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.


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    Title :

    NOSE CONE HEAT EXCHANGER WITH RADIALLY OUTER DISCHARGE


    Additional title:

    NASENKONUSWÄRMETAUSCHER MIT RADIALER AUSSENENTLADUNG
    ÉCHANGEUR DE CHALEUR DE POINT AVANT À DÉCHARGE RADIALE EXTERNE


    Contributors:

    Publication date :

    2019-07-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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