent engineering during customer technical audits, program quality gate reviews, and change control reviews. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Act as the primary technical/program level interface with the client, ensuring alignment on F&DT compliance objectives and deliverables. Professional & Technical Skills:Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have minimum 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Job Requirements Conduct static, transient, linear, nonlinear, fatigue (LCF/HCF), thermal, and structural analyses of wind turbine components using ANSYS Workbench. Evaluate the structural integrity of components by analyzing stress, strain, displacement, and other relevant parameters under various load conditions. Interpret FEA results, identify potential areas for improvement, and propose design modifications to optimize component performance and reliability. Drive technical solutions and reviews with a design team and multiple sub-suppliers and solution providers. Investigate failures, conduct root cause analysis, and implement solutions to prevent recurring issues in wind turbine components. Identify opportunities to improve FEA processes, documentation, and design methodologies. Prepare and document detailed reports summarizing the FEA analysis, results, and recommendations. Participate in hiring, training, mentoring, and reviewing junior engineers. Embrace a proactive approach to quality by adhering to best practices and QMS processes. Work Experience Postgraduate degree holder in Mechanical engineering with over 10 years of professional experience. Proficiency in Finite Element (FE) tools such as ANSYS (Classic/workbench) is essential. Understanding of the structural design principles for large castings, welded structures, and forged components. Solid grasp of High Cycle Fatigue/Low Cycle Fatigue and fracture mechanics. Hands-on experience in performing analytical calculations for bolted/welded assemblies. Proficient in defining contacts, conducting Nonlinear analysis, and performing Buckling Analysis. Familiarity with certification requirements for components used in Wind Turbine Generators (WTG) or similar applications. Knowledge of International safety and mechanical design standards.

About The Role Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 7.5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Join a mid-level leadership role within the Aerostructure Engineering team, supporting both strategy and technical execution across the full engineering lifecyclefrom concept through production, certification, and sustainment. Play a pivotal role in leading engineering delivery, technical governance, and client interactions for high-impact aerospace programs spanning rotary- and fixed-wing platforms. Opportunity to drive digital engineering initiatives including MBD, MBSE, and digital twin integration within legacy and next-gen design environments. Lead fatigue and damage tolerance (F&DT) analysis for metallic/composite parts in primary and secondary rotary wing structures. Guide interpretation of static analysis to define fatigue-critical areas, calc points, load paths, design intent, and scatter factors per FAR/CS 25.571/29.571, MIL-STD-1530, etc. Prepare method registers, F&DT documents, tool alignment, certification checklists, test report templates, and SLAs per scope and client needs. Manage project scope, constraints, and alignments with client during project initiation. Apply standard F&DT methods and best practices, documenting limitations based on NDE/NDI, manufacturing constraints, and design criteria. Provide expertise in deriving fatigue and test load spectra and formalize via documented procedures. Offer technical oversight across concept design, structural layout, compliance checks, integration, certification, and test phases. Support fatigue test plan creation (full/component level), test result interpretation, and correlation; review team outputs. Act as Level II/III checker, approver, and signatory for F&DT analysis, plans, test orders, and reports. Lead root cause investigations, risk assessments, and resolution of stress/F&DT issues, non-conformances, and airworthiness gaps. Analyze complex design issues and recommend optimal engineering solutions aligned with program goals. Support delivery manager and act as the technical voice of the program, enable aligning customer expectations with engineering deliverables and strategic goals. Front face Accenture in all technical discussions and lead the discussion. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Drive robust engineering change management by closely monitoring evolving inputs and requirement changes. Assess and manage the impact of delays on schedule variance, resource allocation, cost, and milestone delivery through a structured change control process aligned with client approvals and governance protocols. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Collaborate and lead cross-functionally with design/analysis team, manufacturing, quality, and systems teams; actively engage in design reviews, issue resolution, and integration discussions. Act as the technical interface with the client, ensuring alignment of F&DT compliance objectives and deliverables. Professional & Technical Skills: Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO / FRANC 3D / MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA / Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have 12 to 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

The ideal candidate for this position will be responsible for performing finite element analyses using ABAQUS CAE Software, including pre-processing, solving, and post-processing tasks. You will be conducting steady state and transient thermal, structural, and thermo-mechanical analyses using ABAQUS CAE. In addition, you will need to understand and define contacts, conduct nonlinear analysis, vibration analysis, buckling analysis, etc., using ABAQUS. Analytical calculations of bolted/welded constructions will also be part of your responsibilities. It is essential to have a good grasp of high-cycle fatigue (HCF), low-cycle fatigue (LCF), creep, and fracture mechanics. You will be required to drive technical solutions, engage in reviews with internal and external customers, and prepare analysis reports and certification reports. Timely and high-quality deliveries for complex development projects will be a key focus. The successful candidate should possess a graduate/postgraduate degree in Mechanical Engineering or equivalent, with 4 to 5 years of experience in finite element analysis (FEA), preferably in the turbomachinery domain. Strong fundamentals in Finite Element Methods and solid mechanics are required. Experience in performing static/dynamic, linear and non-linear thermal and thermo-mechanical analysis using ABAQUS Software is essential. Knowledge of performing low cycle fatigue, high cycle fatigue, and detailed fracture mechanics assessments will be an added advantage. Having a solution-oriented mindset and approach to work is highly valued in this role. Required Tools: ABAQUS CAE ,

