首页> 外国专利> AIRCRAFT LANDING GEAR BAY ROOF COMPRISING AN INCLINED AFT BULKHEAD

AIRCRAFT LANDING GEAR BAY ROOF COMPRISING AN INCLINED AFT BULKHEAD

机译:飞机起落架齿轮舱顶,包括倾斜的船尾舱盖

摘要

An aircraft landing gear bay roof for forming a pressurization barrier between an upper pressurized compartment and a landing gear bay for the housing of a landing gear. The roof comprises a main bulkhead extending in a longitudinal direction, an inclined forward bulkhead, rigidly connected to a forward edge of the main wall, and an inclined aft bulkhead, rigidly connected to an aft edge of the main bulkhead. The forward bulkhead and the aft bulkhead each form an obtuse angle with the main bulkhead. This configuration enables a better absorption of loads by the landing gear bay roof and a shorter and optimized path for transmission of the mechanical loads, in particular to the fuselage member to which the aft bulkhead is configured to be connected.
机译:一种飞机起落架舱顶,用于在上部加压舱和起落架舱之间形成用于起落架壳体的加压屏障。屋顶包括在纵向上延伸的主舱壁,刚性地连接到主壁的前边缘的倾斜的前舱壁,以及刚性地连接到主舱壁的后边缘的倾斜的后舱壁。前舱壁和后舱壁均与主舱壁成钝角。这种构造能够通过起落架舱顶更好地吸收载荷,并且具有较短且优化的路径,用于将机械载荷尤其是传递至构造成与后舱壁相连的机身构件。

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