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Dmitriy B. SIDELKOVSKIY

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  • Ellington, CT, US
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Patents Grantslast 30 patents

  • Information Patent Grant

    After-fan system with electrical motor for gas turbine engines
    • Patent number 12,123,309
    • Issue date Oct 22, 2024
    • RTX Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    After-fan system for a gas turbine engine
    • Patent number 11,994,089
    • Issue date May 28, 2024
    • RTX Corporation
    • Dmitriy B. Sidelkovskiy
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    After-fan system with electrical motor for gas turbine engines
    • Patent number 11,846,196
    • Issue date Dec 19, 2023
    • RTX Corporation
    • Dmitriy B. Sidelkovskiy
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    High bypass ratio engine bypass duct nozzle with controlled nozzle...
    • Patent number 11,585,294
    • Issue date Feb 21, 2023
    • Raytheon Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Nacelle
    • Patent number 11,548,652
    • Issue date Jan 10, 2023
    • Raytheon Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Nacelle
    • Patent number 11,408,369
    • Issue date Aug 9, 2022
    • Raytheon Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Convergent divergent exit nozzle for a gas turbine engine
    • Patent number 11,236,701
    • Issue date Feb 1, 2022
    • Raytheon Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Turbofan with motorized rotating inlet guide vane
    • Patent number 11,085,371
    • Issue date Aug 10, 2021
    • Raytheon Technologies Corporation
    • Daniel Bernard Kupratis
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Nacelle
    • Patent number 11,046,445
    • Issue date Jun 29, 2021
    • Raytheon Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Gas turbine engine bypass drainage systems
    • Patent number 11,028,779
    • Issue date Jun 8, 2021
    • Raytheon Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Method for separated flow detection
    • Patent number 11,027,827
    • Issue date Jun 8, 2021
    • Raytheon Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Nacelle
    • Patent number 10,767,596
    • Issue date Sep 8, 2020
    • Raytheon Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Multi-shaft gas turbine engine
    • Patent number 10,738,710
    • Issue date Aug 11, 2020
    • Rolls-Royce Corporation
    • Dmitriy B. Sidelkovskiy
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Turbofan with motorized rotating inlet guide vane
    • Patent number 10,738,694
    • Issue date Aug 11, 2020
    • United Technologies Corporation
    • Daniel Bernard Kupratis
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Grant

    Track fairing assembly for a turbine engine nacelle
    • Patent number 10,450,898
    • Issue date Oct 22, 2019
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Fan flutter suppression system
    • Patent number 10,422,280
    • Issue date Sep 24, 2019
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Convergent divergent exit nozzle for a gas turbine engine
    • Patent number 10,371,092
    • Issue date Aug 6, 2019
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Multi-shaft gas turbine engine
    • Patent number 9,611,788
    • Issue date Apr 4, 2017
    • Rolls-Royce Corporation
    • Dmitriy B. Sidelkovskiy
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Nacelle bifurcation for gas turbine engine
    • Patent number 9,249,731
    • Issue date Feb 2, 2016
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

  • Information Patent Application

    METHOD OF INLET DISTORTION PREDICTION AND MONITORING
    • Publication number 20250003835
    • Publication date Jan 2, 2025
    • Raytheon Technologies Corporation
    • Dmitriy Sidelkovskiy
    • G08 - SIGNALLING
  • Information Patent Application

    AFTER-FAN SYSTEM WITH ELECTRICAL MOTOR FOR GAS TURBINE ENGINES
    • Publication number 20240035392
    • Publication date Feb 1, 2024
    • RTX Corporation
    • Dmitriy B. Sidelkovskiy
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    NACELLE
    • Publication number 20220063823
    • Publication date Mar 3, 2022
    • RAYTHEON TECHNOLOGIES CORPORATION
    • DMITRIY B. SIDELKOVSKIY
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    HIGH BYPASS RATIO ENGINE BYPASS DUCT NOZZLE WITH CONTROLLED NOZZLE...
    • Publication number 20210262415
    • Publication date Aug 26, 2021
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    AFTER-FAN SYSTEM WITH ELECTRICAL MOTOR FOR GAS TURBINE ENGINES
    • Publication number 20210262359
    • Publication date Aug 26, 2021
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    NACELLE
    • Publication number 20200408169
    • Publication date Dec 31, 2020
    • Raytheon Technologies Corporation
    • DMITRIY B. SIDELKOVSKIY
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    AFTER-FAN SYSTEM FOR A GAS TURBINE ENGINE
    • Publication number 20200325852
    • Publication date Oct 15, 2020
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    GAS TURBINE ENGINE BYPASS DRAINAGE SYSTEMS
    • Publication number 20200248628
    • Publication date Aug 6, 2020
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    METHOD FOR SEPARATED FLOW DETECTION
    • Publication number 20200070962
    • Publication date Mar 5, 2020
    • United Technologies Corporation
    • DMITRIY B. SIDELKOVSKIY
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    TURBOFAN WITH MOTORIZED ROTATING INLET GUIDE VANE
    • Publication number 20200063657
    • Publication date Feb 27, 2020
    • United Technologies Corporation
    • Daniel Bernard Kupratis
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    NACELLE
    • Publication number 20190031356
    • Publication date Jan 31, 2019
    • UNITED TECHNOLOGIES CORPORATION
    • DMITRIY B. SIDELKOVSKIY
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    NACELLE
    • Publication number 20190031357
    • Publication date Jan 31, 2019
    • UNITED TECHNOLOGIES CORPORATION
    • DMITRIY B. SIDELKOVSKIY
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    CONVERGENT DIVERGENT EXIT NOZZLE FOR A GAS TURBINE ENGINE
    • Publication number 20190017470
    • Publication date Jan 17, 2019
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    FAN FLUTTER SUPPRESSION SYSTEM
    • Publication number 20180258854
    • Publication date Sep 13, 2018
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    MULTI-SHAFT GAS TURBINE ENGINE
    • Publication number 20170159571
    • Publication date Jun 8, 2017
    • Rolls-Royce Corporation
    • Dmitriy B. SIDELKOVSKIY
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    TRACK FAIRING ASSEMBLY FOR A TURBINE ENGINE NACELLE
    • Publication number 20160237856
    • Publication date Aug 18, 2016
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Application

    CONVERGENT DIVERGENT EXIT NOZZLE FOR A GAS TURBINE ENGINE
    • Publication number 20160195038
    • Publication date Jul 7, 2016
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    MULTI-SHAFT GAS TURBINE ENGINE
    • Publication number 20140250860
    • Publication date Sep 11, 2014
    • Rolls-Royce Corporation
    • Dmitriy B. SIDELKOVSKIY
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    Gas Turbine Engine Assembly Including A Thrust Reverser
    • Publication number 20140216005
    • Publication date Aug 7, 2014
    • United Technologies Corporation
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    NACELLE BIFURCATION FOR GAS TURBINE ENGINE
    • Publication number 20130319002
    • Publication date Dec 5, 2013
    • Dmitriy B. Sidelkovskiy
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS