WING FLAP WITH TORQUE MEMBER AND METHOD FOR FORMING THEREOF

To provide an aircraft wing flap enabling improvement of cost, weight and structure complexity by including a torque member integrally formed with at least a portion of a flap body.SOLUTION: A torque member 108 of a wing flap 100 is integrally formed with a fuselage side end part 124 of a flap body...

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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
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Beschreibung
Zusammenfassung:To provide an aircraft wing flap enabling improvement of cost, weight and structure complexity by including a torque member integrally formed with at least a portion of a flap body.SOLUTION: A torque member 108 of a wing flap 100 is integrally formed with a fuselage side end part 124 of a flap body 164, and extends outwardly in the fuselage side direction from the fuselage side end part 124 of the flap body 164. The flap body 164 is actuated or moved between a lifting position and a lowering position by the torque member 108 extending through an opening 206 formed on a fuselage 202. The opening 206 is configured to enable the movement in the entire range during actuation of the torque member 108 and the associated flap body 164.SELECTED DRAWING: Figure 4 【課題】フラップ本体の少なくとも一部と一体に成形されたトルク部材を含むことで、コスト、重量、構造複雑さを改善した航空機翼フラップを提供する。【解決手段】翼フラップ100のトルク部材108がフラップ本体164の胴体側端部124と一体であり、フラップ本体164の胴体側端部124から外へ胴体側方向に延びる。フラップ本体164は、胴体202に形成された開口206を通って延びるトルク部材108によって、上げ位置と下げ位置との間で作動又は動かされる。開口206は、トルク部材108及び関連付けられたフラップ本体164の作動中の全範囲の動きを可能とするように構成されている。【選択図】図4