发明名称 Locking actuator for aircraft landing gear
摘要 An actuator 10 comprising: a first part 12 arranged to be driven relative to a second part 18; a locking system 24, 30, 26 having a locking condition in which it is arranged to inhibit relative movement between the first part and the second part and a non-locking condition in which it is arranged to permit relative movement between the first part and the second part; and a release system 26 movable to a release condition in which it changes the locking system from the locking condition to the non-locking condition, wherein the locking system is arranged to mechanically change from the non-locking condition to the locking condition upon the first part assuming a predetermined position relative to the second part. The locking system may comprise resiliently deformable claws 24 including one or more pawls 24a.
申请公布号 GB2492178(A) 申请公布日期 2012.12.26
申请号 GB20110014316 申请日期 2011.08.19
申请人 MESSIER-DOWTY LIMITED 发明人 KYLE SCHMIDT
分类号 F15B15/26;B64C25/26 主分类号 F15B15/26
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