WING FLAP WITH TORQUE MEMBER AND METHOD FOR FORMING THEREOF

A wing flap includes a flap body. The flap body includes an upper skin, a lower skin opposite the upper skin, and a plurality of spars that extend between the upper skin and the lower skin. The wing flap also includes a torque member that is coupled to the flap body. A portion of the torque member i...

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Bibliographische Detailangaben
Hauptverfasser:	BLEAZARD, MARK M, KORDEL, JAN A, SANTINI, GREGORY M, CHOY, WENDELL C. K, BALZER, MICHAEL A, VIRNIG, JACOB D
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A wing flap includes a flap body. The flap body includes an upper skin, a lower skin opposite the upper skin, and a plurality of spars that extend between the upper skin and the lower skin. The wing flap also includes a torque member that is coupled to the flap body. A portion of the torque member is contiguous with at least one of the upper skin and the lower skin. Un volet daile comprend un corps de volet. Le corps de volet comprend un revêtement supérieur, un revêtement inférieur opposé au revêtement supérieur et plusieurs longerons sétendant entre les deux revêtements. Le volet daile comprend également un élément de couple raccordé au corps de volet. Une partie de lélément de couple est contiguë à au moins le revêtement supérieur ou le revêtement inférieur.