发明名称 |
HYBRID AIRPLANE |
摘要 |
The invention relates to a hybrid aircraft (F). According to the invention, a suitable position for mounting an energy generation unit (14) in the aircraft is identified, said energy generation unit comprising an internal combustion engine (34) and an electric generator (30) that is coupled thereto via a shaft. Independently of the position of the energy generation unit (14), a position is also identified for a thrust generation unit (12) comprising an electric motor (24) and a propeller (20) that is coupled thereto via a shaft (22). When the aircraft (F) is built, the thrust generation unit (12) and the energy generation unit (14) are disposed in the positions identified therefor. The generator (30) is then coupled to the electric motor (24) via an electric transmission device (16). |
申请公布号 |
EP2844556(B1) |
申请公布日期 |
2016.04.27 |
申请号 |
EP20130724566 |
申请日期 |
2013.05.16 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
ANTON, FRANK;GEDIGA, SWEN;WOLLENBERG, JOHANNES |
分类号 |
B64C31/024;B64D27/02;B64D27/24 |
主分类号 |
B64C31/024 |
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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