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@article{157626,
        author = {D.B. Jani and Shah Ashish and Singh Aditya and Singh Yash and Singh Bishambhar and Singh Nikhil and Singh Manmohan},
        title = {An overview on aircraft hydraulic system},
        journal = {International Journal of Innovative Research in Technology},
        year = {},
        volume = {6},
        number = {5},
        pages = {6-10},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=157626},
        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. },
        keywords = {Hydraulic fluid, Hydraulic system, Hydraulic reservoirs, Hydraulic pump, Hydraulic accumulators, Hydraulic actuators.},
        month = {},
        }