A compressor manifold (100) includes a primary section (104) having a primary inlet port (110), a first primary outlet port (112), and a second primary outlet port (114), the primary section (104) configured to receive a fluid from a primary heat exchanger (22) through the primary inlet port (110) and direct the fluid to at least one compressor (42) through the first and second primary outlet ports (112, 114). A secondary section (106) includes a first secondary inlet port (116), a second secondary inlet port (118), and a secondary outlet port (120), the secondary section (106) configured to receive the fluid from the at least one compressor (42) through the first and second secondary inlet ports (116, 118) and direct the fluid to a secondary heat exchanger (26) through the secondary outlet port (120). A bypass valve (102) is positioned between the primary section (104) and the secondary section (106) to fluidly couple the primary section (104) and the secondary section (106) to bypass the at least one compressor (42).


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    Titel :

    MULTI-PORT COMPRESSOR MANIFOLD WITH INTEGRAL BYPASS VALVE


    Weitere Titelangaben:

    KOMPRESSORVERTEILER MIT MEHREREN ANSCHLÜSSEN MIT INTEGRIERTEM UMGEHUNGSVENTIL
    COLLECTEUR DE COMPRESSEUR MULTIPORT AVEC SOUPAPE DE DÉRIVATION INTÉGRÉE


    Beteiligte:

    Erscheinungsdatum :

    2019-06-19


    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 / F24F Klimatisierung , AIR-CONDITIONING / F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS



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