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15.0 - 20.0 years
17 - 22 Lacs
Bengaluru
Work from Office
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
Posted 11 hours ago
10.0 - 15.0 years
10 - 15 Lacs
Hyderabad
Work from Office
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.
Posted 11 hours ago
5.0 - 10.0 years
4 - 8 Lacs
Bengaluru
Work from Office
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
Posted 4 days ago
2.0 - 5.0 years
3 - 6 Lacs
Coimbatore
Work from Office
Support the DIC by accomplishing efficient On time Delivery of design release, First time right, and Continual Improvement on skill in Design for Composite parts. Responsibilities Accountabilities Support the DIC by accomplishing efficient On time Delivery of design release, First time right, and Continual Improvement on skill in Design and Analysis. Support the DIC In manging the budget for Engineering department and ensuring that resources are used efficiently. Suggest innovative ideas to reduce cost and improve productivity and efficiency. Control the rejections so as to save costs and produce outputs that are as per specified quality standards and as per customer requirements. Enable customer satisfaction by driving efficiency in internal processes within the department. Ensure appropriate, suitable actions towards customer complaints, so as to facilitate both customer retention as well as identify methods that helps in preventing such breakdowns from recurring. Stress analysis (Composite Metallic) and to checking the detail as per any OEM standards. To work with various analysis types such as linear statics, nonlinear statics (contact, material and large deformation), dynamics (normal modes and cyclic modal). Working knowledge of PATRAN/NASTRAN is most essential requirement. Familiarity with other FEA software will be an advantage Designing of composite parts through Composite Design (CPD) in Catia. Performing FE Modeling (Shell and Solid), FE Analysis for various structural Components. Good exposure on Material properties and allowable. Experience in Hand calculations. Providing design Suggestion /Modification based on failure. Interpreting and understanding FEA results, post-processing and preparing comprehensive analysis reports. Plan and promote continuous improvements in material, machine utilization and process to improve section individual productivity, and quality of the product. Coordinate with the automation team to identify use cases and drive automation / process improvement initiatives within the Section
Posted 5 days ago
12.0 - 17.0 years
16 - 20 Lacs
Bengaluru
Work from Office
At Boeing, we innovate and collaborate to make the world a better place. We’re committed to fostering an environment for every teammate that’s welcoming, respectful and inclusive, with great opportunity for professional growth. Find your future with us. Overview As a leading global aerospace company, Boeing develops, manufactures and services commercial airplanes, defense products and space systems for customers in more than 150 countries. As a top U.S. exporter, the company leverages the talents of a global supplier base to advance economic opportunity, sustainability and community impact. Boeing’s team is committed to innovating for the future, leading with sustainability, and cultivating a culture based on the company’s core values of safety, quality and integrity. Technology for today and tomorrow The Boeing India Engineering & Technology Center (BIETC) is a 5500+ engineering workforce that contributes to global aerospace growth. Our engineers deliver cutting-edge R&D, innovation, and high-quality engineering work in global markets, and leverage new-age technologies such as AI/ML, IIoT, Cloud, Model-Based Engineering, and Additive Manufacturing, shaping the future of aerospace. People-driven culture At Boeing, we believe creativity and innovation thrives when every employee is trusted, empowered, and has the flexibility to choose, grow, learn, and explore. We offer variable arrangements depending upon business and customer needs, and professional pursuits that offer greater flexibility in the way our people work. We also believe that collaboration, frequent team engagements, and face-to-face meetings bring together different perspectives and thoughts – enabling every voice to be heard and every perspective to be respected. No matter where or how our teammates work, we are committed to positively shaping people’s careers and being thoughtful about employee wellbeing. Position Overview Boeing India Engineering is currently looking for Lead Structural Analysis Engineer ( Service Engineering ) to support Airframe Service