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Steven H. Zysman

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  • Amston, CT, US
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Patents Grantslast 30 patents

  • Information Patent Grant

    Composite skins having variable hole sizes and shapes formed using...
    • Patent number 12,109,793
    • Issue date Oct 8, 2024
    • RTX Corporation
    • Brian Kenneth Holland
    • G10 - MUSICAL INSTRUMENTS ACOUSTICS
  • Information Patent Grant

    Engine bleed air ducting into heat exchanger
    • Patent number 11,549,434
    • Issue date Jan 10, 2023
    • Raytheon Technologies Corporation
    • Steven H. Zysman
    • 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

    Environmental sampling system and method
    • Patent number 11,402,304
    • Issue date Aug 2, 2022
    • Raytheon Technologies Corporation
    • Joel H. Wagner
    • G01 - MEASURING TESTING
  • 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

    Engine bleed air ducting into heat exchanger
    • Patent number 11,078,837
    • Issue date Aug 3, 2021
    • Raytheon Technologies Corporation
    • Steven H. Zysman
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • 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

    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

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

    Engine wing
    • Patent number 10,730,635
    • Issue date Aug 4, 2020
    • Raytheon Technologies Corporation
    • Timothy S. Snyder
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Moveable exhaust plug liner
    • Patent number 10,570,852
    • Issue date Feb 25, 2020
    • United Technologies Corporation
    • Andre L. Bent
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Flow modulating airfoil apparatus
    • Patent number 10,557,416
    • Issue date Feb 11, 2020
    • United Technologies Corporation
    • Steven H. Zysman
    • F24 - HEATING RANGES VENTILATING
  • Information Patent Grant

    Fence for duct tone mitigation
    • Patent number 10,487,744
    • Issue date Nov 26, 2019
    • United Technologies Corporation
    • Keith A. Post
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Nacelle short inlet for fan blade removal
    • Patent number 10,479,519
    • Issue date Nov 19, 2019
    • United Technologies Corporation
    • Yuan J. Qiu
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • 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

    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

    Bypass duct with angled drag links
    • Patent number 10,060,390
    • Issue date Aug 28, 2018
    • United Technologies Corporation
    • Steven H. Zysman
    • Y10 - TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Information Patent Grant

    Passive boundary layer bleed system for nacelle inlet airflow control
    • Patent number 9,644,535
    • Issue date May 9, 2017
    • United Technologies Corporation
    • Steven H. Zysman
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Free stream intake with particle separator for reverse core engine
    • Patent number 9,644,537
    • Issue date May 9, 2017
    • United Technologies Corporation
    • Gabriel L Suciu
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Lightweight shrouded fan blade
    • Patent number 9,506,353
    • Issue date Nov 29, 2016
    • United Technologies Corporation
    • Frederick M. Schwarz
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Nacelle scoop inlet
    • Patent number 9,108,737
    • Issue date Aug 18, 2015
    • United Technologies Corporation
    • Steven H. Zysman
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Passive boundary layer bleed system for nacelle inlet airflow control
    • Patent number 8,844,553
    • Issue date Sep 30, 2014
    • United Technologies Corporation
    • Steven H. Zysman
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Passive boundary layer bleed system for nacelle inlet airflow control
    • Patent number 8,839,805
    • Issue date Sep 23, 2014
    • United Technologies Corporation
    • Steven H. Zysman
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Modulating flow through gas turbine engine cooling system
    • Patent number 8,490,382
    • Issue date Jul 23, 2013
    • United Technologies Corporation
    • Steven H. Zysman
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Grant

    Lubricant cooling exchanger dual intake duct
    • Patent number 7,658,060
    • Issue date Feb 9, 2010
    • United Technologies Corporation
    • Steven H. Zysman
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Grant

    Slotted bleed deflector for a gas turbine engine
    • Patent number 7,455,498
    • Issue date Nov 25, 2008
    • United Technologies Corporation
    • Steven H. Zysman
    • F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
  • Information Patent Grant

    Fluid mixer with an integral fluid capture ducts forming auxiliary...
    • Patent number 7,434,384
    • Issue date Oct 14, 2008
    • United Technologies Corporation
    • Wesley K. Lord
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Grant

    Bleed deflector for a gas turbine engine
    • Patent number 6,565,313
    • Issue date May 20, 2003
    • United Technologies Corporation
    • John P. Nikkanen
    • Y10 - TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Information Patent Grant

    Gas turbine engine jet noise suppressor
    • Patent number 6,487,848
    • Issue date Dec 3, 2002
    • United Technologies Corporation
    • Steven H. Zysman
    • B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

