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 19, wherein said first, second and third axis are in a common plane.
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.
这中间支撑结构进行了期刊和沿垂直于第一和第二，第三轴轴承对轴取向。
This intermediate support structure carries a pair of journals and bearings oriented along a third axis perpendicular to each of the first and second axes.
通过第三热压配合部（10）能够将比通过第一热压配合部（8）更大的转矩和比通过第二热压配合部（9）更小的转矩从齿轮（4）传递到轴（2）上。
The third shrink fit (10) allows greater torques to be transmitted from the gear (4) to the shaft (2) than the first shrink fit (8) and smaller torques than the second shrink fit (9).
通过第三热压配合部（10）能够将比通过第一热压配合部（8）更大的转矩和比通过第二热压配合部（9）更小的转矩从齿轮（4）传递到轴（2）上。
The third shrink fit (10) allows greater torques to be transmitted from the gear (4) to the shaft (2) than the first shrink fit (8) and smaller torques than the second shrink fit (9).
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