A compressor mount bracket has a mount floor extending to be perpendicular to a square side extending away from the mount floor in a first direction. A closure side extends from the mount floor in the first direction. An outer surface faces away from the square side. An angled side extends at a non-parallel angle from the square side and back over the mount floor. A mount location extends from the angled side, and further over the mount floor. The closure side extends along the angled side and the mount location. The mount location has a first thickness, and the angled side has a second thickness. A ratio of the first thickness to the second thickness is between 1.38 and 1.63. A cabin air supply system and a method of servicing a cabin air supply system are also disclosed.


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    Titel :

    COMPRESSOR MOUNT BRACKET FOR AIRCRAFT CABIN AIR SUPPLY SYSTEM


    Beteiligte:
    MERRITT BRENT J (Autor:in) / PARENT CALVIN R (Autor:in) / PATEL ALPESH (Autor:in)

    Erscheinungsdatum :

    2016-11-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / F16M Rahmen, Gehäuse oder Grundplatten von Kraftmaschinen oder anderen Maschinen oder von Apparaten, nicht auf eine besondere Art von Maschine oder Apparat eingeschränkt, die anderweitig vorgesehen ist , FRAMES, CASINGS, OR BEDS, OF ENGINES OR OTHER MACHINES OR APPARATUS, NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUS PROVIDED FOR ELSEWHERE



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