Coolant-carrying liner for combustion chambers runs cooler and tolerates high-temperature excursions without burning out. Hot gases flowing through core prevented by liner from damaging shell. Concept applicable to such high-temperature chambers as rocket pre-burners, turbojet cans, stationary-turbine combustors, oil burners, and high-pressure chemical reactors.


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    Title :

    Ribbed Coolant Liners for Combustion Chambers


    Contributors:

    Published in:

    Publication date :

    1984-11-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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