发明名称 |
SYSTEM AND METHOD FOR OPERATING A PRECOOLER IN AN AIRCRAFT |
摘要 |
An aircraft engine includes a precooler disposed within a nacelle. The precooler defines an ambient air passage and a bleed air passage. Air passes through the precooler from an ambient air inlet to an ambient air outlet. Bleed air passes through the precooler from a bleed air inlet to a bleed air outlet. Heat is transferred between the air and the bleed air via heat exchange within the precooler. At least one pressure relief door disposed proximate to the air outlet of the engine. A controller is operatively connected to the pressure relief door. The controller at least opens the pressure relief door based on a demand for increased flow of air through the ambient air passage. |
申请公布号 |
US2014000279(A1) |
申请公布日期 |
2014.01.02 |
申请号 |
US201214004974 |
申请日期 |
2012.03.16 |
申请人 |
BROUSSEAU JEAN;AFRIANTO SIGIT;HAMEL REMI;DESILETS VALERIE;BOMBARDIER INC. |
发明人 |
BROUSSEAU JEAN;AFRIANTO SIGIT;HAMEL REMI;DESILETS VALERIE |
分类号 |
F02C7/00 |
主分类号 |
F02C7/00 |
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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