the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust

Patents Grantslast 30 patents

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    Turbine engine gearbox

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    • RTX Corporation
    • Michael E. McCune
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    Compressor flowpath

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    • RTX Corporation
    • Lisa I. Brilliant
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    Offset cores for gas turbine engines

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    • RTX Corporation
    • Gabriel L. Suciu
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    • RTX Corporation
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    • G06 - COMPUTING CALCULATING COUNTING
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    • Rohr, Inc.
    • Timothy Gormley
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    • Timothy Deryck Stone
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    Aircraft propulsion assembly comprising two adjacent engines, of wh...

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    Hybrid propulsion systems

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    • Rolls-Royce North American Technologies, Inc.
    • Stephen Andrew Long
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    Turbofan with offset gas generator and auxiliary power core

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    • RTX Corporation
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    • General Electric Company
    • Randy M. Vondrell
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    Offset cores for gas turbine engines

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    • RTX Corporation
    • Gabriel L. Suciu
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    Aeronautic propulsion system with low leakage rate and improved pro...

    • Patent number 11,802,515
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    • SAFRAN AIRCRAFT ENGINES
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    Bleed flow assembly for a gas turbine engine

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    • Brandon Wayne Miller
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    Shaft bearing positioning in a gas turbine engine

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    • Rolls-Royce PLC
    • Jillian C Gaskell
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    Compressor flowpath

    • Patent number 11,725,670
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    • Raytheon Technologies Corporation
    • Lisa I. Brilliant
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    Generalized jet-effect and generalized generator

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    • SOLITON HOLDINGS CORPORATION, DELAWARE CORPORATION
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    • Sarah Qureshi
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    • Patent number 11,585,293
    • Issue date Feb 21, 2023
    • Raytheon Technologies Corporation
    • Gabriel L. Suciu
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    Gas turbine engine cooling system

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    • Rolls-Royce PLC
    • Manuel Diaz Brito
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    Gas turbine engine shaft bearing configuration

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    • Issue date Jan 31, 2023
    • Raytheon Technologies Corporation
    • Brian D. Merry
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    Compact low-pressure compressor

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    • Issue date Jan 10, 2023
    • General Electric Company
    • Vinod Shashikant Chaudhari
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    Inducer assembly for a turbine engine

    • Patent number 11,541,340
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    • General Electric Company
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    Turbine engine gearbox

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    • Raytheon Technologies Corporation
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    Compound helicopters having auxiliary propulsive systems

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    • Raytheon Technologies Corporation
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Patents Applicationslast 30 patents

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    BYPASS TURBOFAN INCLUDING A SYSTEM FOR BLOCKING THE SECONDARY FLOW...

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    • Airbus Operations SAS
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    Propulsion System for an Aircraft

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    • GENERAL ELECTRIC COMPANY
    • Randy M. Vondrell
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    Propulsor Fan

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    • Whisper Aero Inc.
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    THRUST VECTORING EXHAUST NOZZLE FOR AIRCRAFT PROPULSION SYSTEM

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    • Paul R. Hanrahan
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    SHAFT BEARING POSITIONING IN A GAS TURBINE ENGINE

    • Publication number 20230349327
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    • Rolls-Royce plc
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    COMPRESSOR FLOWPATH

    • Publication number 20230332622
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    • Raytheon Technologies Corporation
    • Lisa I. Brilliant
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    LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE

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    • Raytheon Technologies Corporation
    • Bruce L. Morin
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    BLEED FLOW ASSEMBLY FOR A GAS TURBINE ENGINE

    • Publication number 20230228214
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    • GENERAL ELECTRIC COMPANY
    • Brandon Wayne Miller
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    SYSTEM AND METHOD FOR AIR COOLING FUEL PURGE FLOW

    • Publication number 20230228217
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    • GENERAL ELECTRIC COMPANY
    • George Frederick Frey
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    BLEED FLOW ASSEMBLY FOR A GAS TURBINE ENGINE

    • Publication number 20230228213
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    • GENERAL ELECTRIC COMPANY
    • Brandon Wayne Miller
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    BLEED FLOW ASSEMBLY FOR A GAS TURBINE ENGINE

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    • GENERAL ELECTRIC COMPANY
    • Brandon Wayne Miller
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    COMPRESSOR FLOWPATH

    • Publication number 20230131276
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    • Lisa I. Brilliant
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    TURBINE ENGINE GEARBOX

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    • Michael E. McCune
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    • SAFRAN AIRCRAFT ENGINES
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    AERONAUTIC PROPULSION SYSTEM WITH LOW LEAKAGE RATE AND IMPROVED PRO...

    • Publication number 20230019277
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    • SAFRAN AIRCRAFT ENGINES
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    GAS TURBINE ENGINE

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    • ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
    • Moritz WIRTH
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    DRIVE SYSTEM FOR TRANSLATING STRUCTURE

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    • Rohr, Inc.
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    HYBRID PROPULSION SYSTEMS

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    • Rolls-Royce North American Technologies, Inc.
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    GEAR TRAIN FOR GAS GEARED GAS TURBINE ENGINE

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    • Raytheon Technologies Corporation
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    SHAFT BEARING POSITIONING IN A GAS TURBINE ENGINE

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    • Rolls-Royce plc
    • Jillian C GASKELL
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    • GENERAL ELECTRIC COMPANY
    • Pranav Kamat
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    • Purdue Research Foundation
    • Qili Liu
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    GEARED TURBOFAN ENGINE GEARBOX ARRANGEMENT

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    • Frederick M. Schwarz
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    • Raytheon Technologies Corporation
    • Gabriel L. Suciu
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
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    • Sarah Qureshi
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    ENGINE

    • Publication number 20210270209
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    • ISRAEL AEROSPACE INDUSTRIES LTD
    • Aviad BRANDSTEIN
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    • ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
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