An aircraft turbomachine including a nacelle and an engine further including at least one outflowing jet of air, wherein a heat exchanger of the precooler type for supplying air to the aircraft is mounted in the nacelle. The exchanger includes a primary circuit, the inlet of which is connected to a supply of compressed air from the engine and the outlet of which is connected to an air supply for supplying air to the aircraft, and a secondary circuit supplied with air taken from said air flow.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft turbomachine comprising a heat exchanger of the precooler type


    Contributors:

    Publication date :

    2021-07-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    AIRCRAFT TURBOMACHINE COMPRISING A HEAT EXCHANGER OF THE PRECOOLER TYPE

    FERT JÉRÉMY EDMOND / DE VULPILLIERES ERIC / PAVILLET JULIEN | European Patent Office | 2017

    Free access

    Air recovery system for precooler heat-exchanger

    CHEONG CHEE YUEN | European Patent Office | 2015

    Free access

    AIR RECOVERY SYSTEM FOR PRECOOLER HEAT-EXCHANGER

    CHEONG CHEE YUEN | European Patent Office | 2015

    Free access

    AIR RECOVERY SYSTEM FOR PRECOOLER HEAT-EXCHANGER AND CORRESPONDING METHOD

    CHEONG CHEE YUEN | European Patent Office | 2020

    Free access

    EVOLUTIVE PRECOOLER

    PRIETO PADILLA JUAN TOMÁS / BARRÓN VEGA DIEGO | European Patent Office | 2025

    Free access