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Mr. Vijet Bhandiwad

Designation: Scientist - D
Centre: Centre for Additive and Special Manufacturing Processes (C-ASMP)
Group: Aerospace Test Rigs & Calibration Group
Joining Date: 14-11-2012
Email Id: vijet[at]cmti[dot]res[dot]in
Office Telephone No: 080-22188363
Mobile No: +91-9035938583

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