发明名称 |
Landing gear retraction/extension device of aircraft |
摘要 |
<p>A landing gear retraction/extension device includes a hydraulic actuator (2), a hydraulic circuit, a hydraulic pump (5), an electric motor (6), and a driver (61). Part of the hydraulic circuit is provided such that heat is exchangeable between operation oil and each of the electric motor (6) and the driver (61). The driver (61) supplies power to the electric motor before landing of an aircraft such that an operation oil temperature is higher than a predetermined temperature upon the landing of the aircraft.</p> |
申请公布号 |
EP2570344(A2) |
申请公布日期 |
2013.03.20 |
申请号 |
EP20120184275 |
申请日期 |
2012.09.13 |
申请人 |
SUMITOMO PRECISION PRODUCTS CO., LTD. |
发明人 |
ONOMICHI, YASUTO;KONDO, TAKU;HAGIHARA, SHOGO;TAKAKI, RYO;ONISHI, TAKAAKI |
分类号 |
B64C25/22;B64C13/50;F15B21/04 |
主分类号 |
B64C25/22 |
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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