PROBLEM TO BE SOLVED: To provide an aircraft landing gear assembly and a method of assembling the same.SOLUTION: A landing gear assembly 102 for use with an aircraft includes: a wheel assembly coupled to an inner cylinder 118, which is slidably coupled within a housing; and the housing including a trunnion brace 136, a drag brace 138 and an aft brace 140 that together define an opening 142 through the housing. The landing gear assembly also includes a shrink link assembly 130 coupled to the housing such that the shrink link assembly is accessible through the opening.SELECTED DRAWING: Figure 2
【課題】航空機着陸装置アセンブリ及びその組立方法を提供する。【解決手段】航空機で使用する着陸装置アセンブリ102は、内側円筒118に結合された車輪アセンブリを含み、この内側円筒は、ハウジング内に摺動可能に結合される。ハウジングを貫通する開口部142を共に画定するトラニオンブレース136と抗力ブレース138と後方ブレース140とを含むハウジングを含む。着陸装置アセンブリはまた、収縮リンクアセンブリ130が開口部を通してアクセス可能であるようにハウジングに結合された収縮リンクアセンブリを含む。【選択図】図2
AIRCRAFT LANDING GEAR ASSEMBLY AND METHOD OF ASSEMBLING THE SAME
航空機着陸装置アセンブリ及びその組立方法
2018-11-15
Patent
Electronic Resource
Japanese
IPC: | B64C AEROPLANES , Flugzeuge |
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