发明名称 |
Energy recovery device for producing electrical energy to e.g. electrical circuit in aircraft, has wing supporting unit connected to energy transformation unit, and profiled wing placed along flow of fluid |
摘要 |
<p>The device (1) has a profiled wing (2) placed along flow of fluid (15) e.g. air or water. An elastic return unit i.e. spring (6), elastically returns an aileron (4) to a position in which the aileron extends from an extension of the wing. Supporting and guiding units e.g. support (7) and guide bearing (9), support and guide the wing in translation to transversely generate oscillating movement of the wing in the direction of circulation of the fluid. A wing supporting unit is connected to the energy transformation unit that constitutes a connecting rod (10) and a crankshaft (12).</p> |
申请公布号 |
FR2964160(A1) |
申请公布日期 |
2012.03.02 |
申请号 |
FR20100056807 |
申请日期 |
2010.08.27 |
申请人 |
SNECMA |
发明人 |
JUCHAULD ETIENNE;FOUCAULT ALAIN, AUGUSTE, JACQUES;BALK WOUTER |
分类号 |
F03D5/06;B64D41/00;F03B17/00 |
主分类号 |
F03D5/06 |
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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