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CV: Electrical Integration Engineer
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Date Submitted: Last Modified: Current job: Employment Term: Job location: Date available: Industry: Keywords|
PROFESSIONAL SUMMARY: |
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Q Work Experience |
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§ Total Experience |
3.4 Years |
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§ Aerospace Experience |
4 Months(Till date) |
Model Based Definition (MBD) for Aircraft fuselage. |
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§ Space Experience |
2 Years |
Spacecraft Assembly,Integration & Testing(AIT)& Electrical Harness design. |
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§ Design Experience |
1 Year |
Designing the material for BHEL by 2D AutoCAD |
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Q Experience |
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Organization |
Project |
Activity |
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§ Unit Force Technologies (July 2012-Till date)
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INFOSYS Technologies limited.
Mitsubishi Regional Jet(Mitsubishi Aircraft Corporation)
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· Concept of design criteria. · Model Based Definition (MBD) activities for frames,Stringers,Splice for fuselage. · Creating Reference Documents for the Evidence reports. · Model Based Definition activities. |
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§ KELTRON (A Govt Undertaking) (June 2010 - Feb 2012) |
Indian Space Research Organisation, ISRO Satellite Centre. Bangalore
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· AIT, Assembly Integration and Testing sequence procedure and documentationfor Scientific Remote Sensing Satellites. · Expert in Harness designing system by using HARNESS DEVELOPMENT SOFTWARE (HDS) & Expert in Routing by using CATIA V5 Electrical Harness Design. · Validating the harness tests, manufacturing. · Design and realization of Electrical Distribution System (EDS). · Clean Room Functional and Integration test (FIT) for all subsystem. |
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§ Classic Industries (June 2009-May 2010)
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§ Bharat Heavy Electricals limited (BHEL) |
· Designing the job material as per BHEL requirement by using 2D - AUTOCAD. · Quality checks done as per QA documents. · Fabricating and testing the manufactured job materials.
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Q Tool Experience |
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§ CATIA V5 |
2 Years |
Electrical Harness Design |
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§ CATIA V5 |
4 Months |
Functional Tolerance and Annotation (FTA) |
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Q Educational Qualification |
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Degree |
Branch / Discipline |
Institute, University |
% &Year |
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Bachelor of Engineering (BE) |
Electrical and Electronics Engineering |
K.S.Rangasamy College of Technology, Anna University-Chennai |
75.13 & 2009 First Class distinction |
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Higher Secondary |
State Board, Tamilnadu |
Bishop Heber Higher Secondary School |
71.83% & First Class /2005 |
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S.S.L.C |
State Board, Tamilnadu |
K.A.P.V Higher Secondary School |
81.6% & First Class /2003 |
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Q Trainings |
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§ CATIA V5 (Electrical) |
20 Days |
EDS Technologies(Certified Education Partner to Dassault Systemes, France) |
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§ CATIAV5 |
30 Days |
Infosys (Internal Training)
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§ AUTOCAD |
30 Days |
Practical Technologies, AUTODESK Certified
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DETAILED PROJECTS SUMMARY
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Project #1 |
PSLV C-16 |
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Spacecraft |
YOUTHSAT(Indo –Russian Mission) |
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Customer |
ISRO Satellite Centre |
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Duration |
Jun 2010 to April 2011 (11 Months) |
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Tool /s |
CATIA V5 |
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Work Location |
Indian Space Research Organisation, Bangalore |
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Role |
Integration Engineer |
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Description |
A cooperative joint scientific mission between India and Russia (Moscow University).The micro satellite bus is planned and designed to carry different kinds of payloads like earth imaging, atmospheric applications, weather monitoring, stellar observations, scientific experiments etc. |
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Responsibilities
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Harness Design, Fabrication, Testing and Routing: · Generation of Electrical Integration requirements such as Harness path, inserts, cutouts etc., as per EMI/EMC aspects. · Good knowledge of CATIA V5 Electrical Harness Discipline. · Expert in Harness designing system by using HARNESS DEVELOPMENT SOFTWARE (HDS). · Responsible for Data base management, which includes Harness design, Compilation of data cards and matching, patch allocation, generation of worksheets as per subsystem requirements. · Electrical Interface Definition includes functional description, signal characteristics, originating connectors details, destination connectors details, types of wire used etc. responsible for matching of source to destination subsystem by using PC based software. · Involved in Electromagnetic compatibility (EMC) design and Electro-Static Discharge (ESD). · Development of a database for satellite and definitions for electrical wiring.
· Designed Mil-std-1553B-Busharness layout to minimize Bus breaks tested and installed.
CLEANROOM Level Assembly Integration and testing(AIT):
Dis-assembled Integrated Satellite Testing During this phase all subassemblies are interconnected using test cables. · Umbilical Checks, Interconnection Checks · Isolation Checks, Functional Checks · Tele command Checks, Telemetry Checks · Electrical ground support equipment(EGSE) · Panel Closure Activity Assembled Integrated Satellite Testing (IST)
· Solar panel deployment Test, Illumination Test · Antenna Deployment Test · Thermo vacuum Test, Vibration Test
· Supported in testing of Youthsat spacecraft with PSLV C-16 in Shriharikota |
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Project #2 |
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Spacecraft |
SARAL (Indo –France CNES Mission) |
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Customer |
ISRO Satellite Centre |
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Duration |
Dec 2011 to Feb 2012 ( 15 Months) |
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Tool /s |
CATIA V5 |
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Work Location |
Indian Space Research Organisation, Bangalore |
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Role
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Integration Engineer |
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Description |
SARAL is a joint scientific mission between India and France (CNES). The first mission with these payloads is called 'SARAL' (Satellite for ARGOS and ALTIKA Payloads) mission.
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Responsibilities |
· Harness designing system by using HARNESS DEVELOPMENT SOFTWARE (HDS).Responsible for Data base management. · Development of a database for satellite and definitions for electrical wiring.
· Finalizing the harness routing and anchoring point for the spacecraft based on the electrical interfaces of all subsystems.
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Project #3 |
Fuselage Designing for Aircraft |
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Aircraft |
Mitsubishi Regional Jet 70-90 seating |
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Customer |
Mitsubishi Aircraft Corporation (MAC),Japan |
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Duration |
July 2012 to Till date (4 Months) |
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Tool /s |
CATIA V5 |
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Work Location |
Infosys Technologies Limited |
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Role |
Design Engineer, Aircraft fuselage |
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Description |
The Mitsubishi Regional Jet (MRJ) is a passenger jet aircraft seating 70–90 passengers manufactured by Mitsubishi. The airliner has been produced in three Fuselage lengths. The Fuselage is a pressurized Semi-Monocoque structure formed from circumferential frames, longitudinal stringers and skin. |
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Responsibilities |
· Involved in MBD (Model Based Definition) activity of Frames (Both Sheet metal, Machined Frames), Stringers, Stringer clips, Stringer splice. · Creating Reference documents, Capture documentand Evidence reports. · Creating MBD models for the parts at DDM, IDM & ADM Stages. · Model based definition (MBD) creation using FTA (GD&T) module for different aircraft components · Installation Definition Model, creation using shape design & FTA in CATIA V5 |
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Personal Details |
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Date of Birth |
December -02- 1987 |
Conclusion
If I am given an opportunity to tackle odd assignment, with my updated Technical knowledge and with my good coordinating and cordial relationship, I will complete the assignment before the time span stipulated.
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