A hydromechanical approach to the problem of reducing the compexity and cost of turbine fuel controls without impairing performance and reliability is described and analyzed. The study applies to the modification of long-range high-performance turbine engines to meet short-range missile requirements. The generalized acceleration and deceleration control parameters are studied, and variable-orifice relations for acceleration and deceleration limits are derived. The hydromechanical speed-sensing and multiplying circuit and the fuel control schematic diagram are discussed.


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    Titel :

    A simplified fuel control approach for low-cost aircraft gas turbines


    Beteiligte:
    Gold, H. (Autor:in)

    Kongress:

    Air Transportation Meeting ; 1973 ; Miami, FL


    Erscheinungsdatum :

    01.04.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :