Comparison of operation and control for free and fixed turbine engines; it seems that overtemperature and overspeed problems are more severe for free turbine engine; free turbine engine is faster and more resonant; shaft torque response is more sensitive to rotor loads for fixed turbine engine.


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    Titel :

    Shaft gas turbines for helicopters


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Miller, Jr., W.S. (Autor:in) / Krebs, R.P. (Autor:in) / Blaschke, T.C. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1955 Jet propelled



    Erscheinungsdatum :

    1955


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Shaft Gas Turbines For Helicopters

    Krebs, R. P. / Blaschke, T. C. / Miller, W. S. | SAE Technical Papers | 1956


    Shaft gas turbines for helicopters

    Miller, Jr., W.S. / Krebs, R.P. / Blaschke, T.C. | Engineering Index Backfile | 1956


    Matching the Characteristics of Helicopters and Shaft-Turbines

    Meyers, D.N. / Ciolkosz, Z.M. | SAE Technical Papers | 1954


    Gas turbines for helicopters

    Brown, J. | Engineering Index Backfile | 1954


    Gas turbines for helicopters

    Morley, A.W. / Cushing, W.R. | Engineering Index Backfile | 1960