发明名称 |
Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow |
摘要 |
An aircraft propulsion unit including a turbojet and a heat exchanger located above the turbojet and drawing a cooling air stream and a hot air stream in the turbojet. Wherein the cooling air intake and hot air intake surfaces in the housing are directed forward of the turbojet and have normal lines inclined relative to the axis of the turbojet. The embodiment also concerns an aircraft equipped with at least one such propulsion unit.
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申请公布号 |
US8522529(B2) |
申请公布日期 |
2013.09.03 |
申请号 |
US20060996019 |
申请日期 |
2006.07.07 |
申请人 |
MARTINOU JEAN-MARC;MARCHE HERVE;AIRBUS OPERATIONS SAS |
发明人 |
MARTINOU JEAN-MARC;MARCHE HERVE |
分类号 |
F02K99/00;B64D33/10;F02C6/04;F02C6/08 |
主分类号 |
F02K99/00 |
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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