| 摘要 |
A propeller (70) for an aircraft (20) having a fuselage (22) and a pair of fixed wings (50a, 50b) includes a mounting member (76) secured to at least one wing. At least one blade (72) is rotatably connected to each mounting member (76) and has an airfoil shape. The at least one blade (72) is in a locked condition during take-off and landing of the aircraft (20) extending parallel to a leading edge of the wing and in an unlocked, rotating condition during flight for propelling the aircraft (20). |
