1. PRAVEENKUMAR.K.HIREMATH
: C/o. #29/5, Poojappa Building,
4th
main, Govindrajanagar,Vijayanagar
Bangalore-560040, Karnataka
: +91- 9916077556(M), +91-80-66931466(O);
: praveenkumar.k.hiremath@gmail.com
To enhance and utilize my innovative ideas, skills & abilities in the field of specialization,
to grow and contribute materially to my company, team and self ; seeking challenging
assignments preferably in Research & Development plot form.
 Total 5 years of experience in CATIA V5 R19 and VPM-ENOVIA and PDM tool.
 Over 2 year experience in Airbus working environment for A350XWB project.
 VPM, PDM frequently used in Airbus environment.
 B.E (Mechanical Engineering) from SBMJCE Bangalore, VTU Belgaum.
Job profile:
 Generation of 3D CAD models from 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 down stream activities.
 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.
 Co-ordination with Design group and System group before freezing the design.
 Generating & managing Project Slips, Change notice & Higher issue drawings through VPM.
 Generation of material schedule, stock size, drawing attributes, MS sheet attributes, drawing
sheet attributes through VPM.
 Generation of CGR assembly from VPM data for other design studies.
 DFMA was carried out to remove the existing problems of manufacturing and assembly, in
close coordination with manufacturing and assembly shop.
 Design Tool : CATIA V5 R19
 PLM/PDM Tool : VPM-ENOVIA 1.6, Team centre, WindChill
 Operating System : Windows, UNIX .
Technical Software Skills

2. Present Company:
Geometric Limited, Bangalore.
Design Engineer
June 2014 to Till Date
Project Carried:
1) Airbus A350 XWB 900RR and 1000RR project
Project Title : AIRBUS PROJECT (A350XWB 900RR and 1000RR)
Client : Aerolia, Airbus
Software : CatiaV5, Enovia, Prime and WindChill
Role : Team member
Description : The scope of the project was to build manufacturing drawings maintaining
stringent quality checks as per Airbus standards. Creation of Manufacturing and Installation
Drawings to be used in Aircraft.
• Creation of manufacturing drawings for tubes
• Creation of installation drawings for tubes
• Creation of bracket manufacturing drawings.
Responsibilities :
As the delivery was every alternate day role was to do regular QC and over view on all the
drawings before sending the data to ensure Airbus quality standards, to meet customer
satisfaction index, Ensuring the Project success and employee satisfaction through optimum and
effective utilization of all available documents so as to contribute to the Division’s objectives.
Previous Company:
Aeronautical Development Agency (ADA), Bangalore.
Engineer ‘A’- Airframe Directorate – Detail Design Group
July 2011 to June 2014
Project Carried:
1) Structural feasibility study on Fixed Aerial Refueling Probe for LCA Mk1.
Description: This structural arrangement starts from the Station 1 to Station 3. It incorporates
Floors, Longerons, Stiffeners, Edge members, Splice plate and LRU’s. The main function of
this assembly is to provide the structural support to Probe and Mast connected to the Interface
Bracket. The entire Station 1 to Station 3 MMR assembly was integrated with a/c structure
assembly
2) Preliminary structural 3d layout of Sta# 1 to Sta# 3 LCA Mk2.
Description: This structural arrangement starts from the Station 1 to Station 3. It incorporates
Floors, Longerons, Stiffeners, Edge members, Splice plate and LRU’s. The main function of
this assembly is to provide the structural support to LRU’s function and Radar and its
associated LRU’s. This assembly attached to the Bulkhead at Station 1 to Station 3 through
the splice plate and spacers.
3) Preliminary structural 3d layout of ENDCONE(Sta# 37 to END) for LCA Mk2.

3. Description: This structural arrangement extends from the end of the rear fuselage to
outer tip of the aircraft. The main function of this assembly is to provide a structural
support at end station in the form of bulkhead, and also this assembly carries the turkey
feather, which creates the partial pressure in engine bay region, enabling engine bay
cooling at lower altitude and at lower mach no.
This region is also where the engine exhausts the hot gases. This assembly consists of
a bulk head , turkey feather and support structure like longeron , stringers and angles .
 Rain Water protection scheme on MMR Region.
 Repair scheme on turkey feather at Bottom End cone Region.
 Radome lock Assembly for LSP of LCA Mk1 to close RFA .
 Conceptual study on locating Beta Vane and Ram Antenna in MMR Region for Mk2.
 Feasibility study of Fixed Aerial Refueling Probe for LCA Mk1.
.
Date of Birth : 1st
June 1988
Languages : English, Hindi and Kannada
Blood group : O +ve
Address : S/o. Kallayya.K.Hiremath
At post: Karamudi
Tq: Yelburga
Dist: Koppal
PIN-583236
Passport : Z2464425
DECLARATION
I hereby declare that the information given above is true to the best of my knowledge.
Date: Sd/-
Place: Bangalore (Praveenkumar.K.Hiremath)
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