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Wesley K. Lord

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  • South Glastonbury, CT, US
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Patents Grantslast 30 patents

  • Information Patent Grant

    Low pressure ratio fan engine having a dimensional relationship bet...
    • Patent number 11,781,447
    • Issue date Oct 10, 2023
    • RTX Corporation
    • Wesley K. Lord
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Grant

    Low pressure ratio fan engine having a dimensional relationship bet...
    • Patent number 11,781,505
    • Issue date Oct 10, 2023
    • RTX Corporation
    • Wesley K. Lord
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Grant

    Turbine section of gas turbine engine
    • Patent number 11,614,036
    • Issue date Mar 28, 2023
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Geared gas turbine engine with reduced fan noise
    • Patent number 11,512,631
    • Issue date Nov 29, 2022
    • Raytheon Technologies Corporation
    • Jonathan Gilson
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Turbine section of high bypass turbofan
    • Patent number 11,486,311
    • Issue date Nov 1, 2022
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Gas turbine engine inlet
    • Patent number 11,480,104
    • Issue date Oct 25, 2022
    • Raytheon Technologies Corporation
    • Yuan J. Qiu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Turbine section of high bypass turbofan
    • Patent number 11,480,108
    • Issue date Oct 25, 2022
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Turbine section of high bypass turbofan
    • Patent number 11,346,289
    • Issue date May 31, 2022
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Low pressure ratio fan engine having a dimensional relationship bet...
    • Patent number 11,286,811
    • Issue date Mar 29, 2022
    • Raytheon Technologies Corporation
    • Wesley K. Lord
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Turbine section of high bypass turbofan
    • Patent number 11,242,805
    • Issue date Feb 8, 2022
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Turbine section of high bypass turbofan
    • Patent number 11,215,123
    • Issue date Jan 4, 2022
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Turbine section of high bypass turbofan
    • Patent number 11,149,650
    • Issue date Oct 19, 2021
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Geared gas turbine engine with reduced fan noise
    • Patent number 11,118,507
    • Issue date Sep 14, 2021
    • Raytheon Technologies Corporation
    • Jonathan Gilson
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Low pressure ratio fan engine having a dimensional relationship bet...
    • Patent number 11,015,550
    • Issue date May 25, 2021
    • Raytheon Technologies Corporation
    • Wesley K. Lord
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Boundary layer cooling air for embedded engine
    • Patent number 10,934,938
    • Issue date Mar 2, 2021
    • Raytheon Technologies Corporation
    • Gabriel L. Suciu
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Transverse-mounted power turbine drive system
    • Patent number 10,830,129
    • Issue date Nov 10, 2020
    • Raytheon Technologies Corporation
    • Wesley K. Lord
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Intercooled cooling air with dual pass heat exchanger
    • Patent number 10,830,148
    • Issue date Nov 10, 2020
    • Raytheon Technologies Corporation
    • Gabriel L. Suciu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Turbine section of high bypass turbofan
    • Patent number 10,794,293
    • Issue date Oct 6, 2020
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Nacelle short inlet
    • Patent number 10,724,541
    • Issue date Jul 28, 2020
    • United Technologies Corporation
    • Yuan J. Qiu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Aft fan counter-rotating turbine engine
    • Patent number 10,723,470
    • Issue date Jul 28, 2020
    • Raytheon Technologies Corporation
    • Gabriel L. Suciu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Intercooled cooling air with dual pass heat exchanger
    • Patent number 10,718,268
    • Issue date Jul 21, 2020
    • Raytheon Technologies Corporation
    • Gabriel L. Suciu
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Variable-geometry boundary layer diverter
    • Patent number 10,718,272
    • Issue date Jul 21, 2020
    • United Technologies Corporation
    • Wesley K. Lord
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Turbine engine with guide vanes forward of its fan blades
    • Patent number 10,711,631
    • Issue date Jul 14, 2020
    • Raytheon Technologies Corporation
    • Gabriel L. Suciu
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Gas turbine engine with low fan noise
    • Patent number 10,704,415
    • Issue date Jul 7, 2020
    • Raytheon Technologies Corporation
    • Bruce L. Morin
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Turbine section of high bypass turbofan
    • Patent number 10,662,880
    • Issue date May 26, 2020
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Geared gas turbine engine with reduced fan noise
    • Patent number 10,655,538
    • Issue date May 19, 2020
    • United Technologies Corporation
    • Jonathan Gilson
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Grant

    Cross flow fan with exit guide vanes
    • Patent number 10,633,090
    • Issue date Apr 28, 2020
    • United Technologies Corporation
    • Wesley K. Lord
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Grant

    Heat exchanger for gas turbine engine
    • Patent number 10,563,585
    • Issue date Feb 18, 2020
    • United Technologies Corporation
    • Wesley K. Lord
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Gas turbine engine with low fan noise
    • Patent number 10,526,914
    • Issue date Jan 7, 2020
    • United Technologies Corporation
    • Bruce L. Morin
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Angled reverse core gas turbine engine with widened nozzle
    • Patent number 10,502,085
    • Issue date Dec 10, 2019
    • United Technologies Corporation
    • Wesley K. Lord
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

