An overview on aircraft hydraulic system

D.B. Jani; Shah Ashish; Singh Aditya; Singh Yash; Singh Bishambhar; Singh Nikhil; Singh Manmohan

An overview on aircraft hydraulic system

Authors: D.B. Jani, Shah Ashish, Singh Aditya, Singh Yash, Singh Bishambhar, Singh Nikhil, Singh Manmohan

Unique Paper ID: 157626
Volume: 6
Issue: 5
PageNo: 6-10

Keywords: Hydraulic fluid Hydraulic system Hydraulic reservoirs Hydraulic pump Hydraulic accumulators Hydraulic actuators.

Abstract:
Hydraulic systems in aircraft provide a means for the operation of aircraft components. The operation of landing gear, flaps, flight control surfaces, and brakes is largely accomplished with hydraulic power systems. Hydraulic system complexity varies from small aircraft that require fluid only for manual operation of the wheel brakes to large transport aircraft where the systems are large and complex. To achieve the necessary redundancy and reliability, the system may consist of several subsystems. Each subsystem has a power generating device (pump) reservoir, accumulator, heat exchanger, filtering system, etc. System operating pressure may vary from a couple hundred pounds per square inch (psi) in small aircraft and rotorcraft to 5,000 psi in large transports.

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Cite This Article

ISSN: 2349-6002
Volume: 6
Issue: 5
PageNo: 6-10

An overview on aircraft hydraulic system

Available:https://ijirt.org/Article?manuscript=157626

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Journal no 47859

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