Engineer Project

CURRICULUM VITAE

D.GOPI

#*/*, ***** ******,

Email : abogxq@r.postjobfree.com

2nd floor, 8th cross,

Contact no : 973-***-****

Maruthi Nagar, Madiwala,

Bangalore

OBJECTIVE:

Intend to build a career with committed & dedicated people,

exploring my potential to serve the organization and willing to work as a

key player in challenging & creative environment.

ACADEMIC PROFILE:

. Completed B.E. (2006) in Mechanical Engineering from A.V. Institute of

Technology,

affiliated to Anna University Chennai, with an aggregate of 77%

with Distinction.

. Completed H.S.C (2002) from Muthialpet Higher Sec School Chennai, with

79.5%.

. Completed S.S.L.C (2000) from Muthialpet Higher Sec School Chennai,

with 84.2%.

PROFESSIONAL EXPERIENCE: 5+ yrs of experience in Aerospace Industry.

EXPERIENCE Summary:

. Working for Textron India Private Ltd., Bangalore in Cessna Business

Unit, since Mar 2010 as a Sr.Engineer-Design.

. Worked for BAeHAL Software Ltd., Bangalore.

- Deputed to work in the Department of Mechanical Installation

Design (Electrical & Avionics Group) Aircraft Research and

Design Centre, Hindustan Aeronautics Limited Bangalore. from Nov

2007 to Mar 2010 as a Software Engineer.

SOFTWARE SKILLS:

. CAD Packages : CATIA V5 R20, AUTOCAD 2000.

. PDM Package : Enovia VPM 1.5 & 3D-COM

. Operating Systems : Windows 98/2000/XP & UNIX.

. Other Package : MS-Office.

NATURE OF WORK DONE IN HAL-ARDC:

. Involved in Designing, Modeling & Detailing of Mechanical Installation

Equipment of EL & AV Group for Light Combat Aircraft (LCA) using CATIA

V5/Enovia.

. Build the Product Structure for Installation and creating work flow

for the release of drawings Using Enovia VPM 1.5.

. Involved in documentation for finalization of Cockpit layouts for

various aircrafts with Pilot's concurrence and interaction with Pilots

to resolve their issues.

. Creation of Layout drawings, Bill of material (BOM) and Project Slips

(PS).

. Coordinating & supervising the activities, concerned with the

Manufacture, Inspection & Testing of the designed components.

PROJECTS:

Project #1

Title : Cockpit installation for Prototype Vehicle

-LCA Fighter & Trainer A/C.

Environment : CATIA V5 R20, ENOVIA VPM.1.6

Description:

Involved in the Design of LH, RH &

Centre Console, Main Instrument Panel, LH & RH Quarter Panel, Coaming &

Glare shield, Helmet Mounting Display Systems will be installed in the

Cockpit based on D.E.P and N.S.R.P as per MIL-STD and with the help of

Pilot. All Controlling systems come in Consoles and all Display systems in

Main Instrument Panel (MIP). All LRU's like HUD, MFD's, SSDU, FSP, CWP, TQA

and Switches will be installed in Cockpit after the Pilot's approval. So

Design of Top Panels, Support Brackets, Side Cover, Tube assembly & Angles

for installation of LRU's and instruments in Cockpit for Fighter and

Trainer variants.

Roles and Responsibilities

< Checking against D.E.P & N.S.R.P.

< Clash analysis of the installation w.r.t other group.

< Drafting of Parts, Assemblies, Installation and

generation of Material

schedule for the Assemblies & Installation.

Project#2

Title : Installation of Avionics Systems

LRU's. - LCA Fighter & Trainer A/C.

Environment : CATIA V5, ENOVIA VPM.

Description:

In this project we deal with

installation of the Electrical & Avionics equipments, Antenna like RAM

Antenna, & TACAN Antenna and LRU's like SSCDR, AMU JUNCTION BOX, APSU,

RADIO ALTIMETER, TRU, TERMINAL BLOCK & VARISTOR etc. Here main Design

constraint is accessibility of the units and unit should not foul with

other routings like Hydraulics and Environmental control system.

Roles and Responsibilities

< Position of the LRU & Antenna as per inboard drawings.

< Involved in modeling of LRU & its mountings. Design of

Support Brackets

For fixing LRU to the Structure.

< Coordination with Structure and Aerodynamics Group for

clearance.

NATURE OF WORK IN CESSNA

. Working in Engineering Change Request (ECR), Quality Notification (QN)

and Drawing Change Notice (DCN) for supporting Sustaining Activities.

. Creating, modifying 3D Models & drawings in CATIA V5 and 3D COM based

on the input.

. Generating Bill of Materials and Release Sheets.

. Providing Technical Support on CATIA V5, 3D COM & Cessna Standards for

team members.

. Provide leadership support to the team to meet execution metrics and

quality standards on complex / critical projects.

. Coordinating with other groups like Stress, Fatigue and Material for

the approval of design changes.

PROJECTS:

. Re-Design of Wing- Spar Assembly for Cessna Mustang Citation Jet:

It is a Cost out Project, so Fwd, Main & Rear Spar, Rib Caps, Rib

Web, Flap Interconnect brackets, Wheel well structure, Speed Brake

assy, Upper and lower skin are re-designed in such a way that to

reduce the machining cost of the parts.

. Sealant Improvement for Cessna Mustang Citation Jet: It is like to

reduce cure time instead of applying the sealant, worked on Cabin

Window, Baggage Door, Radome and Nose Cone Structural Assy, so as to

change the application of the sealant and Discussed with Material and

processing Group for approval.

. Cable Guard Pin Improvement: It is also a Cost out Project,

Current cable guard pin material is too costly and so we decided to

go with different material, so as to reduce cost of the pin. For

this we coordinated with Material and processing Group for

approval.

. Mustang Cable Guard Change: Due to tension applied in yoke, cable is

rubbing in lightening Hole location, so designed a Bracket and Cable

Guard to prevent rubbing condition.

. Blower Clamp Change: To avoid hand forming of clamp in assembly line.

Provided thickened rubber between Blower and clamp so as to reduce man

hour.

. Fastener Substitutions: Due to inaccessibility of some mechanical

fasteners and Rivets in various areas of the aircraft, provided

alternate fasteners/solutions.

. New Avionics Equipment: For GARMIN support, installing DATA COMM and

IRIDIUM

Equipment behind the Aft Baggage compartment. So designed frames and C-

Channel to install the equipments and discussing with Stress and

Fatigue for approval.

. Hydraulic Tubing Corrosion Improvements (510): Cause corrosion issue

due to dissimilar material contact in hydraulic tubing's, areas like

nose, MLG, NLG, wing and cabin fairings etc.

TRAINING UNDERGONE:

. Completed 3D COM & Enovia VPM 1.6 training in Cessna Aircraft Company,

Kansas, US.,

. Completed CATIA V5 Aerospace Sheet Metal training in Cessna Aircraft

Company, KS, US.,

. Completed CATIA V5 Generative Sheet Metal training in Cessna Aircraft

Company, KS, US.,

. Attended Metallic Materials and Finish class, Metal Bond class &

overview in Cessna.

PERSONAL DETAILS:

Father's name : A.N.DURAISAMY

Passport no : G2737260 (Valid Up to 2017)

Nationality : INDIAN

Permanent address : No: 100, Mahalakshmi Nagar,

Vellappan Chavadi,

Chennai-600077.

Languages Known : Tamil, English & Kannada

DECLARATION:

I hereby declare that the information furnished above is true to the

best of my knowledge.

Date

Place: BANGALORE

(D.GOPI)

Contact this candidate