An aircraft assembly with a hot air exhaust outlet. The aircraft assembly has an assembly surface over which a hot-air exhaust flow from the hot-air exhaust outlet is exhausted. The aircraft assembly also has a vortex generator with a flow surface. The flow surface lies in an air flow over the vortex generator. The flow surface is arranged to interrupt the hot-air exhaust flow and generates a flow vortex to cool the air flow over the assembly surface.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft assembly with a hot-air exhaust outlet and cooperating vortex generator, and method controlling same


    Contributors:

    Publication date :

    2022-08-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    EXHAUST ASSEMBLY WITH VORTEX GENERATOR

    IGLEWSKI TOMASZ | European Patent Office | 2018

    Free access

    EXHAUST ASSEMBLY WITH VORTEX GENERATOR

    IGLEWSKI TOMASZ | European Patent Office | 2018

    Free access

    AIRCRAFT ASSEMBLY WITH A HOT-AIR EXHAUST OUTLET

    CUSTANCE DENYS / HEALY DAREN | European Patent Office | 2020

    Free access

    AIRCRAFT ASSEMBLY WITH A HOT-AIR EXHAUST OUTLET

    CUSTANCE DENYS / HEALY DAREN | European Patent Office | 2022

    Free access

    Aircraft assembly with a hot-air exhaust outlet

    DENYS CUSTANCE / DAREN HEALY | European Patent Office | 2020

    Free access