Steven B. Johnson

Person

Stuart, FL, US

People

Patents Grantslast 30 patents

Information Patent Grant
Engine mount system for a gas turbine engine
- Patent number 11,731,773
- Issue date Aug 22, 2023
- Raytheon Technologies Corporation
- Gabriel L. Suciu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine with low stage count low pressure turbine and en...
- Patent number 11,286,883
- Issue date Mar 29, 2022
- Raytheon Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with low stage count low pressure turbine
- Patent number 10,451,004
- Issue date Oct 22, 2019
- United Technologies Corporation
- Gabriel L. Suciu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine compressor arrangement
- Patent number 8,807,477
- Issue date Aug 19, 2014
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with low stage count low pressure turbine
- Patent number 8,800,914
- Issue date Aug 12, 2014
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with low stage count low pressure turbine
- Patent number 8,695,920
- Issue date Apr 15, 2014
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine compressor arrangement
- Patent number 8,684,303
- Issue date Apr 1, 2014
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with low stage count low pressure turbine
- Patent number 8,511,604
- Issue date Aug 20, 2013
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with low stage count low pressure turbine
- Patent number 8,511,605
- Issue date Aug 20, 2013
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rear hub cooling for high pressure compressor
- Patent number 8,459,040
- Issue date Jun 11, 2013
- United Technologies Corporation
- Jorn A. Glahn
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine compressor arrangement
- Patent number 8,448,895
- Issue date May 28, 2013
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Engine mount system for a turbofan gas turbine engine
- Patent number 8,267,349
- Issue date Sep 18, 2012
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rear hub cooling for high pressure compressor
- Patent number 8,256,229
- Issue date Sep 4, 2012
- United Technologies Corporation
- Jorn A. Glahn
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Engine mount system for a turbofan gas turbine engine
- Patent number 8,128,021
- Issue date Mar 6, 2012
- United Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine afterburner
- Patent number 5,685,142
- Issue date Nov 11, 1997
- United Technologies Corporation
- Keith S. Brewer
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Engine exhaust nozzle seal
- Patent number 5,683,034
- Issue date Nov 4, 1997
- United Technologies Corporation
- Bradley C. Johnson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Engine exhaust nozzle seal
- Patent number 5,667,140
- Issue date Sep 16, 1997
- United Technologies Corporation
- Steven B. Johnson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Damper for augmentor liners
- Patent number 5,201,887
- Issue date Apr 13, 1993
- United Technologies Corporation
- Raymond J. Bruchez
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE
- Publication number 20240076050
- Publication date Mar 7, 2024
- Raytheon Technologies Corporation
- Gabriel L. Suciu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINES HAVING CRYOGENIC FUEL SYSTEMS
- Publication number 20220195928
- Publication date Jun 23, 2022
- Raytheon Technologies Corporation
- Steven B. Johnson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE
- Publication number 20210372349
- Publication date Dec 2, 2021
- Raytheon Technologies Corporation
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20200284222
- Publication date Sep 10, 2020
- Gabriel L. Suciu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20170058830
- Publication date Mar 2, 2017
- United Technologies Corporation
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20160097304
- Publication date Apr 7, 2016
- Gabriel L. Suciu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20160047268
- Publication date Feb 18, 2016
- Gabriel L. Suciu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20160032828
- Publication date Feb 4, 2016
- United Technologies Corporation
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20160024957
- Publication date Jan 28, 2016
- Gabriel L. Suciu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20160024958
- Publication date Jan 28, 2016
- Gabriel L. Suciu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20150315977
- Publication date Nov 5, 2015
- United Technologies Corporation
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20150300207
- Publication date Oct 22, 2015
- United Technologies Corporation
- Gabriel L. Suciu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20140174056
- Publication date Jun 26, 2014
- United Technologies Corporation
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20130014490
- Publication date Jan 17, 2013
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20130014489
- Publication date Jan 17, 2013
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
REAR HUB COOLING FOR HIGH PRESSURE COMPRESSOR
- Publication number 20120282079
- Publication date Nov 8, 2012
- Jorn A. Glahn
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
- Publication number 20120233982
- Publication date Sep 20, 2012
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
- Publication number 20120198816
- Publication date Aug 9, 2012
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20120198817
- Publication date Aug 9, 2012
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
- Publication number 20120198815
- Publication date Aug 9, 2012
- Gabriel L. Suciu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
- Publication number 20120121390
- Publication date May 17, 2012
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ENGINE MOUNT SYSTEM FOR A TURBOFAN GAS TURBINE ENGINE
- Publication number 20120099963
- Publication date Apr 26, 2012
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
REAR HUB COOLING FOR HIGH PRESSURE COMPRESSOR
- Publication number 20110247344
- Publication date Oct 13, 2011
- Jorn A. Glahn
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
ENGINE MOUNT SYSTEM FOR A TURBOFAN GAS TURBINE ENGINE
- Publication number 20090314881
- Publication date Dec 24, 2009
- Gabriel L. Suciu
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Steven B. Johnson

Person

Patents Grantslast 30 patents

Engine mount system for a gas turbine engine

Gas turbine engine with low stage count low pressure turbine and en...

Gas turbine engine with low stage count low pressure turbine

Gas turbine engine compressor arrangement

Gas turbine engine with low stage count low pressure turbine

Gas turbine engine with low stage count low pressure turbine

Gas turbine engine compressor arrangement

Gas turbine engine with low stage count low pressure turbine

Gas turbine engine with low stage count low pressure turbine

Rear hub cooling for high pressure compressor

Gas turbine engine compressor arrangement

Engine mount system for a turbofan gas turbine engine

Rear hub cooling for high pressure compressor

Engine mount system for a turbofan gas turbine engine

Gas turbine engine afterburner

Engine exhaust nozzle seal

Engine exhaust nozzle seal

Damper for augmentor liners

Patents Applicationslast 30 patents

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

GAS TURBINE ENGINES HAVING CRYOGENIC FUEL SYSTEMS

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

REAR HUB COOLING FOR HIGH PRESSURE COMPRESSOR

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

ENGINE MOUNT SYSTEM FOR A TURBOFAN GAS TURBINE ENGINE

REAR HUB COOLING FOR HIGH PRESSURE COMPRESSOR

ENGINE MOUNT SYSTEM FOR A TURBOFAN GAS TURBINE ENGINE