Job Summary: We are looking for a skilled Structural Integrity Engineer with a strong focus on steam turbine operations to ensure the structural soundness and reliability of turbine components operating under high thermal and mechanical stresses. This role supports both design validation and operational diagnostics , helping maintain optimal turbine performance while minimizing the risk of failure or unplanned downtime. What will be my responsibilities? Assess the mechanical integrity of critical steam turbine / expander components including rotors, diaphragms, blades, casings, valve bodies, bolts, and welds using detailed FEA and analytical methods. Evaluate damage mechanisms such as: Low-cycle and high-cycle fatigue (LCF/HCF) Creep and creep-fatigue interaction Thermal ratcheting and cyclic thermal stress Crack initiation and propagation (fracture mechanics) Technology development for Steam Turbine Operations based on Turbine Loading conditions, Controlling Logics, Life Assessment, etc. Collaborate with Thermal cycle, Mechanical design, Operations, and Service / Warranty teams to improve component longevity and reliability. Prepare technical documentation: Integrity Assessments, Risk Analyses, Stress Reports, and Service Recommendations. Provide engineering support during Proposal, Manufacturing / Assembly, Turbine Outages, Overhauls, and Start-up/Shutdown sequences. Stay up to date with steam turbine integrity standards, such as ASME PTC, API 579, and OEM guidelines. As per the business needs, flexibly switch to other calculation topics like Rotor dynamics, Thermodynamics, etc. Therefore, additional experience in such calculations would be a great advantage. What do I need to qualify for this job? BE/B.Tech or ME/M.Tech (Mechanical any Govt. Engineering college) with CGPA > 8.0 Minimum 3-8 years of Engineering experience in Structural Integrity, Materials, Life Assessment criterions. Strong command of FEA tools (e.g., ABAQUS, ANSYS) and fatigue/crack growth software. - Mandatory Understanding of Rotordynamics & Thermodynamics fundamentals will be beneficial. Relevant work experience in Turbomachinery will be added advantage. Knowledge of Finite Element Method (FEM) is mandatory. Ability to work in Global Team in VUCA environment. Why Join Us Be part of a cutting-edge R&D team driving innovation in thermal power. Help optimize asset performance and reduce unplanned downtime. Shape the future of safe, efficient and intelligent turbine operation through engineering excellence. Competitive compensation and career development in a forward-looking engineering environment.

