发明名称 |
THERMOELECTRIC GENERATOR IN TURBINE ENGINE NOZZLES |
摘要 |
In one embodiment, a gas turbine engine assembly comprises an engine assembly disposed about a longitudinal axis, a core nozzle positioned adjacent the engine assembly to direct a core flow generated by the engine assembly, a fan nozzle surrounding at least a portion of the core nozzle to direct a fan flow, wherein the core nozzle defines a plenum to receive a portion of the core stream flow from the core nozzle and a thermoelectric generator assembly positioned in the plenum. Other embodiments may be described. |
申请公布号 |
CA2795647(C) |
申请公布日期 |
2016.02.02 |
申请号 |
CA20122795647 |
申请日期 |
2012.11.14 |
申请人 |
THE BOEING COMPANY |
发明人 |
KWOK, DAVID W.;HUANG, JAMES P.;MAULDIN, JACK W. |
分类号 |
F02K1/46;F02C7/32;F02K1/78 |
主分类号 |
F02K1/46 |
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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