Environmental control systems of aircraft include a condenser, an expansion valve, an evaporator, and a compressor rotationally driven by a motor having integrated magnetic bearings, wherein a working fluid is passed through the condenser, the expansion valve, the evaporator, the compressor, and back to the condenser.


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    Title :

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM VAPOR CYCLE COMPRESSOR WITH MOTOR-INTEGRATED ACTIVE MAGNETIC BEARINGS


    Contributors:

    Publication date :

    2024-08-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16C SHAFTS , Wellen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM VAPOR CYCLE COMPRESSOR WITH MOTOR-INTEGRATED ACTIVE MAGNETIC BEARINGS

    GRATHWOHL NATHAN JAMES / KILCHYK VIKTOR | European Patent Office | 2024

    Free access

    Environmental factors affecting bearings for aircraft motor applications

    Johnson, H.B. | Engineering Index Backfile | 1958


    ENVIRONMENTAL FACTORS AFFECTING BEARINGS FOR AIRCRAFT MOTOR APPLICATIONS

    JOHNSON, HOWARD. B. | SAE Technical Papers | 1958


    Centrifuge Test of an Aircraft Vapor Cycle Environmental Control System

    Maxwell, Gerald C. / Martinez, Mayra I. / Dexter, Peter F. et al. | SAE Technical Papers | 1992


    INTEGRATED AUXILIARY POWER UNIT, STARTER-GENERATOR-MOTOR, AND VAPOR CYCLE COOLING SYSTEM FOR AN AIRCRAFT

    BEUNING CHARLES / EBERSOLE NATHAN ROY / GALLMAN JOHN W et al. | European Patent Office | 2016

    Free access