An aircraft assembly comprises a longitudinal spar and an aerofoil cover integrally formed from a composite laminate material to form a spar-cover such that the composite material of the spar extends continuously into the cover through a fold region created between the spar and the cover. The spar and cover are separated by a recess at a longitudinal end of the fold region to define a spar end region and a cover end region, and a reinforcement element extends between the spar end region and the cover end region to couple the spar end region with the cover end region.
一种飞行器组件,该飞行器组件包括纵向翼梁和翼型盖,该纵向翼梁和翼型盖由复合层压材料一体地形成以形成翼梁‑盖,使得翼梁的复合材料通过在翼梁与盖之间产生的折叠区域连续地延伸到盖中。翼梁和盖由位于折叠区域的纵向端部处的凹部间隔开,以限定翼梁端部区域和盖端部区域,并且加强元件在翼梁端部区域与盖端部区域之间延伸以将翼梁端部区域与盖端部区域联接。
AIRCRAFT ASSEMBLY HAVING AN INTEGRAL SPAR-COVER
具有一体式翼梁-盖的飞行器组件
2021-09-07
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |