An auxiliary power unit may comprise a twin centrifugal compressor including a first blade. A turbine may be disposed aft of the twin centrifugal compressor. The turbine may include a second blade. The first blade comprises a first material and the second blade comprises a second material. The first material may the same as the second material. The twin centrifugal compressor may include forward centrifugal compressor and an aft centrifugal compressor disposed aft of the forward centrifugal compressor.


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    Titel :

    Twin centrifugal single spool engine


    Beteiligte:
    KUPRATIS DANIEL BERNARD (Autor:in) / UTAY ARTHUR W (Autor:in) / KASHYAP TANIA BHATIA (Autor:in) / SLAVENS THOMAS N (Autor:in) / RUGG KEVIN L (Autor:in) / ZELESKY MARK F (Autor:in) / MERRY BRIAN D (Autor:in) / SUCIU GABRIEL L (Autor:in)

    Erscheinungsdatum :

    30.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



    TWIN CENTRIFUGAL SINGLE SPOOL ENGINE

    KUPRATIS DANIEL BERNARD / UTAY ARTHUR W / KASHYAP TANIA BHATIA et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    A Twin Spool Engine Emulator for the Study of Power Exchange Idea

    Enalou, Hossein Balaghi / Rashed, Mohamed / Kulsangcharoen, Ponggorn et al. | IEEE | 2018


    Dynamic characteristics of a single-spool turbojet engine

    Craig, R T / Vasu, George / Schmidt, R D | NTRS | 1953


    TWO SPOOL MORE ELECTRICAL ENGINE

    Colin, A. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006