Aspects of the disclosure are directed to a screen configured for use in association with a cooler of an aircraft, the screen comprising: a first portion arranged as a grid and located in a line-of-sight of the cooler with respect to a fluid inlet, and a second portion located out of the line-of-sight of the cooler with respect to the fluid inlet, wherein the second portion is grid-free.


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    Titel :

    Aircraft hail screen


    Beteiligte:
    SNYDER RYAN K (Autor:in) / HEIMS ERIC J (Autor:in)

    Erscheinungsdatum :

    2018-01-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B01D SEPARATION , Trennen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    AIRCRAFT HAIL SCREEN

    SNYDER RYAN K / HEIMS ERIC J | Europäisches Patentamt | 2016

    Freier Zugriff

    Hail Damage to Typical Aircraft Surfaces

    Robert J. Hayduk | AIAA | 1973