Grade HResponsible for providing Floating Systems expertise to projects or operations, including maintenance, inspection and turnaround, proactively interacting with other disciplines, teams, subfunctions and contractors to systematically resolve problems and applying sound engineering judgement to drive integrated, pragmatic solutions focused on risk management, operating efficiency, defect elimination and standardisation. Entity: Production & Operations Engineering Group Job Description: About bp bp Technical Solutions India (TSI) center in Pune, strives to build on bp s existing engineering and technical strengths to deliver high quality services to its hydrocarbons and new energy businesses worldwide! TSI brings together diverse engineering capability to provide technical services across a range of areas including engineering, maintenance, optimization, data processes, projects and subsurface, to deliver safe, affordable, and lower emission energy, while continuously innovating how we work! Let me tell you about the role The offshore structural engineer will provide subject area expertise for project and operation support, including greenfield and brownfield projects, operational modifications, life extension, and decommissioning support. The engineer will proactively collaborate with other subject areas and contractors to systematically resolve technical challenges, apply sound engineering judgment to drive integrated, pragmatic solutions for risk management, project delivery, operational efficiency, defect elimination, and standardization. The offshore structural engineer would be based in Pune, India. We are looking for a candidate with broad experience in both topside (floating or fixed) and jacket design, construction, and installation, as well as a proven technical background who can make fit-for-purpose recommendations for projects and operations. In addition, the candidate needs strong team member leadership skills and the ability to optimally communicate technical outcomes to ensure engineering risks are understood, controlled, and continuously reduced across the business to deliver safe and reliable results. What you will deliver Responsibilities You will be a coordinated member of the central Civil & Structural (C&S) team, Pune branch, providing technical service work for operations and projects to ensure the safe delivery of projects and the maintenance of operating assets in a suitable condition to deliver the company s safety and business goals. As an offshore structural engineer, you will: define the structural engineering scope of work for new construction, modifications to existing assets, life extension, and decommissioning, focusing on topside structure or jacket; Provide technical assurance for third-party engineering deliveries, ensuring design and operations follow industry codes, company technical practices, and performance standards; Perform independent verification for challenging analyses conducted by third party engineers; Manage relationships with third-party providers and contractors; assess the impact of significant weight and metocean changes to operating assets, and deliver fit-for-purpose solutions that consider operational constraints and asset as-is conditions. You will actively supply to the offshore systems Community of Practice by sharing the standard processes and learning. Additionally, you will: support the Subject Matter Experts (SMEs) with the development and upkeep of company engineering technical practices, ensuring they are fit for purpose, and work with SMEs to address lessons learned. You will drive efforts to ensure offshore structural risks, including pre-service and in-place conditions, operation, or metocean factors, are understood, controlled, and continuously reduced across the business to deliver safe and reliable results, and effectively communicate these risks to business and technical team members. People and business related: Provide visible safety leadership in accordance with bp safety leadership principles, lifesaving rules, and process safety fundamentals to model desired safety behaviours Record relevant lessons learned in the bp shared learning system, bring up as vital and incorporate into local activities and specifications/ practices/ procedures. Support performance management through implementation, measurement, and analysis of relevant KPI s to drive continuous improvement What you will need to be successful Must have educational qualifications: BSc or BEng (UK), BSc (US), or international equivalent in civil/structural engineering, or a closely aligned subject area. Must have certifications: Chartered engineer, professional engineer, or near chartered/professional status in a closely aligned subject area, or evidence of progression towards full chartered/professional status. Preferred education/certifications: Postgraduate qualification in civil/structural engineering or a closely aligned subject area. Minimum years of relevant experience: 10+ years Total years of experience: 10+ years Must have experiences/skills (To be hired with) Knowledge of discipline-related industry standards (API RP 2TOP, 2A-WSD, 2EQ, AISC WSD/LRFD, or ISO 19900/19901/19902 series) and class codes, such as DNV. Proven experience in the design of jackets and fixed platform topsides from in-place condition to construction, transportation, and installation. Skilled in nonlinear finite element analyses, hot spot stress calculations, spectral fatigue analyses, utmost and abnormal level earthquake level analyses for topside structures and jackets. Understanding of the structural theory behind code requirements and being capable of interpolating the code conformance in the context of risk. Proven track record as a technical lead in approving design drawings during detailed engineering. People leadership, teamwork, communication skills, and an ability to network and influence across organizational boundaries. Capable of communicating both verbally and in writing clearly and succinctly. Proficient in English, both written and oral. Individual must be highly motivated and a self-starter. Good to have experiences/skills (Can be trained for learning/on-the-job): Experienced in topside analyses for floating structures. Skilled in fracture mechanics analysis for wave introduced cracks. Experience in management of change, risk assessment, performance management, maintenance, and repair strategies. You will work with Other central subject area engineering teams Major project and global concept design teams Operation site project, execution, and decommissioning teams Projects delivery leads External Vendors and Contractors. Ad hoc teams as required Why join bp: We support our people to learn and grow in a diverse and challenging environment. We believe that our team is strengthened by diversity. We are committed to crafting an inclusive environment in which everyone is respected and treated fairly. There are many aspects of our employees lives that are meaningful, so we offer benefits to enable your work to fit with your life. These benefits can include flexible working options, collaboration spaces in a modern office environment, and many others benefits. Travel Requirement Up to 10% travel should be expected with this role Relocation Assistance: This role is eligible for relocation within country Remote Type: This position is not available for remote working Skills: Agility core practices, Analytical Thinking, Commercial Acumen, Communication, Creativity and Innovation, Data Analysis, Design approaches, Designing for climate change and zero carbon, Digital fluency, Emerging technology monitoring, Engineering evaluation, Incident investigation and learning, Inspection and monitoring strategy, Numerical modelling, Scripting, Sustainability awareness and action, Technology Development, Uncertainty Quantification

Exposure to Aero Repairs/Concession Activities Proficiency in MS Office (Word, Excel, PPT) Hands-on experience with Tools NASTRAN, PATRAN & ISAMI Education Requirements BE / MTech in Aerospace or Mechanical Engineering Skills Required to Succeed in This Job Experience in Aero-structure, preferably with wing and high-lift devices Knowledge of concession treatment process Ability to provide stress assessment for various manufacturing non-conformities Strong knowledge in Strength of Materials, Aircraft Materials, and stress justification using hand calculations (classical methods) Experience working on AIRBUS A350 or legacy programs Familiarity with AIRBUS concession processes and methods Knowledge of AIRBUS-specific tools like ISAMI Experience with SAP PR3/PAC Fatigue and Damage Tolerance experience is an added advantage Able to meet tight deadlines and handle customer demands Willing to work early or late shifts based on project needs

