Integration of an air-liquid heat exchanger on an engine

Details Integration of an air-liquid heat exchanger on an engine Integration of an air-liquid heat exchanger on an engine

F - Mech Eng,Light,Heat,Weapons

01

P

F01P 3/18 (2006.01) F01P 3/00 (2006.01)

Patent

CA 2725499

The invention relates to a bypass axial turbomachine (2) comprising a fan (10); a low pressure stator stage (42); a high pressure stator stage (44), the compressors being traversed by a flow referred to as primary flow (4) of the turbomachine; at least one passage (22) of discharge flow rate (24) controlled from the primary flow (4) in one of the stator stages toward the secondary flow (6); a heat exchanger of the surface air-oil (ACOC) type (28) arranged flat on or in the wall (26) surrounding the stator stages and defining the internal surface of the secondary flow (6), directly downstream of the junction of the passage of the discharge flow rate (22) with said wall (26), so as to be run through by the secondary flow (6) enriched with the discharge flow rate (24).

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