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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 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

    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 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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    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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      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 ...

      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 ...

      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 ...

      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 | 2021
      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 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. ...

    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 ...

    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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    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

    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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      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 | 2020

      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 | 2019

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

       ...

      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

       ...

    HEAT EXCHANGER FOR A GAS TURBINE ENGINE PROPULSION SYSTEM

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

    A propulsion system (14,16) including a gas turbine engine (20) and a nacelle (18) surrounding a portion of the gas turbine engine. The

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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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      HEAT EXCHANGER FOR A GAS TURBINE ENGINE PROPULSION SYSTEM

      Freier Zugriff
      PESYNA KENNETH M / SNYDER DOUGLAS J | Europäisches Patentamt | 2021

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

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    COOLING SYSTEM IN HYBRID ELECTRIC PROPULSION GAS TURBINE ENGINE

    Freier Zugriff
    SNYDER DOUGLAS J | Europäisches Patentamt | 2019

    A cooling system in a hybrid electric propulsion gas turbine engine is provided for cooling electrical components therein. The cooling

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      Cooling system in hybrid electric propulsion gas turbine engine

      Freier Zugriff
      SNYDER DOUGLAS J | Europäisches Patentamt | 2020

      A cooling system in a hybrid electric propulsion gas turbine engine is provided for cooling electrical components therein. The cooling

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    Gas turbine engine health determination

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

    GAS TURBINE ENGINE PERFORMANCE SEEKING CONTROL

    Freier Zugriff
    KHALID SYED JALALUDDIN | Europäisches Patentamt | 2022

    A gas turbine engine control system is disclosed having a model and an observer that together can be used to adjust a command issued to

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    COMPACT ACCESSORY SYSTEMS FOR A GAS TURBINE ENGINE

    Freier Zugriff
    ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2021

    An accessory system for a gas turbine engine having a driveshaft is provided. The accessory system includes a towershaft coupled to the

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      COMPACT ACCESSORY SYSTEMS FOR A GAS TURBINE ENGINE

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2017

      An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The accessory system includes a

       ...

      Compact accessory systems for a gas turbine engine

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2021

      An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The accessory system includes a

       ...

      COMPACT ACCESSORY SYSTEMS FOR A GAS TURBINE ENGINE

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2020

      An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The accessory system includes a

       ...

      COMPACT ACCESSORY SYSTEMS FOR A GAS TURBINE ENGINE

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2021

      An accessory system for a gas turbine engine having a driveshaft is provided. The accessory system includes a towershaft coupled to the

       ...

      Compact accessory systems for a gas turbine engine

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2020

      An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The accessory system includes a

       ...

      Compact accessory systems for a gas turbine engine

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2022

      An accessory system for a gas turbine engine having a driveshaft is provided. The accessory system includes a towershaft coupled to the

       ...

      Compact accessory systems for a gas turbine engine

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2022

      An accessory system for a gas turbine engine having a driveshaft is provided. The accessory system includes a towershaft coupled to the

       ...

      COMPACT ACCESSORY SYSTEMS FOR A GAS TURBINE ENGINE

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVES ROCIO | Europäisches Patentamt | 2020

      An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The accessory system includes a

       ...

      Compact accessory systems for a gas turbine engine

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2021

      An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The accessory system includes a

       ...

      COMPACT ACCESSORY SYSTEMS FOR A GAS TURBINE ENGINE

      Freier Zugriff
      ALSTAD SHAWN / DOBOSZ TOMASZ / CHAVEZ ROCIO | Europäisches Patentamt | 2018

      An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The accessory system includes a

       ...

    WANDS FOR GAS TURBINE ENGINE CLEANING

    Freier Zugriff
    GRIFFITHS GEORGE F / HEGGERE PRAHLAD R D / GREEN JEFFREY A | Europäisches Patentamt | 2022

    Wands are used as parts of cleaning systems to conduct cleaning agents into gas turbine engine cores. Wands according to the present

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      Wands for gas turbine engine cleaning

      Freier Zugriff
      GRIFFITHS GEORGE F / HEGGERE PRAHLAD R D / GREEN JEFFREY A | Europäisches Patentamt | 2020

      Wands are used as parts of cleaning systems to conduct cleaning agents into gas turbine engine cores. Wands according to the present

       ...

      Wands for gas turbine engine cleaning

      Freier Zugriff
      GRIFFITHS GEORGE F / HEGGERE PRAHLAD R D / GREEN JEFFREY A | Europäisches Patentamt | 2017

      Wands are used as parts of cleaning systems to conduct cleaning agents into gas turbine engine cores. Wands according to the present

       ...

    Practical Techniques for Modeling Gas Turbine Engine Performance

    Chapman, Jeffryes W. / Lavelle, Thomas M. / Litt, Jonathan S. | AIAA | 2016

    VARIABLE DRIVE GAS TURBINE ENGINE

    Freier Zugriff
    BRADBROOK STEPHEN JOHN | Europäisches Patentamt | 2016

    A system and method for variable drive of a propeller or fan of a gas turbine engine. The gas turbine engine has a combustor and a

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    TWO-PART GAS TURBINE ENGINE

    Freier Zugriff
    ROLT ANDREW | Europäisches Patentamt | 2016

    A gas turbine engine propulsion system (10) in which a first propulsive unit (12) has a core engine (42,44,46) and a first low pressure

     ...

    Bayesian Hierarchical Models for aerospace gas turbine engine prognostics

    Zaidan, Martha A. / Harrison, Robert F. / Mills, Andrew R. et al. | Tema Archiv | 2015
    to perform probabilistic estimation of remaining useful life for civil aerospace gas turbine engines. The paper establishes a Bayesian ...
    Schlagwörter: Gasturbine