发明名称 Turbojet engine with oil cooler in the engine nacelle
摘要 <p>The engine has a core thruster (10) surrounded by a by-pass channel (29). A radially expressed engine cowl (30) encloses the by-pass channel and is placed at a rear portion of a thrust-reverser (31). The thrust-reverser is moveable relative to the engine cowl. A periphery radiator part e.g. surface cooler, matrix cooler and oil cooler, extends in an intermediate area (40) between the engine cowl and the thrust-reverser. The radiator element is arranged at a diverting region (33) of the engine cowl, where the radiator element includes a flow-guiding element (44).</p>
申请公布号 EP2522831(B1) 申请公布日期 2015.10.21
申请号 EP20120003733 申请日期 2012.05.10
申请人 ROLLS-ROYCE DEUTSCHLAND LTD & CO KG 发明人 TODOROVIC, PREDRAG
分类号 F02C7/14;B64D33/10;F02K1/72 主分类号 F02C7/14
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