B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 33/10 (2006.01) F02C 7/14 (2006.01)
Patent
CA 2624010
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).
L'invention se rapporte à un ensemble moteur (1) pour aéronef comprenant un moteur et un mât d'accrochage (4) du moteur, l'ensemble comportant également un système d'échangeur thermique (104) disposant d'une seconde sortie (122a) située entre le caisson et le moteur, en arrière par rapport à l'attache moteur arrière (8). De plus, l'échangeur (114) du système d'échangeur thermique (104) est agencé au moins partiellement à l'intérieur d'un carénage aérodynamique arrière (66) du mât d'accrochage (4), ce carénage aérodynamique arrière (66) étant situé entièrement en arrière par rapport à ladite attache moteur arrière (8).
Brunet Robert
Journade Frederic
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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