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FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F05Engines, pumps F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS F05D2250/00Geometry

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Patents Grantslast 30 patents

Information Patent Grant
Turbomachine blade with improved cooling holes
- Patent number 12,123,318
- Issue date Oct 22, 2024
- SAFRAN AIRCRAFT ENGINES
- Guillaume Klein
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Inner ring for a turbomachine, vane ring with an inner ring, turbom...
- Patent number 11,098,603
- Issue date Aug 24, 2021
- MTU Aero Engines AG
- Lothar Albers
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Inlet screen for aircraft engines
- Patent number 11,084,599
- Issue date Aug 10, 2021
- General Electric Company Polska sp. z o.o.
- Tomasz Iglewski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine airfoil with large thickness properties
- Patent number 11,078,793
- Issue date Aug 3, 2021
- Raytheon Technologies Corporation
- Wolfgang Balzer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Monolithic body including an internal passage with a generally tear...
- Patent number 11,021,963
- Issue date Jun 1, 2021
- Raytheon Technologies Corporation
- Lawrence A. Binek
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Gas turbine engine airfoil with large thickness properties
- Patent number 10,508,549
- Issue date Dec 17, 2019
- United Technologies Corporation
- Wolfgang Balzer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Fastener cover for flowpath fasteners
- Patent number 10,502,133
- Issue date Dec 10, 2019
- General Electric Company
- Richa Awasthi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Hybrid exhaust nozzle
- Patent number 10,443,539
- Issue date Oct 15, 2019
- Rolls-Royce North American Technologies Inc.
- Von D. Baker
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine turbine blade tip cooling
- Patent number 10,436,039
- Issue date Oct 8, 2019
- United Technologies Corporation
- Brooks E. Snyder
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Creep resistant axial ring seal
- Patent number 10,408,074
- Issue date Sep 10, 2019
- United Technologies Corporation
- Brian C. McLaughlin
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Aircraft nozzle with a variable nozzle area of a second flow path
- Patent number 10,371,093
- Issue date Aug 6, 2019
- Rolls-Royce North American Technologies Inc.
- Von D. Baker
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Vane assembly including two- and three-dimensional arrangements of...
- Patent number 10,006,301
- Issue date Jun 26, 2018
- United Technologies Corporation
- John D. Riehl
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Grant
Inlet premixer for combustion apparatus
- Patent number 8,726,666
- Issue date May 20, 2014
- Donald W. Kendrick
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Combustion cavity layouts for fuel staging in trapped vortex combus...
- Patent number 8,689,562
- Issue date Apr 8, 2014
- Donald W. Kendrick
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Vortex premixer for combustion apparatus
- Patent number 8,689,561
- Issue date Apr 8, 2014
- Donald W. Kendrick
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method of fuel staging in combustion apparatus
- Patent number 8,549,862
- Issue date Oct 8, 2013
- Lean Flame, Inc.
- Donald W. Kendrick
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine components with improved film cooling
- Patent number 8,529,193
- Issue date Sep 10, 2013
- Honeywell International Inc.
- Jyothishkumar Venkataramanan
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Airfoil leading edge shape tailoring to reduce heat load
- Patent number 8,439,644
- Issue date May 14, 2013
- United Technologies Corporation
- Jason L. O'Hearn
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Airfoil attachment
- Patent number 8,206,118
- Issue date Jun 26, 2012
- United Technologies Corporation
- Tracy A. Propheter-Hinckley
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Convertible ejector selectively cooled thrust vectoring exhaust nozzle
- Patent number 5,680,755
- Issue date Oct 28, 1997
- General Electric Company
- Thomas A. Hauer
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
INTERMEDIATE CASING FOR A GAS TURBINE ENGINE
- Publication number 20230220786
- Publication date Jul 13, 2023
- SAFRAN AIRCRAFT ENGINES
- Paul Antoine FORESTO
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
MONOLITHIC BODY INCLUDING AN INTERNAL PASSAGE WITH A GENERALLY TEAR...
- Publication number 20200347728
- Publication date Nov 5, 2020
- Lawrence A. Binek
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE AIRFOIL WITH LARGE THICKNESS PROPERTIES
- Publication number 20200141244
- Publication date May 7, 2020
- United Technologies Corporation
- Wolfgang Balzer
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
INNER RING FOR A TURBOMACHINE, VANE RING WITH AN INNER RING, TURBOM...
- Publication number 20190277148
- Publication date Sep 12, 2019
- MTU Aero Engines AG
- Lothar Albers
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOMACHINE BLADE WITH IMPROVED COOLING HOLES
- Publication number 20190071981
- Publication date Mar 7, 2019
- SAFRAN AIRCRAFT ENGINES
- Guillaume KLEIN
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
FASTENER COVER FOR FLOWPATH FASTENERS
- Publication number 20180355796
- Publication date Dec 13, 2018
- GENERAL ELECTRIC COMPANY
- Richa Awasthi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
SPLINE FOR A TURBINE ENGINE
- Publication number 20180340437
- Publication date Nov 29, 2018
- GENERAL ELECTRIC COMPANY
- Robert Charles Groves
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
FILM HOLE ARRANGEMENT FOR A TURBINE ENGINE
- Publication number 20180230812
- Publication date Aug 16, 2018
- GENERAL ELECTRIC COMPANY
- Junwoo Lim
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
MANUFACTURE OF COMPONENT WITH COOLING CHANNELS
- Publication number 20170008086
- Publication date Jan 12, 2017
- Rolls-Royce plc
- Simon L JONES
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
GAS TURBINE ENGINE TURBINE BLADE TIP COOLING
- Publication number 20160265366
- Publication date Sep 15, 2016
- Brooks E. Snyder
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
GAS TURBINE ENGINE AIRFOIL WITH LARGE THICKNESS PROPERTIES
- Publication number 20150354365
- Publication date Dec 10, 2015
- United Technologies Corporation
- Wolfgang Balzer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
STRUT AIRFOIL DESIGN FOR LOW SOLIDITY EXHAUST GAS DIFFUSER
- Publication number 20120198810
- Publication date Aug 9, 2012
- General Electric Company, a New York Corporation
- Asif Iqbal Ansari
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE COMPONENTS WITH IMPROVED FILM COOLING
- Publication number 20110123312
- Publication date May 26, 2011
- Honeywell International Inc.
- Jyothishkumar Venkataramanan
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
COMBUSTION CAVITY LAYOUTS FOR FUEL STAGING IN TRAPPED VORTEX COMBUS...
- Publication number 20110061392
- Publication date Mar 17, 2011
- Donald W. Kendrick
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
VORTEX PREMIXER FOR COMBUSTION APPARATUS
- Publication number 20110061391
- Publication date Mar 17, 2011
- Donald W. Kendrick
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
METHOD OF FUEL STAGING IN COMBUSTION APPARATUS
- Publication number 20110061395
- Publication date Mar 17, 2011
- Donald W. Kendrick
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
INLET PREMIXER FOR COMBUSTION APPARATUS
- Publication number 20110061390
- Publication date Mar 17, 2011
- Donald W. Kendrick
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
AIRFOIL ATTACHMENT
- Publication number 20100284816
- Publication date Nov 11, 2010
- Tracy A. Propheter-Hinckley
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRFOIL LEADING EDGE SHAPE TAILORING TO REDUCE HEAT LOAD
- Publication number 20090148299
- Publication date Jun 11, 2009
- Jason L. O'Hearn
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Two-dimensional

