发明名称 |
GENERATING DEVICE FOR AIRCRAFT |
摘要 |
A generating device (1) capable of preventing an increase in the frontal area of an aircraft engine is provided with: a transmission (22) connected to a rotating shaft of the engine; a generator (34) driven by output from the transmission (22); an input shaft (27) connected to the rotating shaft and having a shaft center extending in a direction perpendicular to the rotating shaft; and a transmission mechanism (21) connected to the input shaft (27) and configured to drive the transmission (22) about the shaft center perpendicular to the input shaft (27). The transmission (22) and the generator (34) are spaced apart from each other in the circumferential direction of the rotating shaft. |
申请公布号 |
CA2832153(C) |
申请公布日期 |
2015.02.10 |
申请号 |
CA20122832153 |
申请日期 |
2012.04.04 |
申请人 |
KAWASAKI JUKOGYO KABUSHIKI KAISHA |
发明人 |
GOI, TATSUHIKO;TANAKA, KENICHIRO;WATANABE, KOJI;FUJII, ISAO |
分类号 |
F02C7/32;B64D41/00;F01D15/10;F01D25/18;F02C7/00;F02C7/36 |
主分类号 |
F02C7/32 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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