A compressor cross bracket for use in an air supply system for an aircraft comprises a ledge extending away from a main body. The main body has ends at opposed sides and a ditch defined between the ends. Each of the ends have at least one bolt hole which has a diameter. A thickness of the ledge is defined in a direction from which the main body extends from the ledge, with a ratio of the thickness to the diameter being between 0.636 and 0.680. A cabin air supply system and a method of servicing a cabin air supply system are also disclosed.
CROSS BRACKET FOR AIRCRAFT CABIN AIR SUPPLY SYSTEM
2016-11-10
Patent
Electronic Resource
English
IPC: | 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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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