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Turbomachine blade with improved cooling holes

Inner ring for a turbomachine, vane ring with an inner ring, turbom...

Inlet screen for aircraft engines

Gas turbine engine airfoil with large thickness properties

Monolithic body including an internal passage with a generally tear...

Gas turbine engine airfoil with large thickness properties

Fastener cover for flowpath fasteners

Hybrid exhaust nozzle

Gas turbine engine turbine blade tip cooling

Creep resistant axial ring seal

Aircraft nozzle with a variable nozzle area of a second flow path

Vane assembly including two- and three-dimensional arrangements of...

Inlet premixer for combustion apparatus

Combustion cavity layouts for fuel staging in trapped vortex combus...

Vortex premixer for combustion apparatus

Method of fuel staging in combustion apparatus

Gas turbine engine components with improved film cooling

Airfoil leading edge shape tailoring to reduce heat load

Airfoil attachment

Convertible ejector selectively cooled thrust vectoring exhaust nozzle

Patents Applicationslast 30 patents

INTERMEDIATE CASING FOR A GAS TURBINE ENGINE

MONOLITHIC BODY INCLUDING AN INTERNAL PASSAGE WITH A GENERALLY TEAR...

GAS TURBINE ENGINE AIRFOIL WITH LARGE THICKNESS PROPERTIES

INNER RING FOR A TURBOMACHINE, VANE RING WITH AN INNER RING, TURBOM...

TURBOMACHINE BLADE WITH IMPROVED COOLING HOLES

FASTENER COVER FOR FLOWPATH FASTENERS

SPLINE FOR A TURBINE ENGINE

FILM HOLE ARRANGEMENT FOR A TURBINE ENGINE

MANUFACTURE OF COMPONENT WITH COOLING CHANNELS

GAS TURBINE ENGINE TURBINE BLADE TIP COOLING

GAS TURBINE ENGINE AIRFOIL WITH LARGE THICKNESS PROPERTIES

STRUT AIRFOIL DESIGN FOR LOW SOLIDITY EXHAUST GAS DIFFUSER

GAS TURBINE ENGINE COMPONENTS WITH IMPROVED FILM COOLING

COMBUSTION CAVITY LAYOUTS FOR FUEL STAGING IN TRAPPED VORTEX COMBUS...

VORTEX PREMIXER FOR COMBUSTION APPARATUS

METHOD OF FUEL STAGING IN COMBUSTION APPARATUS

INLET PREMIXER FOR COMBUSTION APPARATUS

AIRFOIL ATTACHMENT

AIRFOIL LEADING EDGE SHAPE TAILORING TO REDUCE HEAT LOAD