发明名称 |
AUXILIARY POWER UNIT INLET DOOR POSITION CONTROL SYSTEM AND METHOD |
摘要 |
Methods and apparatus are provided for controlling an auxiliary power unit (APU) inlet door. A plurality of APU operational parameters and a plurality of aircraft operational parameters are sensed. The APU operational parameters and the aircraft operational parameters are processed to determine a minimum APU inlet door position that will maintain APU turbine inlet temperature at a predetermined value. The APU inlet door is then moved to the determined minimum APU inlet door position.
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申请公布号 |
US2013074519(A1) |
申请公布日期 |
2013.03.28 |
申请号 |
US201113245612 |
申请日期 |
2011.09.26 |
申请人 |
ERTZ TIMOTHY;GEYER GERGORY;BARON MIKE;HONEYWELL INTERNATIONAL INC. |
发明人 |
ERTZ TIMOTHY;GEYER GERGORY;BARON MIKE |
分类号 |
F02C6/00 |
主分类号 |
F02C6/00 |
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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