Darshan K R is seeking a position that allows him to utilize his 3.6 years of professional experience. He has a B.E. in Industrial and Production Engineering and a diploma in Mechanical Engineering. His experience includes over 2 years working as a Design Engineer at Aeronautical Development Agency, where he has designed structural components for aircraft integration projects. He also has experience as a Project Executive Engineer and Lab Engineer Trainee. His technical skills include CAD modeling in CATIA V5 and structural analysis. He is proficient in design standards and has experience designing aircraft structural parts and assemblies.

1. RESUME
DARSHAN.K.R
Mobile: +91-9740460520
Office No: 080-25087365
E-mail: darshankr2589@gmail.com
OBJECTIVE:
“I am looking for an opportunity where I can use my professional experience. To be an integral part of a
competitive work environment and evolve my technical and professional skills continuously with
commitment for the benefit of the organization and personal growth.”
PROFESSIONAL QUALIFICATION DETAILS:
 B. E, Industrial and Production Engineering (2009-2012) from U.B.D.T College of Engineering,
Davanagere-577004, Kuvempu University with CGPA 7.3 aggregate.
 Diploma Mechanical Engineering (General) (2006-2009) from M.N. Technical Institute
Kammagondanahalli Bangalore-15 with 75% aggregate.
PROFESSIONAL EXPERIENCE DETAILS:
 2.5 years of Experience in Aerospace Design & Development Domain.
 3.6 years overall work experience.
 From Feb 2014 to till date Working as Design Engineer at AERONAUTICAL DEVELOPMENT AGENCY,
MINISTRY OF DEFENCE, Bangalore.
 From July 2013 to Jan 2014 Worked as Project Executive Engineer (supply chain dept.) in ZENITH
PRECITION PVT LTD.UNIT 2 (AEROSPACE DIVISION), Bangalore.
 From Nov 2012 to June 2013 Worked as Lab Engineer trainee (Quality dept.) in SaRc INSTRUMENTS,
Bangalore.
SUMMERY OF TECHNICAL SKILLS & KNOWLEDGE:
 Design of aircraft structural components in a Design-in-context Environment in VPM.
 Finalization of design in coordination with Materials, Stress & Fatigue group.
 Generation of 3D models and detail drawings for fabrication and other downstream activities using
CATIA V5 R19.
 Creating & managing the data in VPM, Creation of PSN tree structure for sub assembly,
Assembly and parts with appropriate NMG’S.
 Finalizing the fasteners type, locations based on the detail design practice.
 Validation of models & drawings against the company standards before initiating action for
Release through VPM.
 Generating & managing Project Slips, Change notice & Higher issue drawings through VPM.
 Detail design support for the disposition given to snags, Production & Shop query.
 Generation of material schedule, stock size, MS sheet attributes, drawing sheet attributes
Through VPM.
 Estimation of number of fastener based on the joint loads.
 FE analysis of metallic structural components of Light Combat Aircraft
(LCA) at part and assembly level.
 Joints/Fastener design by hand calculation used in aircraft components.
 FE analysis includes linear static, non-linear static, analysis.
 Exposure in Catia modeling and Design of Aero Structural Assemblies and Parts.
 Exposure in Using Geometrical Dimensioning & Numerical Tolerance (GD&T -14.5) in compliance with
ASME standards.
 Exposure in Drafting Aero Structural Parts, Assembly, Installations Drawing