  • Information Patent Application

    Propulsor Fan
    • Publication number 20240003317
    • Publication date Jan 4, 2024
    • Whisper Aero Inc.
    • Gabriel L. Suciu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    TURBINE SECTION OF A GAS TURBINE ENGINE
    • Publication number 20230323836
    • Publication date Oct 12, 2023
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    GAS TURBINE ENGINE INLET
    • Publication number 20230025200
    • Publication date Jan 26, 2023
    • Raytheon Technologies Corporation
    • Yuan J. Qiu
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    TURBINE SECTION OF GAS TURBINE ENGINE
    • Publication number 20220074352
    • Publication date Mar 10, 2022
    • Paul R. Adams
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
    • Publication number 20220010689
    • Publication date Jan 13, 2022
    • Raytheon Technologies Corporation
    • Wesley K. Lord
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    GEARED GAS TURBINE ENGINE WITH REDUCED FAN NOISE
    • Publication number 20210372323
    • Publication date Dec 2, 2021
    • Raytheon Technologies Corporation
    • Jonathan Gilson
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    TURBINE SECTION OF HIGH BYPASS TURBOFAN
    • Publication number 20210301731
    • Publication date Sep 30, 2021
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    TURBINE SECTION OF HIGH BYPASS TURBOFAN
    • Publication number 20210301730
    • Publication date Sep 30, 2021
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
    • Publication number 20210285403
    • Publication date Sep 16, 2021
    • Raytheon Technologies Corporation
    • Wesley K. Lord
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Application

    TURBINE SECTION OF HIGH BYPASS TURBOFAN
    • Publication number 20210071587
    • Publication date Mar 11, 2021
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    TURBINE SECTION OF HIGH BYPASS TURBOFAN
    • Publication number 20210040898
    • Publication date Feb 11, 2021
    • Raytheon Technologies Corporation
    • Paul R. Adams
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    GEARED GAS TURBINE ENGINE WITH REDUCED FAN NOISE
    • Publication number 20200386154
    • Publication date Dec 10, 2020
    • Raytheon Technologies Corporation
    • Jonathan Gilson
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
    • Publication number 20200063603
    • Publication date Feb 27, 2020
    • United Technologies Corporation
    • Wesley K. Lord
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
    • Publication number 20200025036
    • Publication date Jan 23, 2020
    • United Technologies Corporation
    • Wesley K. Lord
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    TURBINE SECTION OF HIGH BYPASS TURBOFAN
    • Publication number 20190048803
    • Publication date Feb 14, 2019
    • United Technologies Corporation
    • Paul R. Adams
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    GEARED GAS TURBINE ENGINE WITH REDUCED FAN NOISE
    • Publication number 20190024581
    • Publication date Jan 24, 2019
    • United Technologies Corporation
    • Jonathan Gilson
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    TURBINE SECTION OF HIGH BYPASS TURBOFAN
    • Publication number 20190017445
    • Publication date Jan 17, 2019
    • United Technologies Corporation
    • Paul R. Adams
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    TURBINE SECTION OF HIGH BYPASS TURBOFAN
    • Publication number 20190017446
    • Publication date Jan 17, 2019
    • United Technologies Corporation
    • Paul R. Adams
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    AFT FAN COUNTER-ROTATING TURBINE ENGINE
    • Publication number 20180354637
    • Publication date Dec 13, 2018
    • United Technologies Corporation
    • Gabriel L. Suciu
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    VARIABLE-GEOMETRY BOUNDARY LAYER DIVERTER
    • Publication number 20180298829
    • Publication date Oct 18, 2018
    • United Technologies Corporation
    • Wesley K. Lord
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    INTERCOOLED COOLING AIR WITH DUAL PASS HEAT EXCHANGER
    • Publication number 20180258859
    • Publication date Sep 13, 2018
    • United Technologies Corporation
    • Gabriel L. Suciu
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
    • Publication number 20180209379
    • Publication date Jul 26, 2018
    • United Technologies Corporation
    • Wesley K. Lord
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
    • Publication number 20180163568
    • Publication date Jun 14, 2018
    • United Technologies Corporation
    • Wesley K. Lord
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    CROSS FLOW FAN FOR WIDE AIRCRAFT FUSELAGE
    • Publication number 20180155045
    • Publication date Jun 7, 2018
    • United Technologies Corporation
    • Gabriel L. Suciu
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    INTERCOOLED COOLING AIR WITH DUAL PASS HEAT EXCHANGER
    • Publication number 20180066587
    • Publication date Mar 8, 2018
    • United Technologies Corporation
    • Gabriel L. Suciu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    EXHAUST DUCT FOR TURBINE FORWARD OF FAN
    • Publication number 20180038315
    • Publication date Feb 8, 2018
    • United Technologies Corporation
    • Wesley K. Lord
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    BOUNDARY LAYER COOLING AIR FOR EMBEDDED ENGINE
    • Publication number 20180023474
    • Publication date Jan 25, 2018
    • United Technologies Corporation
    • Gabriel L. Suciu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    TURBINE SECTION OF HIGH BYPASS TURBOFAN
    • Publication number 20170298832
    • Publication date Oct 19, 2017
    • United Technologies Corporation
    • Paul R. Adams
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    NACELLE SHORT INLET
    • Publication number 20170298954
    • Publication date Oct 19, 2017
    • United Technologies Corporation
    • Yuan J. Qiu
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    CROSS FLOW FAN WITH EXIT GUIDE VANES
    • Publication number 20170267342
    • Publication date Sep 21, 2017
    • United Technologies Corporation
    • Wesley K. Lord
    • B64 - AIRCRAFT AVIATION COSMONAUTICS