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    Restarting a gas turbine engine

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    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 ...

    SYSTEMS AND METHODS FOR DETERMINING GAS TURBINE ENGINE OPERATING MARGINS

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    DROLET MARTIN | Europäisches Patentamt | 2024

    A system (10) for a gas turbine engine (20) includes an engine control system (22). The engine control system (22) includes a processor

     ...

      SYSTEMS AND METHODS FOR DETERMINING GAS TURBINE ENGINE OPERATING MARGINS

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      DROLET MARTIN | Europäisches Patentamt | 2024

      A system for a gas turbine engine includes an engine control system. The engine control system includes a processor in communication

       ...

      SYSTEMS AND METHODS FOR DETERMINING GAS TURBINE ENGINE OPERATING MARGINS

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      DROLET MARTIN | Europäisches Patentamt | 2024

      A system for a gas turbine engine (20) includes an engine control system (22). The engine control system (22) includes a processor (62

       ...

    Descent operation for an aircraft parallel hybrid gas turbine engine propulsion system

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    LENTS CHARLES E / STAUBACH JOSEPH B / HARDIN LARRY W et al. | Europäisches Patentamt | 2024

    A gas turbine engine includes a core having a compressor section with a first compressor and a second compressor, a turbine section with

     ...

      DESCENT OPERATION FOR AN AIRCRAFT PARALLEL HYBRID GAS TURBINE ENGINE PROPULSION SYSTEM

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      LENTS CHARLES E / STAUBACH JOSEPH B / HARDIN LARRY W et al. | Europäisches Patentamt | 2022

      A gas turbine engine includes a core having a compressor section with a first compressor and a second compressor, a turbine section with

       ...

    METHODS AND APPARATUS FOR MOUNTING A GAS TURBINE ENGINE

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    CLINE MICHAEL / COLEMAN JONATHAN E / HIGGINS CRAIG W et al. | Europäisches Patentamt | 2024

    Methods, apparatus, systems and articles of manufacture are disclosed. An apparatus for mounting a gas turbine engine to a pylon, the

     ...

      METHODS AND APPARATUS FOR MOUNTING A GAS TURBINE ENGINE

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      CLINE MICHAEL / COLEMAN JONATHAN E / HIGGINS CRAIG W et al. | Europäisches Patentamt | 2022

      Methods, apparatus, systems and articles of manufacture are disclosed. An apparatus for mounting a gas turbine engine (100, 1100, 1200

       ...

      METHODS AND APPARATUS FOR MOUNTING A GAS TURBINE ENGINE

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      CLINE MICHAEL / COLEMAN JONATHAN E / HIGGINS CRAIG W et al. | Europäisches Patentamt | 2023

      Methods, apparatus, systems and articles of manufacture are disclosed. An apparatus for mounting a gas turbine engine to a pylon, the

       ...

    Accuracy of the gas turbine engine dynamic model self-tuning

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    Sergiy Yepifanov / Oleksii Bondarenko | DOAJ | 2024
    forming dynamic mathematical models (MM) of gas turbine engines using real data for the subsequent use of these models to solve problems related ...

    SYSTEMS AND METHODS FOR IDENTIFYING A CONDITION OF GAS TURBINE ENGINE SEALS

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    MARCHAND NICOLAS / WONG VELDA / FARVARDIN EHSAN et al. | Europäisches Patentamt | 2024

    An assembly for an aircraft propulsion system includes a case assembly, at least one seal, a first pressure sensor, and a computing

     ...

    METHOD AND SYSTEM FOR LIMITING POWER OF A GAS TURBINE ENGINE

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    LAMARRE SYLVAIN / LOPEZ SIMON / DES ROCHES-DIONNE NICOLAS et al. | Europäisches Patentamt | 2024

    Systems and methods for limiting power of a gas turbine engine (10) for an aircraft are described herein. A blade angle of a propeller

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    Gas turbine engine communication data management function communicating via aircraft wireless gateway

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    SCHEID PAUL RAYMOND / POSNIAK JASON E | Europäisches Patentamt | 2024

      GAS TURBINE ENGINE COMMUNICATION DATA MANAGEMENT FUNCTION COMMUNICATING VIA AIRCRAFT WIRELESS GATEWAY

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      SCHEID PAUL RAYMOND / POSNIAK JASON E | Europäisches Patentamt | 2022

