Aerospace engineer, Aircraft structural analysis, Nastran, Hypermesh

Vivi Richard D

**************@*****.*** +91-822**-***** / +91-701**-*****

ABOUT

An efficient, dedicated aeronautical engineering professional with 5 years of experience in Aerospace Domain. Experience in classical hand calculation methods for Metallic &Composite Structure Stress Analysis. Ability to adapt quickly to new tools, technical skills and new environments while completing assignments with timeliness and accuracy as priorities.

EXPERIENCE

QuEST Global Engineering Services Pvt Ltd Bangalore, India

STRESS ENGINEER Aug 2018 – July 2020

Performing Static and fatigue strength analysis of aircraft engine nacelle components.

Accomplishing 2D & 3D meshing of electrical and hydraulic brackets. Generating corresponding .bdf files for analysis of brackets.

Supporting for MRB stress on various composite and metallic nonconformance such as Void, Delamination, Wrinkles, FOD, Gouges, Dent, Hole Mis location, Oversized holes flushness. etc.

Design, Stress analysis and Dossier writeup for Mi-17 Helicopter structural modifications.

Preparing formal calculation reports and documentation in support for the concession approval process.

Bangalore Aircraft Industries Pvt Ltd Bangalore, India

ASSISTANT STRUCTURAL ENGINEER Dec 2015 – Jul 2018

Ensuring that designs are prepared in accordance with the necessary standards and procedures.

Conduct extensive research to develop specific designs as per requirements.

Provide support and assistance to lead engineers in the various tasks assigned to them.

EDUCATION

Sathyabama University 2011 – 2015

Bachelor of Engineering in Aeronautical Engineering Chennai

Don Bosco Higher Secondary School 2011

Higher Secondary Certificate (Computer Science, Math, Physics, Chemistry) Tiruvallur, India

78 % in Higher Secondary Certificate

Inter School State Level Basketball Player

Don Bosco Higher Secondary School 2011

Secondary School Leaving Certificate Tiruvallur, India

90 % in SSLC

PROJECTS

A320 (Engine nacelle) MRB Stress Support

Involved in MRB activities and QN releases A320 neo Nacelle which involves analysis and disposition repairs for structural non-conformances in a timely manner to restore design integrity.

Carried out static & fatigue stress calculations to assess design solutions for a range of tasks, ranging from modifications to manufacturing concessions against the Nacelle Design requirements

Analyzing the engineering problems occurring during production with extensive use of PATRAN, NASTRAN and various UTAS in house tools.

Report critical technical issues up through functional management.

Static and Fatigue Analysis of Interior Structural Parts

Design, Stress analysis and dossier write up for Mi-17 helicopter structural modifications.

Preparing formal calculation reports and documents in support for the approval process.

Static and Fatigue Analysis of Interior Structural Parts

2D & 3D meshing, pre-processing of electrical & hydraulic brackets was performed and corresponding .bdf files for analysis of brackets are generated.

Design and stress analysis of lug attachment brackets

Design and Stress analysis of wing to fuselage lug attachment. Preparing formal calculation reports and documentation

SKILLS

Skills: Classical hand calculation methods, Strength of materials Static & fatigue concepts of airframe, Msc. Patran & Nastran, Hypermesh, CATIA V5 ELAM (in-house tool), MS Office.

AWARDS

On the fly award, QuEST Global, (2018)

Place: Bangalore

Date: (VIVI RICHARD. D)

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