公开(公告)号：US20140369812A1

公开(公告)日：2014-12-18

申请号：US14471323

申请日：2014-08-28

Applicant: AIRCELLE

Inventor： Pierre CARUEL ,  Franck ZAGANELLI ,  Patrick GONIDEC ,  Olivier KERBLER

IPC: F01D25/24

CPC classification number: F01D25/24 ,  B64D15/04 ,  B64D33/02 ,  B64D33/10 ,  B64D2033/0233 ,  F02C7/047 ,  F02C7/12 ,  F02K3/06 ,  F05D2240/14 ,  F05D2260/213 ,  Y02T50/676

Abstract: A nacelle of a turbine engine includes an external cowling, an internal cowling, and a heat exchanger associated with at least one circulation duct for a fluid. In particular, the circulation duct forms a recirculation loop through the heat exchanger, and the recirculation loop includes at least one circulation area extending at least partially along the external cowling in contact with a wall of the external cowling so as to allow exchange of heat by conduction with the air outside the nacelle.

Abstract translation: 涡轮发动机的机舱包括外部整流罩，内部整流罩和与用于流体的至少一个循环管道相关联的热交换器。 特别地，循环管道形成通过热交换器的再循环回路，并且再循环回路包括至少部分沿着外部整流罩延伸的至少一个循环区域，该外部整流罩与外部整流罩的壁接触，以便允许通过 与机舱外的空气导通。