    Modelling width of the spectral component of a gas-turbine engine gearbox output shaft speed

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    A. E. Sundukov / E. V. Shakhmatov | DOAJ | 2024
    Gearbox is the most stressed component in an aircraft gas-turbine engine. This implies the need for finding ways to monitor its technical ...
    Schlagwörter: gas-turbine engine

    METHODS AND APPARATUS TO PRODUCE HYDROGEN GAS TURBINE PROPULSION

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    BRADY DAVID JUSTIN / GERNONE MIRKO / GIBSON NATHAN E | Europäisches Patentamt | 2023

    Methods and apparatus to produce hydrogen gas turbine propulsion are disclosed. An example apparatus to produce propulsion in a gas

     ...

      METHODS AND APPARATUS TO PRODUCE HYDROGEN GAS TURBINE PROPULSION

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      BRADY DAVID JUSTIN / GERNONE MIRKO / GIBSON NATHAN E | Europäisches Patentamt | 2024

      Methods and apparatus to produce hydrogen gas turbine propulsion are disclosed. An example apparatus to produce propulsion in a gas

       ...

      Methods and apparatus to produce hydrogen gas turbine propulsion

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      BRADY DAVID JUSTIN / GERNONE MIRKO / GIBSON NATHAN E | Europäisches Patentamt | 2024

      Methods and apparatus to produce hydrogen gas turbine propulsion are disclosed. An example apparatus to produce propulsion in a gas

       ...

    HYBRID PROPULSION SYSTEMS WITH POWER SHARING

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    TRAWICK DAVID RUSSELL | Europäisches Patentamt | 2024
    forward propulsion of the aircraft; a gas turbine engine configured to drive the propulsor; an electrical machine configured to generate, for ...

      HYBRID PROPULSION SYSTEMS WITH POWER SHARING

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      TRAWICK DAVID RUSSELL | Europäisches Patentamt | 2024
      forward propulsion of the aircraft; a gas turbine engine configured to drive the propulsor; an electrical machine configured to generate, for ...

      HYBRID PROPULSION SYSTEMS WITH POWER SHARING

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      TRAWICK DAVID RUSSELL | Europäisches Patentamt | 2024
      forward propulsion of the aircraft; a gas turbine engine configured to drive the propulsor; an electrical machine configured to generate, for ...

    HYBRID PROPULSION SYSTEMS WITH POWER SHARING

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    TARWICK DAVID RUSSELL | Europäisches Patentamt | 2024
    to provide forward propulsion of the aircraft; a gas turbine engine (30A) configured to drive the propulsor (32A); an electrical machine (26A ...

    DISTRIBUTED PROPULSION WITH OFFSET PROPULSION MODULES

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    GONIDEC PATRICK / AGUIRRE MIGUEL ANGEL / DUPLAA SÉBASTIEN et al. | Europäisches Patentamt | 2024

    A propulsion unit including: a gas generator including a compressor, a combustion chamber, a turbine, at least two compressed-air

     ...

      DISTRIBUTED PROPULSION WITH OFFSET PROPULSION MODULES

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      GONIDEC PATRICK / AGUIRRE MIGUEL ANGEL / DUPLAA SÉBASTIEN et al. | Europäisches Patentamt | 2024

      A propulsion unit including: a gas generator including a compressor, a combustion chamber, a turbine, at least two compressed-air

       ...

    Aircraft hybrid propulsion system

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    SWANN PETER / BRITCHFORD KEVIN M | Europäisches Patentamt | 2024

    An aircraft hybrid propulsion system (5) comprising an inboard gas turbine engine (10a, 10c) and an outboard gas turbine engine (10b

     ...

      AIRCRAFT HYBRID PROPULSION SYSTEM

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      SWANN PETER / BRITCHFORD KEVIN M | Europäisches Patentamt | 2023

      An aircraft hybrid propulsion system (5) comprising an inboard gas turbine engine (10a, 10c) and an outboard gas turbine engine (10b

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      Aircraft hybrid propulsion system

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      SWANN PETER | Europäisches Patentamt | 2022
      ) includes a gas turbine engine (10) coupled to a generator (28, 32), a propeller (12) coupled to an electric motor (28), and an electrical storage ...

