发明名称 Pilot control system with compact gimbal mechanism
摘要 <p>According to one embodiment, a control assembly (200) includes a first gimbal (260) and a second gimbal (270). The first gimbal (260) is rotatable about a first axis of rotation. The first gimbal (260) comprises a first linkage attachment point offset from the first axis of rotation. The second gimbal (270) is rotatably coupled to the first gimbal (260) and rotatable relative to the first gimbal (260) about a second axis of rotation. The second gimbal (270) comprises a second linkage attachment point offset from the second axis of rotation and a control shaft attachment point.</p>
申请公布号 EP2626296(B1) 申请公布日期 2014.08.13
申请号 EP20130153191 申请日期 2013.01.30
申请人 BELL HELICOPTER TEXTRON INC. 发明人 YATES, TRAVIS L;LINTON, BRADLEY D
分类号 B64C13/04;B64C27/56 主分类号 B64C13/04
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