Engineering Capability at Boeing India, Bangalore. This position will focus on providing 24/7 support to Boeing commercial airplane customers. This position offers a unique opportunity to work complex technical challenges in support of safety operation and return to service. Our team of engineers support over 14,000 aircraft around the globe, and work closely with our customers to ensure that their fleet is operating safely, efficiently, and reliably. Join us today and help shape the future of commercial aviation. Position Responsibilities Primary responsibilities for this position include: Responsible for performing structural analysis of aircraft components, assemblies, and systems while working as an integrated team Responsible to collaborate with Service Engineers to perform root cause analysis and corrective actions on In-Service issues for Airframe and other Mechanical systems. Performs detailed structural analysis (static strength, durability/fatigue and damage tolerance) to determine structural integrity (margins of safety), using classical techniques and Boeing tools. Evaluate structural integrity of aircraft components by way of classical hand calculations and, finite element method Generate documentation to report analysis and test results to support certification/Qualification Support Gated Reviews to validate the quality and completeness of work packages Familiar with regulatory framework (FAA and Mil-Spec), for warranting safety and regulatory compliance. Guides structural design and configuration development. Supports in-service products by investigating failures and analyzing improvements Performs trade studies to optimize structure and meet program requirements. Researches and prepares data to support definition of structural design requirements. Willing to support a 24/7 on-call rotation schedule and the ability to work variable shifts, including weekends or overtime. Basic Qualifications (Required Skills/Experience) Bachelor’s degree in Mechanical/Aerospace/Applied Mechanics/Structural engineering and 12+ years of experience in stress analysisin Services related to Fleet Support. Preferred Qualifications (Desired Skills/Experience) Experience in structural analysis of various airframe structures Experience of Aircraft maintenance and service procedures Experience with structural analysis of metallic and composite structures (good experience with composite structures) Experience with static, fatigue and damage tolerance analysis Knowledge of airplane operating environments Robust understanding of engineering fundamentals such as material properties, Free-body diagrams, structural loads and analysis methods Experience in utilizing FEM software (e.g., ABAQUS, PATRAN/NASTRAN, Hyperworks) Experience or training with computer programming languages (e.g., Matlab, Python, Visual Basic) Experience in utilizing industry CAD systems (e.g., NX/Teamcenter and CATIA/ENOVIA) Candidate demonstrates excellent analytical and problem-solving skills Good verbal and written communication skills to liaise with several Stakeholders Ability to work across functional teams and organizations Willingness to expand into technical areas without prior experience Desire to continuously improve our airplanes Typical Education & Experience Education/experience typically acquired through advanced education (e.g. Bachelor) and typically 12+ years' related work experience or an equivalent combination of education and experience (e.g. Masters+11 years' related work experience etc.) Relocation This position does offer relocation based on candidate eligibility within INDIA. Applications for this position will be accepted until Jun. 06, 2025 Export Control This is not an Export Control position. Education Bachelor's Degree or Equivalent Required Relocation This position offers relocation based on candidate eligibility. Visa Sponsorship Employer will not sponsor applicants for employment visa status. Shift Not a Shift Worker (India) Equal Opportunity Employer: We have teams in more than 65 countries, and each person plays a role in helping us become one of the world’s most innovative, diverse and inclusive companies. We are proud members of the Valuable 500 and welcome applications from candidates with disabilities. Applicants are encouraged to share with our recruitment team any accommodations required during the recruitment process. Accommodations may include but are not limited toconducting interviews in accessible locations that accommodate mobility needs, encouraging candidates to bring and use any existing assistive technology such as screen readers and offering flexible interview formats such as virtual or phone interviews.
