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Aerospace Stress Engineer Resume Sample, Experience : 4 years

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Biodata

Name of the Candidate:[Private]
Name of the Post Applied:Aerospace Stress Engineer
Job related skills / software:Hand Calculations, CATIA V5, Excel VBA Macro, Boeing Tools, Airbus Tools, Nastran, Patran, Hypermesh
Category:Design Engineering
Sub Category:CAD Design Engineer / CAD Designer
Years of Experience:4 years
State:Karnataka
Gender:Male
Salary Expected per Month(Rs):50,000 to 60,000
Highest Qualification attained:B.Tech. : Bachelor of Technology
Major / Specialization:Material Sciences & Metallurgical Engineering
Email Id:[Private]
 
Are you looking for job now?:Yes
Can the recruiter contact you?:Yes
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Resume Format / CV Sample Template / Example / Model :

    

Shobhit Rastogi
Current Residence  :Grace House, 8th B Main, BTM Layout, Ist Stage, Bangalore - 029.
Permanent Address  : 239/6, Yahiyaganj Crossing, Lucknow - 003.
Mail  : shobhit.rastogi.sp AT gmail.com, Shobhit_rastogi01 AT infosys.com M: +91-9986527811

CAREER OBJECTIVE  :
To become skilled and innovative professional seeking a challenging position in the field of Engineering Analysis, in a reputed concern for mutual development, progress and promising career.

PROFESSIONAL SYNOPSIS  :
Young, energetic and result oriented professional with an experience of 42 months in Engineering Services and a total experience of 4 yearsin IT industry.
Strong academic background.
Exceptional general management, communication, analytical, inter personal and problem solving skills
Ability to prioritize and remain focused on the essence of an issue
Skilled at learning new concepts quickly, working well under pressure and communicating ideas clearly and effectively
Outstanding within a fast-paced environment, continually taking on increased levels of responsibility

TECHNICAL PROFICIENCY  :
Proficient in Aerospace domain.
Proficient in Static Strength & Stability Analysis for secondary structures in Commercial Aircrafts.
Proficient in Hand Calculations.
Proficient in Boeing tools.
Proficient in MS-Office.
Basic knowledge on CATIA V5, Patran, Nastran, Hypermesh & Excel Macros.
Basic knowledge in Airbus tools.

MANAGEMENT PROFICIENCY  :
Certified Associate in Project Management, Project Management Institute.

PROFESSIONAL EXPERIENCE  :
Infosys Limited, Bangalore. (Dec’09 – to till date)
Stress Engineer
Domain  :Aerospace

Responsibilities  :
Stress Analysis using Classical approach.
Configuration Controller.
Team Mentor.
Core Project Management Team Player.
Team Supervisor.

Hindustan Aeronautics Limited, Lucknow. (May’08 – June’08)Intern (Trainee)
Responsibility  :
Inventory Control for Instrumentation Division.

NIIT, Lucknow. (May’09 – Dec’09) Trainer
Tata Consultancy Services, Lucknow. (July’08 – Aug’08) Summer Trainee

PROJECT DETAILS  :
Project  : Boeing 787-9, S41 - Systems
Scope  : Static Strength Analysis
Organization  : Infosys Ltd.
Client  : Spirit Aerosystems
Scope  : Stress Analysis for System Attachments in Boeing 787-9 (Forward Fuselage, Section 41).

Project Profile  :
The objective of the project is to provide the static strength analysis for system attachments installed in Section 41 (Forward Fuselage) of Boeing 787-9. The system attachments, generally, comprises of spanner bars, metallic brackets and standoffs supporting the Wiring Harness/Environment Control Systems installations and metallic panels and fittings supporting Electrical Equipments.

Role  : Team Mentor and Configuration Controller
Team Size  : 7

Contribution/Highlights  :
Involved in static strength analysis of parts by classical stress approach and Boeing tools.
Acted as a coordinator between the onsite and the offshore team.
Responsible for requirement gathering and work allocation.
Team Mentoring.
Responsible for offshore analysis review.
Resizing and design change propositions.
Acted as a coordinator between the design and stress team.
Responsible for analysis documentation.
Worked as Configuration Controller for the project.
Responsible for developing training and analysis methodology material.
Role play in Team Management.

Project  : Boeing 787-9 - Flight Deck Floors - Layouts
Scope  : Static Strength Analysis
Organization  : Infosys Ltd.
Client  : Spirit Aerosystems
Scope  : Stress Analysis for Wiring & Ducting support installations in Boeing 787-9 (Flight Deck Floor, Section 41).

