发明名称 |
COMBUSTION ENGINE, AIRCRAFT PROVIDED WITH SAID ENGINE AND METHOD FOR MANUFACTURING SUCH AN ENGINE |
摘要 |
The present invention relates to a combustion engine (1) which includes: at least one crankshaft (2) rotating about a first rotation shaft (3); at least one output shaft (4) outputting an engine torque, said output shaft (4) rotating about a second rotation shaft (5) separate from said first rotation shaft (3); at least one transmission assembly (6) rotating about said first rotation shaft (3) and being rotated by said crankshaft (2) in order to transmit said engine torque to said output shaft (4). |
申请公布号 |
WO2017021165(A1) |
申请公布日期 |
2017.02.09 |
申请号 |
WO2016EP67400 |
申请日期 |
2016.07.21 |
申请人 |
AIRBUS HELICOPTERS |
发明人 |
MERCIER, Christian;HUBERT, Pierre-Julien;GAVANIER, Pierre;BALASTRIER, Yann |
分类号 |
F16D1/06;F16D3/06;F16H57/00 |
主分类号 |
F16D1/06 |
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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