发明名称 LANDING GEAR OF AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To further reduce air noises of landing gear.SOLUTION: Landing gear 1 includes a stud 2 for supporting a wheel 51, and link members (an upper arm 31, a lower arm 32, an upper link 41, and a lower link 42) which are attached to the stud. The link member has connection parts 311 and 411 on the side of one end, connection parts 312 and 412 on the side of the other end, and intermediate parts 313, 314 and 413 that connect the connection parts on the side of the one end and the connection parts on the side of the other end to one another. A clearance between both side edges of the intermediate part is closed.
申请公布号 JP2015229390(A) 申请公布日期 2015.12.21
申请号 JP20140115418 申请日期 2014.06.04
申请人 SUMITOMO PRECISION PROD CO LTD 发明人 INOUE TAKESHI
分类号 B64C25/16 主分类号 B64C25/16
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