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Composite spar structure having integral fitting for rotational hub mounting

机译:具有用于旋转轮毂安装的整体配件的复合翼梁结构

摘要

Hollow filament wound spar structure is provided adapted for rotational hub mounting under centrifugal and bending loads. The structure comprises an integrally wound, filament and resin composite spar of a predetermined wall thickness, a fitting integrally wound therein, the fitting defining rotational hub fastening means and comprising a plug having a mechanical engagement groove circumferentially of its longitudinal axis into which the opposing spar wall portion is deflected responsive to winding fabrication of the spar wall on the fitting. Belt means additionally are provided opposite the groove locally peripherally confining the deflected spar wall portion in mechanical engagement reinforcing relation, against relative dislodgement of the spar wall portion from the plug groove in the mounted condition of the spar structure, under centrifugal and bending loads.
机译:提供了空心丝缠绕的翼梁结构,该结构适于在离心和弯曲载荷下安装旋转毂。该结构包括整体缠绕的,具有预定壁厚的长丝和树脂复合翼梁,一体地缠绕在其中的配件,该配件限定了旋转毂固定装置,并且包括具有在其纵轴的圆周方向上具有机械接合槽的塞子,相对的翼梁进入该塞子中壁部分响应于配件上翼梁壁的缠绕制造而偏转。另外,在槽的对面设有皮带装置,以在机械接合加强的情况下将偏斜的梁壁部分局部地周边地限制在翼梁结构的安装状态下在离心力和弯曲载荷下梁壁部分从塞子槽中的相对移动。

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