发明名称 |
TURBOJET ENGINE FOR AIRCRAFT |
摘要 |
<p>A turbojet engine for an aircraft that includes an engine provided in a nacelle and at least one heat exchanger for cooling down a hot fluid collected in the propulsion system of the turbojet engine before re-injecting the aforementioned partially-cooled hot flow into the aforementioned propulsion system, wherein at least one heat exchanger is a radial heat exchanger extending in the lower portion of the turbojet engine at a lower branching of the turbojet engine.</p> |
申请公布号 |
EP2167798(A2) |
申请公布日期 |
2010.03.31 |
申请号 |
EP20080806024 |
申请日期 |
2008.06.18 |
申请人 |
AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE) |
发明人 |
BULIN, GUILLAUME;OBERLE, PATRICK |
分类号 |
F02C7/14;F02K3/06 |
主分类号 |
F02C7/14 |
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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