Hi Professionals, We are planning for Scheduled walk-in interviews on 26th July 2025 (Saturday). Only shortlisted candidates will be invited for the interview. Shortlisted candidates will get an official invite with venue details. Walk Interview Location: Bangalore Interview Date: 26th July 2025 (Saturday) Interview Time: 9 AM to 1 PM Interested candidates share your profile to sandhya.rani@quest-global.com Position: FEA/Stress Engineer ANSYS APDL Aero Engine Job Location: Bangalore Exp: 2 to 10 Years Note: Shortlisted candidates should be available for the in-person in the Bangalore office. REFERENCES WOULD BE HIGHLY ENCOURAGED. Job Requirements Structural Analysis Engineer for Gas Turbine Engines Roles & Responsibilities: Performing linear and non-linear structural analysis using ANSYS Mechanical (APDL) Understand and develop run scripts using APDL for different types of structural analysis Developing APDL macros to reduce time in pre & post processing in ANSYS Analysis review document preparation and presenting it to the reviewers during Toll Gate reviews. Participating in the status meeting and communicating with the clients as and when required. Mentoring young engineers and help them to perform their tasks without any mistakes. Maintaining 100% OTD and FTY=1 for himself and for the team Work Experience Required Skills (Technical Competency): Must have 2+ years of experience in FE Analysis using ANSYS Classic Experience in NX UG tool will be a plus. Should have Good Knowledge in Linear & Non-Linear Static, Dynamic, and Thermo-mechanical analysis involving Materials, Geometric & Contact Non-linearitys in ANSYS. Should be Good in hand calculations, Verification & interpretation of FE Results Should have good exposure to Fatigue analysis & Creep calculations. Experience in SIESTA tool will be a plus. Desired Skills: ANSYS APDL HYPERMESH SIESTA PS: Please note that we require all applicants to have experience specifically in ANSYS APDL/Classic. If you do not have this exposure, we kindly ask you not to apply. Thank you for your understanding. We look forward to finding the right candidates for our team! DISCLAIMER: -> No DA / TA Allowed -> Only candidates meeting above respective job descriptions should attend the interview. -> Freshers are not eligible

Carry out static/transient, Linear/Non-linear thermal and thermo mechanical FEA (Finite element analysis) of Gas Turbine static & Rotating components (eg blades & Vanes, combustion, Rotor, casing etc) using commercial software such as ANSYS mechanical, ANSYS workbench, NX-CAE, Nastran & Abaqus. Perform Low cycle fatigue, High Cycle fatigue and detailed Fracture mechanics assessment of Gas Turbine s static & rotating components. Perform high temperature creep calculation and assessment. Creep-fatigue interaction needs to be checked. Prepare and document FE calculation in the form of structural integrity design report. Participate and conduct structural integrity design review at component level. Seamless transfer of structural integrity calculation input and output between design team and project lead respectively. We don t need superheroes, just super minds: Mechanical Engineer graduate/Post graduate from recognized college/university More than 6 years of experience in CAE/FEA (Finite Element Analysis) for linear, Non- linear, static, Transient, thermal and structural calculations. Experience in FEA software ANSYS mechanical or ANSYS Workbench or NX-CAE, Nastran or Abaqus Experience in Product Design in Turbo Machinery or Automotive or General Engineering Strong background in engineering Mechanics and mechanical design. Experience in turbo machinery ie Gas turbine, Steam turbine will be preferred Strong soft personal skill ie team player, quick learner, ability to adapt quickly & effectively etc

We are looking for candidate who has strong hold on structural mechanics Ansys workbench & Mechanical APDL. Is able to perform the required checks to be able to validate the FEA results. Has strong experience in calculation domain. Design and 3D modelling abilities will be a plus Roles and Responsibilities to perform all types of FEA based mechanical calculations for main hydro components to perform fatigue analysis according to ASME FKM Eurocode . to perform welding calculation (static and fatigue assessment) to perform fracture mechanics analysis to perform design optimization and weight reductions by means of design of experiments to support the COEs : valves IB turbine generator and technical tendering regarding calculation. to create quality internal or customer calculation notes in English to participate to the cost out effort particularly by using the optimization tool to suggest solution and design improvement in case of issues to present the results internally or to the final customers Validate calculation of other team members Partner and support with other region; answer technical question and take and be part of technical decision; Required Qualifications University degree in mechanical engineering Good knowledge in machine design MIV turbine and generators Ansys very good knowledge both APDL and workbench good knowledge in design modeler and space claim good knowledge in fatigue fracture mechanics rotor dynamic bearing calculation good knowledge in shaft line calculation Atleast 5 years experience in mechanical engineering Pro-activeness sense of urgency autonomy Good communication skills Ability to work in a multi-cultural and multi-locational environment. Good analytical skills Team player positive willingness to learn & adapt to business needs Ability to travel Strong communication skills What Do We Offer Environment: A multicultural & diverse environment with an enthusiastic team and supportive leaders. We have a pleasant and modern work infrastructure at our offices Opportunities: We offer career growth opportunities professional and personal trainings Benefits: We offer a competitive salary with multiple benefits like subsidized meals medical accidental & life insurance coverage. We provide home office opportunity and flexible working hours (subject to business and HR approval)

