Stuart S. Ochs

Person

Manchester, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Boundary layer ducted fan propulsion system
- Patent number 11,964,772
- Issue date Apr 23, 2024
- RTX Corporation
- Jon E. Sobanski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Diffuser for rotating detonation engine
- Patent number 11,591,101
- Issue date Feb 28, 2023
- Raytheon Technologies Corporation
- Christopher Britton Greene
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
System to promote accelerated boundary layer ingestion
- Patent number 11,124,291
- Issue date Sep 21, 2021
- Raytheon Technologies Corporation
- Neil Terwilliger
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active flow control for nacelle inlet
- Patent number 9,157,368
- Issue date Oct 13, 2015
- United Technologies Corporation
- Wayne Hurwitz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with low fan pressure ratio
- Patent number 8,459,035
- Issue date Jun 11, 2013
- United Technologies Corporation
- Peter G. Smith
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with variable geometry fan exit guide vane system
- Patent number 8,347,633
- Issue date Jan 8, 2013
- United Technologies Corporation
- Peter G. Smith
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Rotor hub fairing system for a counter-rotating, coaxial rotor system
- Patent number 7,530,787
- Issue date May 12, 2009
- Sikorsky Aircraft Corporation
- Fabio P. Bertolotti
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Ceramic matrix composite turbine engine vane
- Patent number 7,452,189
- Issue date Nov 18, 2008
- United Technologies Corporation
- Jun Shi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
BOUNDARY LAYER DUCTED FAN PROPULSION SYSTEM
- Publication number 20230242267
- Publication date Aug 3, 2023
- Raytheon Technologies Corporation
- Jon E. Sobanski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DIFFUSER FOR ROTATING DETONATION ENGINE
- Publication number 20210215098
- Publication date Jul 15, 2021
- United Technologies Corporation
- CHRISTOPHER BRITTON GREENE
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
SYSTEM TO PROMOTE ACCELERATED BOUNDARY LAYER INGESTION
- Publication number 20200189724
- Publication date Jun 18, 2020
- United Technologies Corporation
- Neil Terwilliger
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Active Regenerative Heating and Cooling
- Publication number 20170045258
- Publication date Feb 16, 2017
- Subramanyaravi Annapragada
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
GAS TURBINE ENGINE WITH IMPROVED FUEL EFFICIENCY
- Publication number 20150192298
- Publication date Jul 9, 2015
- United Technologies Corporation
- Karl L. Hasel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO
- Publication number 20150132106
- Publication date May 14, 2015
- United Technologies Corporation
- Peter G. Smith
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO
- Publication number 20120233981
- Publication date Sep 20, 2012
- Peter G. Smith
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE WITH GEARED ARCHITECTURE
- Publication number 20120222398
- Publication date Sep 6, 2012
- Peter G. Smith
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO
- Publication number 20120222397
- Publication date Sep 6, 2012
- Peter G. Smith
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE WITH IMPROVED FUEL EFFICIENCY
- Publication number 20120124964
- Publication date May 24, 2012
- Karl L. Hasel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE WITH VARIABLE GEOMETRY FAN EXIT GUIDE VANE SYSTEM
- Publication number 20090097967
- Publication date Apr 16, 2009
- Peter G. Smith
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
ACTIVE FLOW CONTROL FOR NACELLE INLET
- Publication number 20090060704
- Publication date Mar 5, 2009
- Wayne Hurwitz
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Ceramic matrix composite turbine engine vane
- Publication number 20070258811
- Publication date Nov 8, 2007
- United Technologies Corporation
- Jun Shi
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Rotor hub fairing system for a counter-rotating, coaxial rotor system
- Publication number 20070166163
- Publication date Jul 19, 2007
- Sikorsky Aircraft Corporation
- Fabio P. Bertolotti
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Stuart S. Ochs

Person

Patents Grantslast 30 patents

Boundary layer ducted fan propulsion system

Diffuser for rotating detonation engine

System to promote accelerated boundary layer ingestion

Active flow control for nacelle inlet

Gas turbine engine with low fan pressure ratio

Gas turbine engine with variable geometry fan exit guide vane system

Rotor hub fairing system for a counter-rotating, coaxial rotor system

Ceramic matrix composite turbine engine vane

Patents Applicationslast 30 patents

BOUNDARY LAYER DUCTED FAN PROPULSION SYSTEM

DIFFUSER FOR ROTATING DETONATION ENGINE

SYSTEM TO PROMOTE ACCELERATED BOUNDARY LAYER INGESTION

Active Regenerative Heating and Cooling

GAS TURBINE ENGINE WITH IMPROVED FUEL EFFICIENCY

GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO

GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO

GAS TURBINE ENGINE WITH GEARED ARCHITECTURE

GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO

GAS TURBINE ENGINE WITH IMPROVED FUEL EFFICIENCY

GAS TURBINE ENGINE WITH VARIABLE GEOMETRY FAN EXIT GUIDE VANE SYSTEM

ACTIVE FLOW CONTROL FOR NACELLE INLET

Ceramic matrix composite turbine engine vane

Rotor hub fairing system for a counter-rotating, coaxial rotor system