A gas turbine engine (10) has a nose cone (80), a fan for delivering air into a bypass duct as bypass flow, and into a core engine to be delivered to a compressor. The nose cone (80) includes a vent (84) to receive air and deliver the air across a heat exchanger (86), which receives a fluid to be cooled. The air from the vent (84) is delivered to an outlet (104) downstream of the heat exchanger (86), such that a majority of the air being delivered to the outlet (104) becomes part of the bypass flow.
NOSE CONE HEAT EXCHANGER WITH RADIALLY OUTER DISCHARGE
NASENKONUSWÄRMETAUSCHER MIT RADIALER AUSSENENTLADUNG
ÉCHANGEUR DE CHALEUR DE POINT AVANT À DÉCHARGE RADIALE EXTERNE
31.07.2019
Patent
Elektronische Ressource
Englisch
Engine with nose cone heat exchanger and radially outer discharge
Europäisches Patentamt | 2019
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