Job Requirements Roles & Responsibilities: - Good Understanding of Engineering Drawing, GD&T & Stack-up Analysis - In-depth working knowledge of Aero/Gas turbine engine system, assembly, sub-assembly & parts - Knowledge of Assembly & Dis-assembly of Aero Engine parts - Experience on design reviews, Repair design assessment & Repair substantiation - Knowledge of Mechanical Calculations like Stress/ Kt, Fatigue, Fracture Mechanics, Creep, Overspeed, Buckling & Bolted joints - Knowledge of various manufacturing techniques and also their application during component repair. - Knowledge of various types of repairs which can be applied to components - In-depth knowledge of various failure/ deterioration mechanisms leading to component/ system failures Work Experience Required Skills (Technical Competency): - Teamcenter - Experience on UGNX - Knowledge on ANSYS - Repair design substantiation - Stack-up Analysis - Repair techniques - New Repair development

Job Requirements Job Outline: Providing key Subsea and Onshore Pipelines Systems Integrity technical input and assist in implement the integrity Programs, strategy and the timely and effective implementation of the Subsea & onshore Pipeline systems Integrity Management Programs and advocating Emergency Pipeline Repair System Challenges to be addressed: Delivering the solutions for complex discipline specific and multi-discipline related problems and issues particularly in relation to subsea and onshore pipelines. Delivering end to end solutions through pipeline integrity programs. Developing the work methods from several alternative options in accordance with established pipeline integrity management programs, procedures and professional standards including planning, execution and results assessment concluding pipeline risk assessment and recommendations to extend the remaining life of pipelines. Rapid or immediate response to the pipeline related failure events, issues and/or incidents often requiring team to conduct critical technical tasks and requiring extensive engineering analysis based on available information, in a timely manner and support pipeline related activities, both Offshore and Onshore. Key Job Accountabilities : Perform as subject matter expert in pipelines and subsea structural integrity, ensuring team involvement in all areas of pipeline integrity programs. Oversee the planning and completion of all necessary integrity related tasks and reports the status, results and current issues, and coordinating measurement and verification activities. Performing or advising the checks on data accuracy for different damage mechanism in coordination with other inspection datasets, corrosion monitoring etc. Provides technical and operational support and performs as technical pipeline integrity expert and ensures technical advisory support to all operating areas. Supporting the development, implementation and maintenance of Pipeline Integrity Management system (PIMS) based on the best industry standards supported by computerized system for the management of Threats and Risks, Mitigation Plan, Discovery Management, Integrity Assessment and Performance Monitoring and link program scope with execution activity. Identify, evaluate and implement appropriate new technologies available in the market. Prepares and maintains short and long term pipeline inspection plans based on Company approved inspection strategy. Prepares scope of work for subsea / onshore pipeline inspections including ILI, ROV surveys, CP surveys and any ad-hoc inspections. Ensure all UWI & ILI findings and observations are professionally assessed and classified. Generate technical recommendations and support implementation until satisfactory close-out. Performing internal high end engineering assessments as dents, cracks, free span, buckling etc. Participate in Root Cause Failure Analysis (RCFA), Incident Investigations, SHE reviews (HAZOPs, HAZIDs, risk assessments) Interfaces with Quality groups, performs necessary studies to support the development or understanding of new technologies. Provide integrity input for proposed future pipelines to ensure the facilities and associated documentation are fit and have been designed with long-term integrity considerations. Drive core team members to recruit skilled resources and train internal resources to build required competency Work Experience Qualifications : Engineering degree in Metallurgy, Chemical, Mechanical OR Pipeline engineering 8-10 years of oil gas experience in related industry (Onshore/Offshore pipeline projects and design) Should have sound knowledge on Oil & Gas upstream and downstream business in the following areas Risk Based Inspection methodologies Fracture Mechanics, Flow Assurance, Stress Analysis Engineering assessment of different pipeline damage mechanisms Fixed equipment inspection tasks/ procedures Inspection Optimization Fitness for Service & Life extension studies Repair scope preparation Familiarity with codes and standards Knowledge of software (CAESAR, OLGA, Pestra, Credo, Meridium etc. ) Excellent verbal & written communication Should be able to perform pipeline risk assessments of Offshore & Onshore pipelines Should have knowledge of corrective and preventative maintenance strategy Good interpersonal skills and working collaboratively with the other teams Experience with Office applications (Word, Excel, and Power Point)

