Dilip Kumar
Program Manager at Samniya Avionics Techsys Pvt.Ltd.- Claim this Profile
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English Professional working proficiency
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Kannada Native or bilingual proficiency
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Telugu Native or bilingual proficiency
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Tamil Full professional proficiency
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Hindi Professional working proficiency
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Malyalam Limited working proficiency
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French Elementary proficiency
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Bio
Experience
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Samniya Avionics Techsys Pvt.Ltd.
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India
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Aviation and Aerospace Component Manufacturing
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1 - 100 Employee
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Program Manager
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Apr 2023 - Present
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Electro Circuit Systems
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India
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Aviation and Aerospace Component Manufacturing
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1 - 100 Employee
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Professional Freelancer
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May 2022 - Apr 2023
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Aeronautical Development Establishment
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India
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Space Research and Technology
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1 - 100 Employee
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Senior Project Engineer
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May 2019 - May 2022
DESIGN & DEVELOPMENT • Involved in Design and development of Electro Mechanical Actuators, Servo controllers, load Test jigs & ATE of various UAV’s & Missiles.REPORT GENERATION • Visualising Actuator parameters using MATLAB and evaluating the performance of actuator. Generating Acceptance Test Record (ATR) for QA clearance of actuators.FIELD TRIALS• Supporting field trials of the various unmanned aircrafts & missile platforms at DRDO & Industry partners' test facilities. Fault finding in various operating scenarios and eliminating them at the product level & implementing design modifications for further improvements.• Post Flight Data Analysis of the actuators using Matlab and presenting the visualization data for the reviews. Generating review reports & technical memos of the analysis and actions carried out. Show less
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Project Engineer
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Jun 2016 - May 2019
TESTING• Bench Level testing of Electro mechanical & Hydraulic Actuators and ESS and EMI/EMC Testing as per the MIL standards like 461E, 704D, 810G, RTCA-DO-160F, etc. •Hardware In Loop Simulation (HILS)Testing :Cleared Actuators are carried to Hardware in Loop Simulation (HILS) facility to perform simulation using Flight Control Computer before integrating into aircraft.INTEGRATION • Integration of actuators on various UAV/Missile platforms.Neutral checks of the control surfaces ensured after integrating actuators on the airframe.Conducting post Integration performance tests which ensures all the actuators works properly when put together via 1553B communication system using FFC (Flight control computer). Show less
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