发明名称 TWO MOTOR REDUNDANT DRIVE MECHANISM
摘要 A redundant drive mechanism (10) comprises a platform (16) and a shaft (30) rotatably mounted with respect to the platform (16). A first motor (42) is stationarily mounted with respect to the platform (16). The first motor (42) drives a first pinion (50). A ring gear carrier (56) is mounted on the shaft (30) and is rotationally fixed to the shaft (30). A ring gear (62) is rotatably mounted on the ring gear carrier (56). The first pinion (50) is in gear-tooth engagement with the ring gear (62). A second motor (44) is mounted on the ring gear carrier (56). The second motor (44) drives a second pinion (52) which, in turn, is in gear-tooth engagement with the ring gear (62). Energization of either the first or second motor (42, 44) causes rotation of the shaft (30) with respect to the platform (16).
申请公布号 EP0311872(B1) 申请公布日期 1993.05.05
申请号 EP19880116388 申请日期 1988.10.04
申请人 HUGHES AIRCRAFT COMPANY 发明人 GRANT, RICHARD W.
分类号 F16H1/20;B64C13/34;F16D65/14;F16H37/06;H01Q3/04;H02K7/116;H02K16/00 主分类号 F16H1/20
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