Design Engineer with focus on Design and development of fighter aircraft LRUs (Actuators and Pump)and special-purpose custom test rigs for performance and Qualification testing
Experience:
- 3 years Experience in Design of test rigs for aircraft line replacement units(LRU)
- 3 years Experience in design of aircraft LRUS( actuators and pump)
Skills
- Solidworks
- Ansys
- Hypermesh
- KISSSOFT
- MATLAB
- AutoCAD
Others
- Trained Internal auditor for ISO/IEC 17025:2017
B.E (Mechanical Engineering)
- Design and development of test rigs (mechanical and Hydraulics)
- Design of aircraft LRUs’ with focus on linear actuators, rotary actuators (with compound planetary stages for limited envelope high reduction requirements) and engine driven pump.
- Design and development of assembly and disassembly fixturing for special purpose toolings
- Development of parallel kinematics machine
- Qualification testing of Leading-edge slat actuators
- Design and development of 30 lpm axial piston pump – airworthy
- Design and development of Geared rotary actuator for fighter aircrafts
- Development of Flight control system actuator test rig as a part of the development of Hyd. Second-line test rig for HAL
- Quality manager for accreditation of Aerospace lab activities to ISO/IEC : 17025: 2017
- Technical Evaluation and Procurement of Electron beam welding machine
- Article “Electron beam welding of oxide dispersion strengthened 9 Cr martensitic steel-an experimental and theoretical perspective “ in Materials today: proceedings 22:2509-2519 · January 2020
- Part of the team for successful qualification testing of Leading Edge Slat Actuators (LESA) for airworthiness which also recently completed successful flight trials at supersonic speeds
- Completed Preliminary Design Review of Geared rotary actuator engineering model which is an essential demonstrator for Leading-edge vortex control and weapon bay door applications for carrier take-off fighter aircraft (Naval versions).
- Completed Preliminary design review (PDR) for Design of FCS test rig as a part of Hyd. Second-line test rig development for HAL.
- Part of the team to assemble and run prototype I of axial piston pump 30 LPM which is a secondary pump for aircraft hyd. System.
- Part of the team for calibration activities on Parallel kinematics machine, which was also exhibited during IMTEX 2015, BIEC, Bengaluru