Aircraft landing gear assembly and method of assembling the same

The invention relates to an aircraft landing gear assembly and a method of assembly the same. A landing gear assembly for use with an aircraft includes a housing including a trunnion brace, a drag brace, and an aft brace that together define an opening through the housing. The landing gear assembly...

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Bibliographic Details
Main Authors COTTET JUSTIN, SONNENBURG GEORGE, CUSWORTH JAMES
Format Patent
LanguageChinese
English
Published 02.11.2018
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention relates to an aircraft landing gear assembly and a method of assembly the same. A landing gear assembly for use with an aircraft includes a housing including a trunnion brace, a drag brace, and an aft brace that together define an opening through the housing. The landing gear assembly also includes a shrink link assembly coupled to the housing such that the shrink link assembly is accessible through the opening. 本发明涉及飞行器起落架组件及其组装方法。与飞行器起使用的起落架组件包括壳体，所述壳体包括起限定通过壳体的开口的耳轴支架、阻力支架和后支架。起落架组件还包括收缩连杆组件，所述收缩连杆组件被耦接到壳体，使得收缩连杆组件可通过开口进入。
Bibliography:Application Number: CN201810163344