Fachinformationsdienst BAUdigital

Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik

    ROTOR BLADE AND ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    Neue Suche nach: ROBERGE GARY D

    A rotor blade is provided for a gas turbine engine. This rotor blade includes a rotor blade pair (42) including a mount (38), a first airfoil (40A) and a second airfoil (40B). The mount includes a forked body with a first leg (50A) and a second leg (50B). The first airfoil is connected to the first leg. The second airfoil is connected to the second leg and arranged circumferentially next to the first airfoil.

    Zugriff

    Download

    Zugriff

    Download

    Seitennavigation

    Dokumentinformationen
    Ähnliche Titel

    Exportieren, teilen und zitieren

    ROTOR BLADE AND ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    Neue Suche nach: ROBERGE GARY D

    A rotor blade is provided for a gas turbine engine. This rotor blade includes a rotor blade pair (42) including a mount (38), a first airfoil (40A) and a second airfoil (40B). The mount includes a forked body with a first leg (50A) and a second leg (50B). The first airfoil is connected to the first leg. The second airfoil is connected to the second leg and arranged circumferentially next to the first airfoil.

    Zugriff

    Download

    ROTOR BLADE AND ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    Neue Suche nach: ROBERGE GARY D

    A rotor blade is provided for a gas turbine engine. This rotor blade includes a rotor blade pair (42) including a mount (38), a first airfoil (40A) and a second airfoil (40B). The mount includes a forked body with a first leg (50A) and a second leg (50B). The first airfoil is connected to the first leg. The second airfoil is connected to the second leg and arranged circumferentially next to the first airfoil.

    Zugriff

    Download

    Zugriff

    Download

    Seitennavigation

    Dokumentinformationen
    Ähnliche Titel

    Exportieren, teilen und zitieren

    Dokumentinformationen
    Titel:

    ROTOR BLADE AND ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    Weitere Titelangaben:

    ROTORSCHAUFEL UND ROTORZUSAMMENBAU FÜR EIN GASTURBINENTRIEBWERK
    AUBE ROTORIQUE ET ENSEMBLE ROTOR POUR UN MOTEUR À TURBINE À GAZ

    Beteiligte:

    ROBERGE GARY D (Autor:in)

    Erscheinungsdatum:

    28.06.2023

    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

    Ähnliche Titel

    TURBINE ROTOR BLADE

    KAWANISHI KEN / WATANABE FUMIAKI / AHARA TAKAO et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    ROTOR BLADE AND METHOD FOR ASSEMBLY OF A ROTOR BLADE

    SÖDERIN GEIR / OLIVEGREN DAVID / DÖLERUD ERIK | Europäisches Patentamt | 2022

    Freier Zugriff

    ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    ROBERGE GARY D | Europäisches Patentamt | 2023

    Freier Zugriff

    ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    ROBERGE GARY D | Europäisches Patentamt | 2023

    Freier Zugriff

    ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

    ROBERGE GARY D | Europäisches Patentamt | 2023

    Freier Zugriff
    Nach oben