THE production problems associated with turbojet engines are not more complex than those encountered with reciprocating engines, according to the author, but they are of a surprisingly different nature.For instance, he points out that, whereas reciprocating engine parts are made chiefly from forgings, castings, and bar stock, the major portion of the turbojet engine is welded sheet metal structure.Then, the so-called hot parts - the combustion chamber, nozzle diaphragm, turbine, and tail cone - also present entirely new problems. The control of heat distortion caused by the high temperatures and the high temperature differentials in these parts requires closer coordination with metallurgists, steel mills, forge shops, welders, and parts fabricators than is required with reciprocating engines.


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    Titel :

    Production Problems of Turbojet Engines


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    McCRAE, T. S. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1949-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    PROBLEMS RELATED TO THE INTRODUCTION OF TITANIUM INTO PRODUCTION TURBOJET ENGINES

    LaMARCA, J. L. / McCABE, J. L. | SAE Technical Papers | 1956


    Large lightweight turbojet engines

    Grinyer, C.A. | Engineering Index Backfile | 1957


    Large Lightweight Turbojet Engines

    Grinyer, C. A. | SAE Technical Papers | 1958


    Large lightweight turbojet engines

    Grinyer, C.A. | Engineering Index Backfile | 1957


    Starters For Turbojet Engines

    DOWNS, WILLIAM D. | SAE Technical Papers | 1951