Perform fatigue and damage tolerance analysis of metallic and composite structures in accordance with regulatory and OEM standards (e.g., FAA, EASA). Utilize tools like NASGRO , DARWIN , or other proprietary applications for crack growth and fracture mechanics analysis. Conduct life prediction assessments under static and dynamic loading conditions, including variable amplitude loading. Support aircraft certification programs by providing substantiation reports and analysis documentation. Work closely with design, stress, materials, and manufacturing teams to define inspection intervals and structural integrity requirements. Interpret test data and validate analytical models against physical test results. Develop and review fatigue test plans and evaluate test outcomes. Document assumptions, methodologies, and results in clear, traceable technical reports. Required Skills & Qualifications: Bachelor's or Master's degree in Mechanical, Aerospace, or Structural Engineering. 3 to 7 years of experience in fatigue and damage tolerance analysis. Hands-on experience with at least one of the following tools: NASGRO , DARWIN , or equivalent. Solid understanding of fracture mechanics , crack growth behaviour , and fatigue life prediction methodologies. Familiarity with aerospace materials, especially metallic alloys used in aircraft structures. Experience working in a regulated environment with exposure to FAA/EASA certification processes . Strong analytical, problem-solving, and documentation skills. Excellent communication skills and ability to work collaboratively in a multidisciplinary team. Attention to detail and accuracy in calculations and reporting. Proactive attitude towards continuous improvement and learning.

Key Responsibilities: Perform fatigue and damage tolerance analysis of metallic and composite structures in accordance with regulatory and OEM standards (e.g., FAA, EASA). Utilize tools like NASGRO , DARWIN , or other proprietary applications for crack growth and fracture mechanics analysis. Conduct life prediction assessments under static and dynamic loading conditions, including variable amplitude loading. Support aircraft certification programs by providing substantiation reports and analysis documentation. Work closely with design, stress, materials, and manufacturing teams to define inspection intervals and structural integrity requirements. Interpret test data and validate analytical models against physical test results. Develop and review fatigue test plans and evaluate test outcomes. Document assumptions, methodologies, and results in clear, traceable technical reports. Required Skills & Qualifications: Bachelor’s or Master’s degree in Mechanical, Aerospace, or Structural Engineering. 3 to 7 years of experience in fatigue and damage tolerance analysis. Hands-on experience with at least one of the following tools: NASGRO , DARWIN , or equivalent. Solid understanding of fracture mechanics , crack growth behaviour , and fatigue life prediction methodologies. Familiarity with aerospace materials, especially metallic alloys used in aircraft structures. Experience working in a regulated environment with exposure to FAA/EASA certification processes . Strong analytical, problem-solving, and documentation skills. Excellent communication skills and ability to work collaboratively in a multidisciplinary team. Attention to detail and accuracy in calculations and reporting. Proactive attitude towards continuous improvement and learning. Preferred: Experience in aircraft structural analysis . Knowledge of residual strength , multiple-site damage (MSD) , or widespread fatigue damage (WFD) assessments. Familiarity with probabilistic analysis techniques . Experience with scripting or automation (e.g., Python, VBA).

Design and analyze heat exchangers and pressure vessels, perform FEA and thermal-hydraulic calculations, troubleshoot failures, review vendor packages, validate repairs, and ensure compliance with ASME, API, and International O&G standards. Required Candidate profile BE/BTech in Mechanical Engineering with 7–12 years’ experience in heat exchanger and pressure vessel design, FEA, thermal analysis, ASME/API codes, and vendor coordination. Oil & Gas or EPC background

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : Airbus Configuration ToolsMinimum 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking a skilled and detail-oriented Stress Engineer to support the structural analysis of aircraft wing components. The role involves performing static and fatigue & damage tolerance (F&DT) analyses to support in-service structural repairs on aircraft wings. Roles & Responsibilities:Perform detailed static stress analysis of wing structures to support repair solutions for in-service damage.Conduct fatigue and damage tolerance (F&DT) analysis in line with EASA requirements to assess the continued airworthiness of repairs.Develop and validate analytical models (hand calculations, FEM) for primary and secondary structural components.Provide technical substantiation reports and stress dossiers to support repair design and regulatory approval.Collaborate with design engineers to ensure repair feasibility, manufacturability, and certification compliance.Use OEM tools, methods, and allowable (preferably Airbus) for substantiation.Participate in peer reviews, design/stress reviews, and sign-off assigned activities. Professional & Technical Skills: Strong knowledge of static strength, fatigue life estimation, and fracture mechanics.Proficiency in industry-standard tools such as ISAMI, Mathcad, PATRAN.Proficient in engineering documentation systems relevant to Repair.(Tech Request, ICARUS, Airbus World)Familiarity with EASA regulations, structural repair manuals (SRMs), and OEM guidelines (preferably Airbus)Strong problem-solving abilities and an analytical mindset.Good communication and stakeholder management skills.Prior experience in MRO or airline engineering support roles in Repairs will be desirable.Previous experience with Airbus wing structure analysis tools and standards will be desirable. Additional Information:- The candidate should have a minimum of 2 to 8 years of experience in aircraft structures design or repair, preferably with a focus on wings.- This position is based at our Bengaluru office.- A 15 years full-time education is required. Qualification 15 years full time education