2. (Metallic, Non-Metallic, Sheet metal, Composite Parts Drawings).
 Well Versed with Hindustan Aeronautics Limited (HAL) design standards.
 Effective utilization of DFM and DFA techniques to design cost effective and light weight components
and to meet the functional requirements
 Preliminary Catia analysis has been carried out on MMR structure assembly.
 CAD : CATIA V5 R19, AUTO CAD, SOLID WORKS.
 PLM : ENOVIA (VPM).
 PDM : TEAM CENTER.
 Exposure in strength of material, machine design, mechanical fundamentals.
PROJECT DETAILS:
Organization: AERONAUTICAL DEVELOPMENT AGENCY, MINISTRY OF DEFENCE, Bangalore.
Designation: Design Engineer
Period: 1.3 Years (19 Feb 2014 - till date)
Project 1: Design of Structural components for Integration of Aerial refueling probe on LCA-Mk1
Aircraft
Team size: 7 Role: Team Member Duration: Feb 2014 to till date
Work description:-
 Feasibility study for integration of AAR based on the refueling probe system requirements.
 Detail development of Structural parts as per the design criteria
 Generation of CAD models in Design in context to suit surrounding structure.
 Preliminary stress analysis based on the loads available
 Selection of material, Fastener type before entering Detail design phase.
 Generation of material requirement data required for procurement.
 Preparation of Layouts, Part and Assembly drawings.
 Preparation of BOM & PDR (Preliminary Design Review) documentation.
 Data management and stage wise release of products and drawings through PLM.
Project 2: Design of Structural components to accommodate LRU’S in STA#1 to STA#3 for
MK1 (NP5) Aircraft:
Team size: 4 Role: Team Member Duration: Jan 2015 to till date
Work description:-
 This structural arrangement incorporates Floors, Longerons, Stiffeners, Edge members, Splice plate,
spacers and LRU’s.
 Structure was designed to prevent Rain Water leakage on MMR Region.
 Generation of 3D models from rough sketches using NMG’S, in a Design-in-Context
Environment in a concurrent engineering mode in VPM.
 Generation of detail drawings for fabrication and other downstream activities.
 Creating & managing the data in VPM, Creation of PSN tree structure for sub assembly,
Assembly and parts with appropriate NMG’S.
 Radome lock Assembly for Tejas LCA.
 Design of monolithic composite parts for Access panels.
 Suitable selection of sealants, adhesive & shims for ease of assembly.
Project 3: Design of Structural components to accommodate AESA RADAR for
MK1 (LSP2 & LSP4) Aircraft:
Team size: 2 Role: Team Member Duration: Aug 2015 to till date
Work description:-

3.  This structural arrangement incorporates Floors, Longerons, Stiffeners, Edge members, Splice plate,
spacers and LRU’s.
 Generation of detail drawings for fabrication and other downstream activities.
 Detail development of Structural parts as per the design criteria
 Generation of CAD models in Design in context to suit surrounding structure.
 Preliminary stress analysis based on the loads available
 Selection of material, Fastener type before entering Detail design phase.
 Checking position and location of LRU’s 3D models with structure.
 Co-ordination with LRDE (DRDO) LRU’s team, stress, fatigue, weight control, material, dynamics
group before freezing the design.
OTHER TECHNICAL ACTIVITIES:
 Applying GD&T to achieve interchangeability and to reduce the assembly level problems.
 Feasibility studies to position LRU'S & AESA,MSR radar
 Design modifications on aircraft were made to close Request for Action (RFA).
Organization: ZENITH PRECITION PVT LTD.UNIT 2 (AEROSPACE DIVISION), Bangalore
Designation: Project Executive Engineer (Supply Chain Dept)
Period: 6 months (July 2013 – Jan 2014)
Project: Seating, Cargo.
Client: UTAS (UTC Aerospace) & GOODRICH, WIPRO, FDBA etc.
Work description:-
 Follow upping the seating project individually.
 Follow upping the all machining process & special process.
 Selection and procuring raw materials.
 Handling ppc & design aspects, SAP, customer, packing & dispatch.
 Checking & validation of parts as per the company standards (Quality).
PROFESSIONAL TRAINING PROGRAMS UNDERGONE:
 CatiaV5 R19 in CADD MAX SOLUTION RPC Layout Bangalore
 CatiaV5 R19, professional training by Dassault Systems.
 ENOVIA R19, professional training by TATA Technologies.
OTHER INFORMATION, WHICH I THINK, MAKES SUITABLE FOR THE JOB
 Hard working nature, Self learning, Commitment towards work and Flexible to any work conditions.
 Capable of doing the work as an individual as well as in a team.
 Innovative, Productive and Quick Learner
PERSONAL PROFILE:
Name : Darshan.K.R
Date of Birth : 02-May-1989
Sex : Male
Known Languages : Kannada & English
Nationality : Indian
Permanent address : S/o. Raveendra Kumar .D
Kalkere
Kodagihalli (P) Turuvekere (TQ) Tumkur(DIST)-572227 Karnataka, India.
REFERENCES
Mr. Neelakandan.S Mr. S.N Sreenivas Rao

4. Scientist / Engineer ‘E’, Airframe Scientist/Engineer‘G’,Group director
Aeronautical Development Agency Aeronautical Development Agency
Ph: +91-9900123411 Ph: 08025087361
E-mail: neelakandan@jetmail.ada.gov.in E-mail: snsrao@jetmail.ada.gov.in
DECLARATION:
I hereby declare that the above information is true to the best of my knowledge. Given an opportunity I
leave no stone unturned until I draw your best impression.
Place: Bangalore
Date: (DARSHAN K R)