  • Information Patent Application

    COMPOSITE SKINS HAVING VARIABLE HOLE SIZES AND SHAPES FORMED USING...
    • Publication number 20240416640
    • Publication date Dec 19, 2024
    • RTX Corporation
    • Brian Kenneth Holland
    • B24 - GRINDING POLISHING
  • 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

    ENGINE BLEED AIR DUCTING INTO HEAT EXCHANGER
    • Publication number 20210363923
    • Publication date Nov 25, 2021
    • Raytheon Technologies Corporation
    • Steven H. Zysman
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • 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

    COMPOSITE SKINS HAVING VARIABLE HOLE SIZES AND SHAPES FORMED USING...
    • Publication number 20210158792
    • Publication date May 27, 2021
    • United Technologies Corporation
    • Brian Kenneth Holland
    • G10 - MUSICAL INSTRUMENTS ACOUSTICS
  • Information Patent Application

    ENVIRONMENTAL SAMPLING SYSTEM AND METHOD
    • Publication number 20210003485
    • Publication date Jan 7, 2021
    • United Technologies Corporation
    • Joel H. Wagner
    • G01 - MEASURING TESTING
  • 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

    ENGINE BLEED AIR DUCTING INTO HEAT EXCHANGER
    • Publication number 20200248620
    • Publication date Aug 6, 2020
    • United Technologies Corporation
    • Steven H. Zysman
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    BOUNDARY LAYER INGESTING FAN
    • Publication number 20200024982
    • Publication date Jan 23, 2020
    • United Technologies Corporation
    • Steven H. Zysman
    • B64 - AIRCRAFT AVIATION COSMONAUTICS
  • Information Patent Application

    MOVEABLE EXHAUST PLUG
    • Publication number 20190085789
    • Publication date Mar 21, 2019
    • United Technologies Corporation
    • Andre L. Bent
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • 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

    MOVEABLE EXHAUST PLUG
    • Publication number 20180355821
    • Publication date Dec 13, 2018
    • United Technologies Corporation
    • Andre L. Bent
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    FLOW MODULATING AIRFOIL APPARATUS
    • Publication number 20180355739
    • Publication date Dec 13, 2018
    • United Technologies Corporation
    • Steven H. Zysman
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • 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

    FENCE FOR DUCT TONE MITIGATION
    • Publication number 20170335771
    • Publication date Nov 23, 2017
    • United Technologies Corporation
    • Keith A. Post
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    NACELLE SHORT INLET FOR FAN BLADE REMOVAL
    • Publication number 20170190438
    • Publication date Jul 6, 2017
    • United Technologies Corporation
    • Yuan J. Qiu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    GAS TURBINE ENGINE WITH MINIMIZED INLET DISTORTION
    • Publication number 20170175626
    • Publication date Jun 22, 2017
    • United Technologies Corporation
    • Yuan J. Qiu
    • 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

    LIQUID SEPARATING AIR INLETS
    • Publication number 20160153363
    • Publication date Jun 2, 2016
    • United Technologies Corporation
    • Steven H. Zysman
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    PASSIVE BOUNDARY LAYER BLEED SYSTEM FOR NACELLE INLET AIRFLOW CONTROL
    • Publication number 20140321970
    • Publication date Oct 30, 2014
    • Steven H. Zysman
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    FREE STREAM INTAKE FOR REVERSE CORE ENGINE
    • Publication number 20140260182
    • Publication date Sep 18, 2014
    • United Technologies Corporation
    • Gabriel L. Suciu
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    LIGHTWEIGHT SHROUDED FAN BLADE
    • Publication number 20140169935
    • Publication date Jun 19, 2014
    • United Technologies Corporation
    • Frederick M. Schwarz
    • F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
  • Information Patent Application

    NACELLE SCOOP INLET
    • Publication number 20140053532
    • Publication date Feb 27, 2014
    • Steven H. Zysman
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    BYPASS DUCT WITH ANGLED DRAG LINKS
    • Publication number 20130219857
    • Publication date Aug 29, 2013
    • Steven H. Zysman
    • F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • Information Patent Application

    MODULATING FLOW THROUGH GAS TURBINE ENGINE COOLING SYSTEM
    • Publication number 20100180571
    • Publication date Jul 22, 2010
    • Steven H. Zysman
    • Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
  • Information Patent Application

    PASSIVE BOUNDARY LAYER BLEED SYSTEM FOR NACELLE INLET AIRFLOW CONTROL
    • Publication number 20100074739
    • Publication date Mar 25, 2010
    • Steven H. Zysman
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
  • Information Patent Application

    PASSIVE BOUNDARY LAYER BLEED SYSTEM FOR NACELLE INLET AIRFLOW CONTROL
    • Publication number 20090301095
    • Publication date Dec 10, 2009
    • Steven H. Zysman
    • F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...