- Chicago IL, US Jeffrey Allen Cartwright - Arlington WA, US Adam Arthur Logue - Everett WA, US Robert B. Fowler - Everett WA, US
International Classification:
B64F 5/10
Abstract:
An assembly to connect a panel to a support member. The assembly may include a saddle fitting configured to connect to the support member and including first and second plates. A back fitting may be positioned between the second plate of the saddle fitting and a second face of the panel. An index fitting includes a flange that may be positioned between the first plate of the saddle fitting and a first face of the panel, and a boss that extends outward from the flange and through the opening in the panel. The index fitting is wider than the panel and sized to fit within the gap of the saddle fitting with a first end of the index fitting contacting against the first plate and a second end of the index fitting contacting against the second plate. One or more fasteners may connect the saddle fitting to the index fitting.
Ceiling Retaining Assemblies And Methods For An Internal Cabin Of A Vehicle
- Chicago IL, US Bryan Charles Bundy - Mukilteo WA, US Jeffrey Allen Cartwright - Arlington WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B64D 11/00
Abstract:
A retaining assembly and method for use within an internal cabin of an aircraft, in which the retaining assembly includes a hinge including a biasing member. The hinge is moveable between a retaining position, in which the biasing member is configured to exert a biasing force into a top surface of a ceiling panel within an internal cabin of a vehicle to prevent the ceiling panel from upward motion, and a release position, in which the hinge is configured to be pivoted away from the ceiling panel and the biasing member is configured to be separated from the ceiling panel.
Aircraft Interior Module Support System Including Shared Fittings
- Chicago IL, US Jeffrey A. Cartwright - Arlington WA, US Mark J. Nadvornick - Lynnwood WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B64D 11/00 B64C 1/06
Abstract:
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.
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