Project Profile  :
The objective of the project is to provide the static strength analysis for the system attachments installed in Flight Deck Floor region. The system attachments, generally, comprises of spanner bars, metallic brackets and standoffs supporting the wiring harness or Environment Control System installations. The analysis is mainly done using classical stress methodologies.
Role  : Team Mentor and Configuration Controller
Team Size  : 7

Contribution/Highlights  :
Involved in static strength analysis of installations by classical approach and Boeing tools.
Acted as a coordinator between the onsite and the offshore team.
Responsible for requirement gathering and work allocation.
Team Mentoring.
Responsible for offshore analysis review.
Resizing and design change propositions
Acted as a coordinator between the design and stress team.
Responsible for analysis documentation.
Worked as Configuration Controller for the project.
Project  : Boeing 787-8 - Refurb

Scope  : Static Strength Analysis
Organization  : Infosys Ltd.
Client  : Spirit Aerosystems

Project Profile  :
The objective of the project is to provide the Stress Substantiation for Loose Hardware attachments essential for Airworthiness certification.
Role  : Team Member
Team Size  : 12

Contribution/Highlights  :
Involved in static strength analysis of parts using various tools and hand checks.
Responsible for analysis documentation.

Project  : Spanner Bar Analysis
Scope  : Static Strength Analysis
Organization  : Infosys Ltd
Client  : Spirit Aerosystems

Project Profile  :
Scope of this project involves identification of Ducts and wires connecting to spanner bars of Electrical Design Zones (EDZ’s) and estimation of the loads for each of the set of wires and ducts that attach to the spanner bars.
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Once the loads are estimated, Shear force, Bending moment, Axial and Torsion diagrams are drawn for each of the spanner bars. The spanner bars are analyzed at the critical location from the maximum loads obtained from the SF and BM diagrams. Prepared strength check notes (SCN) for the spanner bar analysis of Section 41 of 787 dream liner.

Role  : Team Member
Team Size  : 12

Contribution/Highlights  :
Involved in static strength analysis.
Responsible for analysis documentation.

Project  : NCR Sustaining
Scope  : Sustenance Analysis
Organization  : Infosys Ltd.
Client  : Spirit Aerosystems

Project Profile  :
Non compliance rejection tags are raised against the defects arising at shop floor during manufacturing and installation processes. The parts have to be checked for the sustenance in accordance with the repair processes. The joint locations have to be reanalyzed as there is an impact on the bearing and bypass loads in the joints and the new interaction margin has to be tabulated. The defected parts are mainly analyzed for their static stability on their usage or installation. The project is critical as it affects the production time on the shop floor.
Role  : Team Member
Team Size  : 4

Contribution/Highlights  :
Worked for process automation and reducing the part hold time on floor shop.
Acted as a coordinator between onsite and offshore team.
Mentored the team.
Managed work allocation according to the team size.
Responsible for offshore review.
Responsible for analysis documentation.
Worked as Configuration Controller for the project.

Project  : Skin Stringers
Scope  : Static Strength & Stability Analysis
Organization  : Infosys Ltd.
Client  : Spirit Aerosystems

Project Profile :
The scope of this project involves static & stability analysis for skin & stringers of Section 15 (Fuselage) of Airbus XWB - 900. The scope also includes joint analysis for skin with A-brackets (brackets attaching to primary structures), creation of PSN1 files for GFEM modifications as per the latest resizing configuration of skin panel & stringers and panel modeling in Airbus FE tool.
Role  : Team Member
Team Size  : 4

Contribution/Highlights :
Involve in stress analysis activities.
Involve in requirements gathering and initial input study.
Involve in efforts estimation.
Involve in Team management and Process Management.
Working as Configuration Controller.
Involve in Team mentoring & imparting training sessions.

EDUCATION SYNOPSIS :
Degree School/College University/Board Year of passing Percentage High School
Lucknow Public School U.P. Higher Secondary Education 2003 75.6
Intermediate Lucknow Public School U.P. Higher Secondary Education 2005 84.2
B.Tech. (Material Sciences and Metallurgical Engg.) Institute of Engineering and Technology CSJM University 2009 66.9

EXTRA CURRICULAR ACHIEVEMENTS :
“Spot Award Winner for Excellence” in contribution towards developing analysis tools in Excel for System Attachment Analysis and Team Knowledge Management.
Contributed in Knowledge Management by publishing BOK for System Attachment Analysis.
Participated in several Debate Competitions on State and City Level during schooling tenure.

PERSONAL PROFILE :
Name  : Shobhit Rastogi
Father’s Name  : Mr. Arvind Rastogi
Age  : 25 years
Date of Birth  : 18th March, 1987.
Marital Status  : Unmarried
Permanent Address  : 239/6, Yahiyaganj Crossing, Lucknow.
(Shobhit Rastogi)

Date : 11/06/2013

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