发明名称 |
HYBRID POWER SYSTEM ARCHITECTURE FOR AN AIRCRAFT |
摘要 |
A hybrid power distribution system for an aircraft generates hydraulic power from one of a plurality of power sources based on which power source provides energy most efficiently. Power sources includes an electric power distribution bus that distributes electrical energy onboard the aircraft, a pneumatic distribution channel that distributes pneumatic energy onboard the aircraft, and mechanical power provided by one or more engines associated with the aircraft.
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申请公布号 |
US2013306790(A1) |
申请公布日期 |
2013.11.21 |
申请号 |
US201313953164 |
申请日期 |
2013.07.29 |
申请人 |
HAMILTON SUNDSTRAND CORPORATION |
发明人 |
BRUNO LOUIS J.;JONES ANTHONY C.;SPIERLING TODD A.;DEFRANCESCO GREGORY L. |
分类号 |
B64D41/00 |
主分类号 |
B64D41/00 |
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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