Posted 1 week ago
10 - 20 years
15 - 22 Lacs
Bengaluru
Work from Office
Greetings from Metrics Numero Talent Acquisition Team !!! Metrics Numero and Alpha Numero are group companies , offering top-of-the-line Avionics/Aerospace technology services and Solutions, ERP consulting and SMA/SME services, AI Data and Analytics, Software Consulting, Mechanical Engineering and Design Services, as well as Product Design and Engineering. Experience : 7+ Yrs Location : Bangalore Job Description : Good experience in Stress Analysis experience in Aerospace Domain. Able to analyse stress (Static and Fatigue) and perform hand calculation Experience with FEM tool (Hyperworks /Nastran /Patran) Experience in DTA (Damage Tolerance Analysis) would be preferred Good technical leadership and delivery management skill
Posted 1 month ago
10 - 15 years
12 - 17 Lacs
Hyderabad
Work from Office
Minimum 5-15 years experience in aerostructure analysis, with minimum of 3 years of experience in composite analysis. Excellent knowledge of Aircraft Primary and Secondary structureal components. Hands-on experience with relevant tools (ISAMI, NASGRO, MSC Nastran/Patran and Altair Hypermesh). Experience on Simcenter 3D is an advantage. Knowledge on CATIA is desirable Strong experience in Static Strength, Fatigue & Damage Tolerance Analysis of aircraft primary structures A strong theoretical and practical foothold on analyses of metallic and composite structures Domain-wide experience from initial sizing to aftermarket services A well-balanced expertise including a sound understanding of basic structural concepts, hand calculations Knowledge of concessions and MRB
Posted 3 months ago
2 - 5 years
4 - 7 Lacs
Bengaluru
Work from Office
About The Role : Primary Skill: hypermesh experinece with 2 years in Abaqus - minimum 1 year of experience Good in client management, good communication skills Secondary skill: Hypermesh, Nastran, TCL, Python
Posted 3 months ago
5 - 9 years
7 - 11 Lacs
Bengaluru
Work from Office
Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:-Engineering Services Senior Analyst - L10 Role:- Stress Analysis Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Experience in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Experience in Buckling and Modal Analysis. Experience in engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Experience Sizing/Justification of aircraft components by providing the solution to the problem. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. Stress tasks quality check Qualification Who are we looking for? 5 to 9 years of Aerostructure Stress Analysis Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to work individually and Guide the team. Supporting continuous improvement initiatives to increase team efficiency. Highly preferred primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.
Posted 3 months ago
2 - 5 years
7 - 11 Lacs
Bengaluru
Work from Office
Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:-Engineering Services Senior Analyst - L10 Role:- Stress Analysis Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Experience in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Experience in Buckling and Modal Analysis. Experience in engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Experience Sizing/Justification of aircraft components by providing the solution to the problem. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. Stress tasks quality check
Posted 3 months ago
5 - 10 years
7 - 11 Lacs
Bengaluru
Work from Office
Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:- Engineering Services Specialist - L9 Role:- Stress Analysis Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Expertise in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Expertise in Buckling and Modal Analysis. Strong technical aptitude, including applicable engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Expertise in Sizing/Justification of aircraft components by providing the mitigation solution for critical components. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing and checking skills. Building, Leading, and guiding the team to execute the tasks. Stress quality check and Delivery responsibility. Training the resources to fill the knowledge gap. Qualification Who are we looking for? Overall 9 to 12 years of experience in Aerostructure domain Minimum 9 years of Aerostructure Stress Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred A350/A350F primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.
Posted 3 months ago
5 - 10 years
7 - 11 Lacs
Bengaluru
Work from Office
Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:- Engineering Services Specialist - L9 Role:- Stress Analysis Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Expertise in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Expertise in Buckling and Modal Analysis. Strong technical aptitude, including applicable engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Expertise in Sizing/Justification of aircraft components by providing the mitigation solution for critical components. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing and checking skills. Building, Leading, and guiding the team to execute the tasks. Stress quality check and Delivery responsibility. Training the resources to fill the knowledge gap.
Posted 3 months ago
5 - 9 years
6 - 10 Lacs
Bengaluru
Work from Office
Entity:- Accenture Industry XPractice:- Aero Engineering (Aerostructure)Title:- Engineering Services AnalystRole:- F&DT EngineeringJob location:- BangaloreAbout Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments.Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs Fatigue and Damage Tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phases.What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX and Cargo floors. Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis) Experienced in spectrum generation. Calculation of Fatigue life by using or DFEM or ISAMI modules. Understanding of mission profiles, calculating rain flow counting, Preparation of stress files and FESPS databases Knowledge on Material and surface protection treatment to be used for fatigue calculations. Experience on Damage tolerance, crack propagation analysis on aircraft components. Should have strong foundation in the area of load/stress analysis with abilities to formulate "free body diagrams" and identify load path of structures. Knowledge on Non-destructive testing approaches. Experience with the use of both Finite Element (NASTRAN/PATRAN/HYPER MESH) and classical methods to perform structural load/Fatigue stress analysis for primary airframe structures is preferred. Continuous learning ability to understanding best practices in analysis and methodologies. Good Knowledge on CATIA and experience in reading assembly drawings. Strong Technical Report (Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. F&DT tasks quality check. Qualifications Who are we looking for? 5 to 9 years of Aerostructure F&DT Analysis Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage.Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.
