发明名称 |
ENGINE ASSEMBLY FOR AN AIRCRAFT COMPRISING AN ENGINE AS WELL AS AN ENGINE MOUNTING STRUCTURE FOR SUCH AN ENGINE |
摘要 |
<p>The invention concerns an engine assembly (1) for an aircraft comprising an engine and an engine mounting structure for (4) the engine, the assembly also comprising a heat exchanging system (104) provided with a second outlet (122a) located between the structure box and the engine, rearwards relative to the rear engine attachment (8). Moreover, the exchanger (114) of the heat exchanging system (104) is arranged at least partly inside a rear aerodynamic fairing (66) of the engine mounting structure (4), said rear aerodynamic fairing (66) being located entirely rearwards relative to said rear engine attachment (8).</p> |
申请公布号 |
WO2007036523(A1) |
申请公布日期 |
2007.04.05 |
申请号 |
WO2006EP66742 |
申请日期 |
2006.09.26 |
申请人 |
AIRBUS FRANCE;JOURNADE, FREDERIC;BRUNET, ROBERT |
发明人 |
JOURNADE, FREDERIC;BRUNET, ROBERT |
分类号 |
B64D33/10;F02C7/14 |
主分类号 |
B64D33/10 |
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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