Perform fatigue and damage tolerance analysis of metallic and composite structures in accordance with regulatory and OEM standards (e.g., FAA, EASA). Utilize tools like NASGRO , DARWIN , or other proprietary applications for crack growth and fracture mechanics analysis. Conduct life prediction assessments under static and dynamic loading conditions, including variable amplitude loading. Support aircraft certification programs by providing substantiation reports and analysis documentation. Work closely with design, stress, materials, and manufacturing teams to define inspection intervals and structural integrity requirements. Interpret test data and validate analytical models against physical test results. Develop and review fatigue test plans and evaluate test outcomes. Document assumptions, methodologies, and results in clear, traceable technical reports. Bachelor’s or Master’s degree in Mechanical, Aerospace, or Structural Engineering. 7 to 15 years of experience in fatigue and damage tolerance analysis. Hands-on experience with at least one of the following tools: NASGRO , DARWIN , or equivalent. Experience on Stress Concentration evaluation fro Joints and Notches Solid understanding of fracture mechanics , crack growth behavior , and fatigue life prediction methodologies. Ability to use FE tools like HM and Patran for Extraction of Loads/stress for FDT analysis. Familiarity with aerospace materials, especially metallic alloys used in aircraft structures. Experience working in a regulated environment with exposure to FAA/EASA certification processes . Strong analytical, problem-solving, and documentation skills. Excellent communication skills and ability to work collaboratively in a multidisciplinary team.

1 The Geomechanics Fracturing Modeling Specialist will provide fracture modeling support to enhance shale tight (ST) recovery, reduce cost, optimize completion designs, enable safe fracturing operations, reduce environmental risk, and safeguard the system integrity reliability. The position supports the construction, setup and execution of geomechanically models for hydraulic fracturing that are integral to ST business unit (BU) activities. Strong knowledge in fracture mechanics is required. Extensive experience in geomechanics, stimulation and reservoir simulation is required. Advanced degree in geomechanics or related discipline is required. A functional knowledge of shale and tight operations, the role geomechanics plays in them, and geomechanics related business decisions is required. Background in development of 1d or 3D Mechanical Earth Models (MEM) is preferred. The role brings together working subsurface knowledge and expertise in a growing technical area with significant impact to shale tight (unconventional) assets. The role requires close collaboration with subject matter experts and chapter managers in Chevron Technical Center to maintain workflow alignment. Key responsibilities: The position supports the construction, setup and execution of geomechanically models for hydraulic fracturing that are integral to ST business unit (BU) activities. Model construction and analyses are conducted to address geomechanically challenges for ST assets such as: hydraulic fracturing, fracture height growth, drainage height assessment, fracture driven interaction, job optimization including well and cluster spacing, landing point optimization etc. Populate hydraulic fracture models for ST assets with geological and geophysical data, rock properties, pump schedules, fluid rheology and, relevant pressure and temperature conditions under collaboration with relevant subject matter experts in Chevron Technical Center. Execute hydraulic fracture ST models, extract relevant data and manage results repository. Assess interactions between parent and child wells utilizing workflows that couple hydraulic fracture models, reservoir simulators and 4D MEM models. Required Qualifications: BS and MS in Earth science disciplines (Geology, Geophysics, Geomechanics) or Petroleum or equivalent Engineering 5-7 years of pertinent industry experience. Experience in oil and gas industry Experience in hands-on geomechanics hydraulic fracture modeling for ST applications (e.g. Kinetix, ResFrac or equivalent software) Experience with well operations and understanding of the interplay between subsurface conditions in unconventional assets and well performance Experienced in unconventional resources and proficient in a wide range of geomechanics analysis techniques to handle field and well data Preferred Qualifications: 5-7 years of experience in geomechanics field Experience in hydraulic fracture modeling software for shale and tight applications such as Kinetix, ResFrac or StimPlan Experience in one dimensional well log software such as Techlog or Geolog Experience in finite element solvers such as Abaqus, ParaGeo or Elfen Chevron ENGINE supports global operations, supporting business requirements across the world. Accordingly, the work hours for employees will be aligned to support business requirements. The standard work week will be Monday to Friday. Working hours are 8:00am to 5:00pm or 1:30pm to 10:30pm. Chevron participates in E-Verify in certain locations as required by law.