Posted 3 months ago
5 - 9 years
7 - 11 Lacs
Bengaluru
Work from Office
Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:- Engineering Services Senior Analyst - 10 Role:- F&DT Engineering Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments. Know more:- www.youtube.com/watchv=XaLxTEI3atI WHAT'S IN IT FOR YOU Performs Fatigue and Damage Tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phases. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX and Cargo floors. Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis) Experienced in spectrum generation. Calculation of Fatigue life by using or DFEM or ISAMI modules. Understanding of mission profiles, calculating rain flow counting, Preparation of stress files and FESPS databases Knowledge on Material and surface protection treatment to be used for fatigue calculations. Experience on Damage tolerance, crack propagation analysis on aircraft components. Should have strong foundation in the area of load/stress analysis with abilities to formulate "free body diagrams" and identify load path of structures. Knowledge on Non-destructive testing approaches. Experience with the use of both Finite Element (NASTRAN/PATRAN/HYPER MESH) and classical methods to perform structural load/Fatigue stress analysis for primary airframe structures is preferred. Continuous learning ability to understanding best practices in analysis and methodologies. Good Knowledge on CATIA and experience in reading assembly drawings. Strong Technical Report (Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. F&DT tasks quality check. Qualifications Who are we looking for 5 to 9 years of Aerostructure F&DT Analysis Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.
Posted 3 months ago
8 - 12 years
10 - 14 Lacs
Bengaluru
Work from Office
Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:- Engineering Services Specialist Role:- F&DT Engineering Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs Fatigue and Damage Tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phases. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX and Cargo floors. Expertise of Fatigue life calculation by using DFEM or ISAMI modules, Crack Propagation Analysis. Expertise in ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch, Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.,) Experience with the use of both Finite Element (NASTRAN/PATRAN/HYPER MESH) and classical methods to perform structural load/Fatigue stress analysis for primary airframe structures is preferred. Expertise in Sizing/Justification of aircraft components by providing the mitigation solution for critical components. Experienced in documents (like PDR/CDR/Certification reports, Concessions, Repairs) and report creation and getting validated. High level of customer and quality orientation together with strong abilities in consulting and implementation. Experience on to industry standard verification & validation methods Good written and oral communication skills in English. Perform in a pressure environment and make quick yet meaningful decisions. Continuous learning ability to understanding best practices in analysis and methodologies. Good Knowledge on CATIA and experience in reading assembly drawings. Strong Technical Report (Dossier) writing and checking skills. Building, Leading, and guiding the team to execute the tasks. F&DT quality check and Delivery responsibility. Good experience in planning the training for freshers and experienced resources to fill the knowledge gap. Qualifications Who are we looking for? Overall 8 to 12 years of experience in Aerostructure domain Minimum 9 years of Aerostructure F&DT Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred A350/A350F primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.
