WING FLAP WITH TORQUE MEMBER AND METHOD FOR FORMING THE SAME

WING FLAP WITH TORQUE MEMBER AND METHOD FOR FORMING THE SAME

To provide a wing flap of an aircraft improved in the cost, weight and complexity.SOLUTION: A wing flap 100 includes a flap body. The flap body includes an upper skin 102, a lower skin 104 opposite the upper skin 102, and a plurality of spars 106 that extend between the upper skin 102 and the lower...

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Bibliographische Detailangaben
Hauptverfasser: JAN A KORDEL, WENDELL C K CHOY, MICHAEL A BALZER, GREGORY M SANTINI, JACOB D VIRNIG, MARK M BLEAZARD
Format: Patent
Sprache:eng ; jpn
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:To provide a wing flap of an aircraft improved in the cost, weight and complexity.SOLUTION: A wing flap 100 includes a flap body. The flap body includes an upper skin 102, a lower skin 104 opposite the upper skin 102, and a plurality of spars 106 that extend between the upper skin 102 and the lower skin 104. The wing flap 100 also includes a torque member 108 that is coupled to the flap body. In one example, the torque member 108 is contiguous with at least one of the upper skin 102 and the lower skin 104.SELECTED DRAWING: Figure 3 【課題】コスト、重量、及び複雑さにおいて優位な航空機の翼フラップを提供する。【解決手段】翼フラップ１００はフラップ本体を含む。フラップ本体は、上方外板１０２、上方外板１０２に対向する下方外板１０４、及び、上方外板１０２と下方外板１０４との間で延びる複数の桁１０６を含む。翼フラップ１００は、フラップ本体に連結されたトルク部材１０８も含む。一例では、トルク部材１０８が、上方外板１０２及び下方外板１０４のうちの少なくとも一方に連続している。【選択図】図３