A surface cooler having a first cooling passage section configured to be operably coupled to a fan casing of an aircraft engine, the cooling passage section having a heat exchanger body defining a first distal end and a second distal end and having a set of fluid passages internal to the heat exchanger body and a first set of fins located on a first exterior surface of the heat exchanger body and a manifold operably coupled to a first distal end of the cooling passage section and wherein the manifold includes a manifold body having an interior fluidly coupled to at least one of the set of fluid passages and a second set of fins located on the manifold body to define a finned manifold and a method for forming same.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT SURFACE COOLER ASSEMBLY



    Publication date :

    2020-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke




    Cooler Assembly

    MIZE JR ALLEN HOBBS | European Patent Office | 2020

    Free access

    Cooler assembly

    MIZE JR ALLEN HOBBS | European Patent Office | 2022

    Free access

    FUEL COOLER ASSEMBLY

    JORGENSEN INER M | European Patent Office | 2016

    Free access

    PLATE COOLER FOR AIRCRAFT ELECTRONIC COMPONENTS

    TOMESCU DANA / BERTON GUILLAUME | European Patent Office | 2021

    Free access