Posted 3 months ago
4 - 9 years
6 - 11 Lacs
Bengaluru
Work from Office
Entity:- Accenture Industry XPractice:- Aero Engineering (Aerostructure)Title:- Engineering Services Associate Manager - L8Role:- F&DTJob location:- BangaloreAbout Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitmentsKnow more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs Fatigue and Damage Tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phases.What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX and Cargo floors. Expertise of Fatigue life calculation by using DFEM or ISAMI modules, Crack Propagation Analysis. Expertise in ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch, Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.,) Experience with the use of both Finite Element (NASTRAN/PATRAN/HYPER MESH) and classical methods to perform structural load/Fatigue stress analysis for primary airframe structures is preferred. Expertise in Sizing/Justification of aircraft components by providing the mitigation solution for critical components. Experienced in documents (like PDR/CDR/Certification reports, Concessions, Repairs) and report creation and getting validated. High level of customer and quality orientation together with strong abilities in consulting and implementation. Experience on to industry standard verification & validation methods Good written and oral communication skills in English. Perform in a pressure environment and make quick yet meaningful decisions. Continuous learning ability to understanding best practices in analysis and methodologies. Good Knowledge on CATIA and experience in reading assembly drawings. Strong Technical Report (Dossier) writing and checking skills. Good Experience in preparing effort estimation, Planning of the project deliverables and risk assessment. Customer interaction regarding technical discussion and project status. Capable of handling multiple projects. Building, Leading, and guiding the team to execute the tasks. F&DT quality Qualifications Who are we looking for? Overall 14+ years of experience in Aerostructure domain Minimum 12 years of Aerostructure F&DT Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred A350/A350F primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage.Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.
Posted 3 months ago
3 - 5 years
5 - 9 Lacs
Bengaluru
Work from Office
Project Role : Manufacturing Engineering Practitioner Project Role Description : Define processes to fabricate, assemble, inspect and test new products and machines based on production engineering and design principles. Define the supporting tools and fixtures needed for production. Develop procedures, product specifications and define the quality standards and inspection methods. Must have skills : Aircraft Structural Analysis Good to have skills : NA Minimum 3 year(s) of experience is required Educational Qualification : Bachelors or Masters degree in Mechanical or Aerospace or Structural engineering Summary :As an Aircraft Structural Analysis Manufacturing Engineering Practitioner, you will be responsible for defining processes to fabricate, assemble, inspect, and test new products and machines based on production engineering and design principles. Your typical day will involve developing procedures, product specifications, and defining quality standards and inspection methods for aircraft structural analysis. WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Experience in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Experience in Buckling and Modal Analysis. Experience in engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Experience Sizing/Justification of aircraft components by providing the solution to the problem. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. Stress tasks quality check Who are we looking for? 5 to 9 years of Aerostructure Stress Analysis Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to work individually and Guide the team. Supporting continuous improvement initiatives to increase team efficiency. Highly preferred primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Qualification Bachelors or Masters degree in Mechanical or Aerospace or Structural engineering
Posted 3 months ago
3 - 8 years
7 - 15 Lacs
Pune
Hybrid
Required Domain Expertise (skills): Graduate / Post Graduate Engineer (Aerospace Engineering / Mechanical Engineering). Experience working with Aerospace OEM / Tier / Suppliers on Specific Design activities. Tools : Patran/Nastran, Hypermesh, ISAMI (preferred) Experience: 3 - 10 years Soft skills: Ability to work independently & in a team ( including overseas teams) Ability to communicate effectively (oral, written & presentation) Flexibility & adaptability to changing project scenarios and requirements Key skills: Sound knowledge of structural design principles, aircraft loads and aircraft structures Experience in static, fatigue and damage tolerance analysis of aircraft structural components (Airbus methods and tools would be preferable) Background in design and sizing of aircraft primary structure components and parts Ability to liaise/negotiate with design, stress, EU teams and customer services Certification requirements and experience with stress dossiers Finite element method / finite element analysis (FEM / FEA) Very good analytical and reasoning skills Job Description: Stress analysis of metallic and composite aircraft structures using hand calculations, ISAMI, GFEM and DFEMs Extraction of loads, stresses, generation of spectra and mission files Extraction of material data, geometry details and fastener specifications from part & assembly drawings Application of appropriate static, fatigue and damage tolerance design values from standard references. Creation of FEMs using geometric data from part & assembly drawings Sizing of primary and secondary parts for static and fatigue requirements. Fastener load extraction and joint analysis. RF calculation for different failure modes such as strength, buckling, shear panel failure, damage tolerance etc. Low RF mitigations using classical or numerical methods. Preparation of stress certification dossiers, ACD4 and ACD6
Posted 1 month ago
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