This paper reviews those requirements that are common in the design of all gas turbines combustion equipment. Where necessary, a distinction is made between the demands of industrial and aircraft chambers. The problem of designing equipment for long life and low pressure loss, in a size compatible with the overall engine, is discussed in detail, and the application of combustor characteristics and design factors to the demands of new aircraft and industrial turbines are anticipated.


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    Title :

    General Considerations in the Design of Combustion Chambers for Aircraft and Industrial Gas Turbines


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE World Congress & Exhibition ; 1964



    Publication date :

    1964-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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