Aircraft receptacle

A system and method for an aircraft refueling receptacle. The aircraft refueling receptacle comprises a pedestal, a flanged structure, a sliding valve, and a bolt. The flanged structure has a first ledge, a second ledge, and a number of flanges extending inwardly. The pedestal contacts the first led...

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Bibliographische Detailangaben
Hauptverfasser:	Nguyen, Ky Huu, Byrne, Dennis P, Weber, Paul Gerard, Klenke, Paul William, Lewis, Brian
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A system and method for an aircraft refueling receptacle. The aircraft refueling receptacle comprises a pedestal, a flanged structure, a sliding valve, and a bolt. The flanged structure has a first ledge, a second ledge, and a number of flanges extending inwardly. The pedestal contacts the first ledge. The sliding valve has a first face that contacts the second ledge of the flanged structure during refueling. The bolt extends a part of a length of the pedestal and is connected to a receiver within the pedestal.