A method for providing electrical power and cooling for an aircraft includes: connecting a starter generator to an energy accumulator bus; selectively connecting the energy accumulator bus to a first power distribution unit in a first power channel or a second power distribution unit in a second power channel; wherein the starter generator is coupled to a shaft in an integrated power and cooling unit that includes a cooling turbine coupled to the shaft; a compressor coupled to the shaft and including an input for receiving engine bleed air or ambient air and an output for discharging compressed air; a flywheel coupled to the shaft; and a power turbine coupled to the shaft; and using energy stored in the flywheel to rotate the shaft enabling the starter generator to supply electrical power to the energy accumulator bus.


    Access

    Download


    Export, share and cite



    Title :

    APPARATUS FOR AIRCRAFT WITH HIGH PEAK POWER EQUIPMENT


    Contributors:

    Publication date :

    2016-08-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Apparatus for aircraft with high peak power equipment

    HO YUHANG / KNOWLES JEFFREY A | European Patent Office | 2016

    Free access

    Improving Peak Power Capability of an Aircraft

    Sarlioglu, Bulent / Ganev, Evgeni D. | SAE Technical Papers | 2010


    Conceptual Design and Weight Optimization of Aircraft Power Systems with High-Peak Pulsed Power Loads

    Devarajan, Balakrishnan / Boroyevich, Dushan / Raj, Pradeep et al. | SAE Technical Papers | 2016


    Conceptual Design and Weight Optimization of Aircraft Power Systems with High-Peak Pulsed Power Loads

    Li, Qian / Devarajan, Balakrishnan / Zhang, Xuning et al. | British Library Conference Proceedings | 2016


    Equipment power supply system of aircraft and aircraft

    HU HUAZHI / XIE HUIPENG / LIU YONG et al. | European Patent Office | 2022

    Free access