Total Number of Openings 1 About the position: The Mechanical Engineer is part of the Materials Equipment Quality (MEQ) team at the Chevron ENGINE and is responsible for providing expertise in areas of pressure vessel & piping mechanical design/repair/alteration, code interpretation, and post construction repair across Chevron assets. Key responsibilities: Provides enterprise-wide support of in-service pressure vessels and piping, new construction project support, and maintains Chevron s technical standards Assist with concept development, work scoping, troubleshooting, failure analysis and repairs. Support research and technology development projects, Perform mechanical design analysis, using finite element analysis (FEA), of fixed equipment components in pressure vessels, heat exchangers, and piping. Determine stresses applied to components are within allowable stress limits and determine max strain/deflections are also within allowable limits Apply fracture mechanics, fatigue, buckling, creep, and mechanical design principles to evaluate components in mechanical equipment are within allowable stress range Select post construction repair options for mechanical equipment (sleeves, patches, weld repairs, etc) and validate the design meets ASME code requirement Review supplier pressure vessel design packages Required Qualifications: Bachelor's degree in mechanical engineering from a recognized (AICTE) University. Proven experience with ASME Sec VIII Division 1 and 2, PCC-2 Proven experience performing finite element analysis (FEA) Skilled use of an FEA software package such as SolidWorks, Ansys, or Abaqus Skilled use of a pressure vessel design software package such as Compress or PV Preferred Qualifications: 10+ years of experience in pressure vessel or mechanical design in the oil & gas industry Advanced degree in Mechanical Engineering (Masters or Doctorate) Oil & gas or petrochemical experience, or experience working with a pressure vessel fabricator Chevron ENGINE supports global operations, supporting business requirements across the world. Accordingly, the work hours for employees will be aligned to support business requirements. The standard work week will be Monday to Friday. Working hours are 8:00am to 5:00pm or 1:30pm to 10:30pm. Chevron participates in E-Verify in certain locations as required by law.

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As an Engineering Services Practitioner, you will assist with end-to-end engineering services to develop technical engineering solutions, solve problems, and achieve business objectives. You will work across structural and stress design, qualification, configuration, and technical management. Roles & Responsibilities:- Expected to be an SME.- Collaborate and manage the team to perform.- Responsible for team decisions.- Engage with multiple teams and contribute on key decisions.- Provide solutions to problems for their immediate team and across multiple teams.- Lead technical discussions and provide guidance to team members.- Develop innovative engineering solutions to address complex challenges.- Conduct regular reviews and assessments to ensure project success. Professional & Technical Skills: - Must To Have Skills: Proficiency in Fatigue & Damage Tolerance F&DT.- Strong understanding of structural and stress analysis.- Experience in technical management and configuration control.- Knowledge of scientific and socio-economic principles in engineering.- Hands-on experience in developing engineering solutions.- Good To Have Skills: Experience with Finite Element Analysis (FEA). Additional Information:- The candidate should have a minimum of 5 years of experience in Fatigue & Damage Tolerance F&DT.- This position is based at our Bengaluru office.- A 15 years full-time education is required. Qualification 15 years full time education

In this role person demonstrates technical expertise in leading projects to achieve program goals within the program schedule and processes. In this role you will lead in a cross functional team working on GE Aerospace commercial engines like GENX, GE9X, GE90 and GP. You will be responsible for engine critical parts to certify safe and competitive life limits for entire product life cycle. Role Overview: In this role, you will report to Life Management Sub-Section Manager, BEC, JFWTC Bangalore. You will be responsible for engine critical parts to certify safe and competitive life limits for entire product life cycle. Additionally, you need to proactively resolve field issues, enable repairs and serviceable limits. You will interface with other teams such as Life Cycle Engineering, Services Engineering, Systems, Projects, collaboration with FAA, EASA and agencies based on business need. In-depth understanding on solid mechanics In-depth understanding of mechanical/thermal engineering fundamentals Sound knowledge on Fatigue (LCF and HCF) and Fracture mechanics Good Understanding on manufacturing process and rotor hardware Experience in mechanical component analysis (FEA/CAE) and design Own and execute critical parts life management programs, repairs and serviceable limits using sound engineering principles and adhering to business standards, practices, procedures, and product / program requirements. Collaborate and Communicate with all stakeholders on project status, business issues and significant developments as appropriate. Collaborate with regulatory agencies like FAA, EASA and deliver life reports/technical memorandums for assigned programs. Contribute to Life Management Digital play book. Assure proper documentation of technical data generated for the assigned projects and/or tasks consistent with engineering policies and procedures. Demonstrate clear thinking, strong technical articulation, manage hand-offs between different organizations. Foster and inspire a collaborative work style and display team-oriented behavior with a proactive example of communication internally and externally. Required Qualifications: PhD / MTech / MS / BE from an accredited university or college in Mechanical, Aerospace, Structural Engineering. 4+ years of experience in Aviation Engines or Turbo machinery Engineering position (design, analysis, systems, services) In-depth understanding on solid mechanics In-depth understanding of mechanical/thermal engineering fundamentals Sound knowledge on Fatigue (LCF and HCF) and Fracture mechanics Good Understanding on manufacturing process and rotor hardware Experience in mechanical component analysis (FEA/CAE) and design Strong project management skills including cross-functional coordination of activities. Strong Design creativity and problem-solving capabilities. Ability to communicate effectively with all levels of the organization both internally and externally. Preferred Qualifications: Good Knowledge on Field failures and manufacturing processes Experience with engine field problem resolution Familiarity with aircraft flight operations, engine performance, thermal and stress analysis Exposure to FAA requirements for life limited parts Strong oral and written communication skills Relocation Assistance Provided: Yes