The device of claim 3, wherein said first and second shafts further comprise.
该设备的索赔3，其中第一和第二轴进一步包括。
The device of claim 19, wherein said first, second and third axis are in a common plane.
该设备的索赔19 ，其中说，第一，第二和第三轴是在一个共同的飞机。
The device of claim 18, wherein said first, second and third sections of said stabilizer are a one-piece unit.
该设备的索赔18，其中说，第一，第二和第三部分说，稳定是一个单件单位。
The flap or slat drive system in the aircraft according to claim 24, wherein said first and second high-lift device groups are located on a same wing among said two wings.
皮瓣或金属板驱动系统在飞机按照要求24个，其中说，第一届和第二届高扬程设备集团设在同一间翼说，两个翅膀。
The device of claim 18, wherein said first, second and third shafts each have an internal bore sized to receive a corresponding one of said first, second and third sections of said stabilizer.
该设备的索赔18，其中说，第一，第二和第三轴都有一个内部口径大小获得相应的一个说，第一，第二和第三部分说的稳定作用。
The device of claim 18, wherein said first, second and third shafts each have an internal bore sized to receive a corresponding one of said first, second and third sections of said stabilizer.
该设备的索赔18，其中说，第一，第二和第三轴都有一个内部口径大小获得相应的一个说，第一，第二和第三部分说的稳定作用。
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