      AIRCRAFT HYBRID PROPULSION SYSTEM

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      SWANN PETER / BRITCHFORD KEVIN | Europäisches Patentamt | 2024

      An aircraft hybrid propulsion system (5) comprising an inboard gas turbine engine (10a, 10c) and an outboard gas turbine engine (10b

       ...

    AIRCRAFT PROPULSION SYSTEM

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    SWANN PETER | Europäisches Patentamt | 2023

    An aircraft propulsion system includes first and second engines and first and second electrical machines coupled to the first and second

     ...

      Aircraft propulsion system

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      SWANN PETER / BRITCHFORD KEVIN M | Europäisches Patentamt | 2024
      gas turbine engine such that the overall propulsion system produces a minimum overall noise level and meets the required overall propulsion ...

      AIRCRAFT PROPULSION SYSTEM

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      SWANN PETER / BRITCHFORD KEVIN | Europäisches Patentamt | 2024
      each aircraft gas turbine engine such that the overall propulsion system produces a minimum overall noise level and meets the required overall ...

      AIRCRAFT PROPULSION SYSTEM

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      SWANN PETER / HOLT JONATHAN E | Europäisches Patentamt | 2022

      An aircraft propulsion system includes a hydrocarbon fuel store, a hydrogen fuel store, an engine system capable of producing thrust by

       ...

    AIRCRAFT PROPULSION SYSTEM

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    YANG JINGBIN | Europäisches Patentamt | 2024

    An oil system for an aircraft propulsion system. The aircraft propulsion system comprises a motor configured to drive a propulsor via a

     ...

    ensemble de Propulsion

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    CAPASSO VALERIO / GLEMAREC GUILLAUME | Europäisches Patentamt | 2024

    PROPULSION SYSTEM ARCHITECTURE

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    SCHOLL NATHANIEL BLAKE | Europäisches Patentamt | 2024

    An aircraft propulsion system having a variable airflow capture area is provided. The propulsion system includes a main propulsion

     ...

      PROPULSION SYSTEM ARCHITECTURE

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      SCHOLL NATHANIEL BLAKE | Europäisches Patentamt | 2024

      An aircraft propulsion system having a variable airflow capture area is provided. The propulsion system includes a main propulsion

       ...

    PROPULSION SYSTEM ARCHITECTURE

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    OSTDIEK DAVID MARION / STUART ALAN ROY / NIERGARTH DANIEL ALAN et al. | Europäisches Patentamt | 2021
    ; dividing the second stream of air into a core stream and a fan stream; and directing the core stream into a gas turbine engine core. ...

      Propulsion system architecture

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      OSTDIEK DAVID MARION / STUART ALAN ROY / NIERGARTH DANIEL ALAN et al. | Europäisches Patentamt | 2024
      ; dividing the second stream of air into a core stream and a fan stream; and directing the core stream into a gas turbine engine core. ...

    AIRCRAFT PROPULSION SYSTEM GEARTRAIN

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    HANRAHAN PAUL R / MYLREA BENJAMIN T / STACHOWIAK DAVID A | Europäisches Patentamt | 2024
    ). The rotating structure (68) includes a turbine rotor (60). The rotating structure (68) is configured to drive rotation of the first propulsor ...

      AIRCRAFT PROPULSION SYSTEM GEARTRAIN

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      HANRAHAN PAUL R / MYLREA BENJAMIN T / STACHOWIAK DAVID A | Europäisches Patentamt | 2024

      AIRCRAFT PROPULSION SYSTEM GEARTRAIN

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      HANRAHAN PAUL R / STACHOWIAK DAVID A | Europäisches Patentamt | 2024
      coupled to the first ring gear (100) and includes a turbine rotor (60). The rotating structure (68) is configured to drive rotation of the first ...

      AIRCRAFT PROPULSION SYSTEM GEARTRAIN

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      HANRAHAN PAUL R / STACHOWIAK DAVID A | Europäisches Patentamt | 2024
      structure is coupled to the first ring gear and includes a turbine rotor. The rotating structure is configured to drive rotation of the first ...

      AIRCRAFT PROPULSION SYSTEM GEARTRAIN

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      HANRAHAN PAUL R | Europäisches Patentamt | 2024