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    Gas turbine engine

    Freier Zugriff
    ANDREA MINELLI | Europäisches Patentamt | 2023

    A gas turbine engine 10 for an aircraft has hydraulic actuators, a fuel circuit 50 with a high and low 53 pressure pump and a fuel

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    GAS TURBINE ENGINE

    Freier Zugriff
    KANAKHIN YURIJ ALEKSANDROVICH / KUPRIK VIKTOR VIKTOROVICH / MARCHUKOV EVGENIJ YUVENALEVICH et al. | Europäisches Patentamt | 2019
    systems and discharge compressor, and drain system is communicated with flow part of gas turbine engine. Self-contained power supply via ...

    Gas turbine engine systems

    Freier Zugriff
    BROUGHTON PAUL / PEACE RICHARD / SKINNER GARY ALAN et al. | Europäisches Patentamt | 2017

    A gas turbine engine 10 comprises at least one rigid raft assembly that has a fluid passageway 210 at least partially embedded therein

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    Gas Turbine Engine Heaters

    Freier Zugriff
    BOYCE BENJAMIN J / ABBOTT MICHAEL T | Europäisches Patentamt | 2023

    An engine heater system for supplying compressed air to an air brake of a vehicle. The engine heater system including a gas turbine. A

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    Gas Turbine Engine Part

    Freier Zugriff
    BROUGHTON PAUL / PEACE RICHARD / SKINNER GARY et al. | Europäisches Patentamt | 2019
    systems/components embedded in the electrical raft (200). The raft map (400) may be useful in assembly, repair and fault diagnosis, for example. ...

    PROPULSION SYSTEM ARRANGEMENT FOR TURBOFAN GAS TURBINE ENGINE

    Freier Zugriff
    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | Europäisches Patentamt | 2022

    An integrated propulsion system according to an example of the present disclosure includes, among other things, a fan section, a gas

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    Restarting a gas turbine engine

    Freier Zugriff
    GARETH E MOORE / PAUL R DAVIES / STEPHEN M HUSBAND et al. | Europäisches Patentamt | 2024
    turbine engine 110 of such power and propulsion systems 100 during flight are provided. One such aircraft power and propulsion system 100 ...

    Propulsion system arrangement for turbofan gas turbine engine

    Freier Zugriff
    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | Europäisches Patentamt | 2021
    a gas turbine engine, a nacelle assembly and a mounting assembly, the system designed by a process comprising identifying two or more of ...

    Propulsion system arrangement for turbofan gas turbine engine

    Freier Zugriff
    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | Europäisches Patentamt | 2023

    An integrated propulsion system according to an example of the present disclosure includes, among other things, a fan section, a gas

     ...

    PROPULSION SYSTEM ARRANGEMENT FOR TURBOFAN GAS TURBINE ENGINE

    Freier Zugriff
    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | Europäisches Patentamt | 2020
    a gas turbine engine, a nacelle assembly and a mounting assembly, the system designed by a process comprising identifying two or more of ...

    GAS TURBINE ENGINE NOISE REDUCTION

    Freier Zugriff
    RAMAKRISHNAN KISHORE / WOOD TREVOR HOWARD / CAFARO STEFAN JOSEPH et al. | Europäisches Patentamt | 2023

    Systems and methods for controlling an unducted turbofan engine to limit noise. The unducted turbofan engine may include an unducted fan

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    Propulsion system arrangement for turbofan gas turbine engine

    Freier Zugriff
    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | Europäisches Patentamt | 2018
    engine and a nacelle assembly together in an interactive process, the engine including a turbine section configured to drive a fan section and a ...

    GAS TURBINE ENGINE FAN BLADE CONTAINMENT SYSTEMS

    Freier Zugriff
    FRACCHIA CARLOS ANGELO / JOST KAREN M / HIGGINS MARK DAVID et al. | Europäisches Patentamt | 2022

    Gas turbine engine fan blade containment systems are disclosed. An example fan blade containment system includes a shield to be coupled

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    GAS TURBINE ENGINE FAN BLADE CONTAINMENT SYSTEMS

    Freier Zugriff
    FRACCHIA CARLOS ANGELO / JOST KAREN M / HIGGINS MARK DAVID et al. | Europäisches Patentamt | 2021

    Gas turbine engine fan blade containment systems are disclosed. An example fan blade containment system includes a shield to be coupled

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    Gas Turbine Engine Behavioral Modeling

    Meyer, Richard T | Online Contents | 2015
    This paper develops and validates a power flow behavioral model of a gas turbine engine (GTE) composed of a gas generator and free power ...
    Schlagwörter: Gasturbine

    PROPULSION SYSTEM ARRANGEMENT FOR TURBOFAN GAS TURBINE ENGINE

    Freier Zugriff
    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | Europäisches Patentamt | 2018
    engine and a nacelle assembly together in an interactive process, the engine including a turbine section configured to drive a fan section and a ...

    Gas turbine engine fan blade containment systems

    Freier Zugriff
    FRACCHIA CARLOS ANGELO / JOST KAREN M / HIGGINS MARK DAVID et al. | Europäisches Patentamt | 2020

    Gas turbine engine fan blade containment systems are disclosed. An example fan blade containment system includes a shield to be coupled

     ...

    Gas turbine engine health determination

    Freier Zugriff
    SOARES JR ALVARO JOSE / MCKENNA DAVID JOSEPH / ASACK MARTA KATARZYNA | Europäisches Patentamt | 2018

    GAS TURBINE ENGINE FAN BLADE CONTAINMENT SYSTEMS

    Freier Zugriff
    FRACCHIA CARLOS ANGELO / JOST KAREN M / HIGGINS MARK DAVID et al. | Europäisches Patentamt | 2020

    The present invention relates to a gas turbine engine fan blade containment system including a shield (318) to be coupled to an aircraft

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    Heat exchanger for a gas turbine engine propulsion system

    Freier Zugriff
    PESYNA KENNETH M / SNYDER DOUGLAS J | Europäisches Patentamt | 2020

    A propulsion system including a gas turbine engine is disclosed herein. The propulsion system further includes a heat exchanger arranged

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