Methods and systems for operating a turboprop engine having a high pressure spool and a low pressure spool rotating independently from one another. Each spool contains at least one compressor stage and the low pressure spool is connected to a propeller. The method comprises determining a target temperature-corrected rotational speed of the low pressure spool for a given set of operating parameters; and controlling a mechanical speed of the low pressure spool to maintain the temperature-corrected rotational speed of the low pressure spool substantially constant throughout at least a portion of a range of a power demand on the turboprop engine.


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    Titel :

    Power plant thrust management system for turboprop engines


    Beteiligte:
    MORGAN KEITH (Autor:in) / PLANTE GHISLAIN (Autor:in) / FAUCHON TANIA (Autor:in)

    Erscheinungsdatum :

    2019-11-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge



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    Single Lever Power Management of Turboprop Engines

    Prevallet, L.C. | SAE Technical Papers | 1991


    Modern turboprop engines

    Saravanamuttoo, H.I.H. | Elsevier | 1986