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    ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    Neue Suche nach: ROBERGE GARY D

    A rotor assembly is provided for a gas turbine engine. This rotor assembly includes a first rotor disk (110A), a second rotor disk (110B), a plurality of rotor blades (34) and a plurality of disk mounts (118). The first rotor disk is configured to rotate about a rotational axis (32). The second rotor disk is configured to rotate about the rotational axis. The rotor blades are arranged circumferentially around the rotational axis. Each of the rotor blades is mounted to the first rotor disk and to the second rotor disk. The rotor blades include a first rotor blade (34A). Each of the disk mounts connects the first rotor disk and the second rotor disk together. The disk mounts include a first disk mount (118A) that further supports the first rotor blade.

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    ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    Neue Suche nach: ROBERGE GARY D

    A rotor assembly is provided for a gas turbine engine. This rotor assembly includes a first rotor disk (110A), a second rotor disk (110B), a plurality of rotor blades (34) and a plurality of disk mounts (118). The first rotor disk is configured to rotate about a rotational axis (32). The second rotor disk is configured to rotate about the rotational axis. The rotor blades are arranged circumferentially around the rotational axis. Each of the rotor blades is mounted to the first rotor disk and to the second rotor disk. The rotor blades include a first rotor blade (34A). Each of the disk mounts connects the first rotor disk and the second rotor disk together. The disk mounts include a first disk mount (118A) that further supports the first rotor blade.

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    ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    Neue Suche nach: ROBERGE GARY D

    A rotor assembly is provided for a gas turbine engine. This rotor assembly includes a first rotor disk (110A), a second rotor disk (110B), a plurality of rotor blades (34) and a plurality of disk mounts (118). The first rotor disk is configured to rotate about a rotational axis (32). The second rotor disk is configured to rotate about the rotational axis. The rotor blades are arranged circumferentially around the rotational axis. Each of the rotor blades is mounted to the first rotor disk and to the second rotor disk. The rotor blades include a first rotor blade (34A). Each of the disk mounts connects the first rotor disk and the second rotor disk together. The disk mounts include a first disk mount (118A) that further supports the first rotor blade.

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    Titel:

    ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    Weitere Titelangaben:

    ROTORZUSAMMENBAU FÜR EIN GASTURBINENTRIEBWERK
    ENSEMBLE ROTOR POUR UN MOTEUR À TURBINE À GAZ

    Beteiligte:

    ROBERGE GARY D (Autor:in)

    Erscheinungsdatum:

    14.06.2023

    Medientyp:

    Patent

    Format:

    Elektronische Ressource

    Sprache:

    Englisch

    Klassifikation:

    IPC:  F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / C04B Kalk , LIME

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