An aircraft fuselage comprises a support structure, a first interior module having a first support arm, a second interior module having a second support arm, and a support system for suspending the first and second interior modules from the support structure. The support system includes a shared fitting for releasably attaching to the first and second support arms of the first and second interior modules. The shared fitting is configured to react a first rotational force when the first support arm is attached and the second support arm is released. The shared fitting is configured to react a second rotational force when the second support arm is attached and the first support arm is released.
Aircraft interior module support system including shared fittings
2018-03-20
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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