A propeller blade arrangement comprising a propeller blade attached to and rotatable with a hub, via a retention bearing, the blade being rotatable about a center line of the blade, the retention bearing configured to tilt the blade such that its center line is tilted with respect to the hub.
一种螺旋桨桨叶布置,包括螺旋桨桨叶,所述螺旋桨桨叶经由保持轴承附接到桨毂并且能够随所述桨毂旋转,所述桨叶能够围绕所述桨叶的中心线旋转,所述保持轴承被配置为使所述桨叶倾斜,使得所述桨叶的中心线相对于所述桨毂倾斜。
PROPELLER BLADE ARRANGEMENT
螺旋桨桨叶布置
2021-10-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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