Fuel System-Pressure Transducer for Aircraft Applications

Project Description
  • The pressure transducer is used to measure the system pressure during fuel tank pressurization, fuel transfer and refueling functions. 
  • The pressure transducer shall be of compact size capable of meeting the requirements. 
  • A MEMS based transducer is desirable. The operating pressure range is           0 - 110 psia for absolute Pressure transducer and 0 - 150 psig for gauge pressure transducer. 
  • Transducer shall be designed to have maximum accuracy and output shall linearly proportional to the pressure. 
  • The working media for pressure transducer is Air, Nitrogen, Jet A1 fuel and mixture of air & fuel vapor. 
  • This unit shall also be compactable with Bio fuel confirming to IS71081-2019, Aviation Turbine fuel containing synthesized hydrocarbons.



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Project Awarded To

Chakradhara Aerospace and Cargo Pvt Ltd

Company Profile :
Design and development of products, sub-assemblies & components such as Pressure Sensors, Accelerometer, Electro-Mechanical Actuators, Torque Motors, Solenoids, Valves & Control System Sub-Assemblies for Aerospace & Defence applications. Manufacture of Precision Components for Aero Engine – domestic & international customers