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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
Turbine engine having a compressor with an inducer
- Patent number 12,305,535
- Issue date May 20, 2025
- General Electric Company
- Antonio Guijarro Valencia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with fluid circuit and ejector
- Patent number 11,885,240
- Issue date Jan 30, 2024
- General Electric Company Polska sp. z o.o.
- Tomasz Edward Berdowski
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
De-icing device for an air intake of an aircraft turbojet engine na...
- Patent number 11,879,390
- Issue date Jan 23, 2024
- SAFRAN NACELLES
- Thierry Jacques Albert Le Docte
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Segmented augmented turbine assembly
- Patent number 11,773,736
- Issue date Oct 3, 2023
- ORGANOWORLD INC.
- Frederick Churchill
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Aircraft propulsion system exhaust nozzle with ejector passage(s)
- Patent number 11,754,018
- Issue date Sep 12, 2023
- Rohr, Inc.
- Timothy Gormley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Convergent-divergent flap pair for a variable-geometry turbojet eng...
- Patent number 11,739,712
- Issue date Aug 29, 2023
- SAFRAN AIRCRAFT ENGINES
- François Leglaye
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Convergent-divergent flap pair for a variable-geometry turbojet eng...
- Patent number 11,713,730
- Issue date Aug 1, 2023
- SAFRAN AIRCRAFT ENGINES
- Thierry Kohn
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Last chance screen for aircraft fuel system
- Patent number 11,702,989
- Issue date Jul 18, 2023
- Hamilton Sundstrand Corporation
- Murtuza Lokhandwalla
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
2D variable-area plug nozzle
- Patent number 11,661,905
- Issue date May 30, 2023
- Florida Turbine Technologies, Inc.
- Robert A. Ress
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Compressor bleed apparatus for a turbine engine
- Patent number 11,635,030
- Issue date Apr 25, 2023
- General Electric Company
- Stephen Raymond Donnelly
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
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
Generalized jet-effect and fluid-repellent corpus
- Patent number 11,499,525
- Issue date Nov 15, 2022
- Yuri Abramov
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Grant
Gas turbine engine inlet
- Patent number 11,480,104
- Issue date Oct 25, 2022
- Raytheon Technologies Corporation
- Yuan J. Qiu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nozzle of a turbomachine provided with chevrons with a non-axisymme...
- Patent number 11,274,632
- Issue date Mar 15, 2022
- SAFRAN AIRCRAFT ENGINES
- Jonathan Langridge
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine component with cooling aperture having shaped inlet and...
- Patent number 11,220,918
- Issue date Jan 11, 2022
- Honeywell International Inc.
- Jeff Howe
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Gas turbine component with cooling aperture having shaped inlet and...
- Patent number 11,208,900
- Issue date Dec 28, 2021
- Honeywell International Inc.
- Jeff Howe
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Turbocharger
- Patent number 11,199,220
- Issue date Dec 14, 2021
- BMTS TECHNOLOGY GMBH & CO. KG
- Martin Berger
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle of a gas turbine engine
- Patent number 11,187,186
- Issue date Nov 30, 2021
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag Todorovic
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Centrifugal compressor with diffuser with throat
- Patent number 11,125,235
- Issue date Sep 21, 2021
- Cummins Ltd.
- Subenuka Sivagnanasundaram
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Acoustic liners with oblique cellular structures
- Patent number 11,059,559
- Issue date Jul 13, 2021
- General Electric Company
- Richard David Cedar
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Supply duct of a compressor of a turbine engine
- Patent number 11,047,303
- Issue date Jun 29, 2021
- SAFRAN AIRCRAFT ENGINES
- Jacky Novi Mardjono
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Turbomachine airfoil
- Patent number 10,830,072
- Issue date Nov 10, 2020
- General Electric Company
- Jason Edward Albert
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine component with cooling aperture having shaped inlet and...
- Patent number 10,830,052
- Issue date Nov 10, 2020
- Honeywell International Inc.
- Jeff Howe
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Variable thickness core for gas turbine engine component
- Patent number 10,815,827
- Issue date Oct 27, 2020
- Raytheon Technologies Corporation
- Anthony B. Swift
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Impingement holes for a turbine engine component
- Patent number 10,815,789
- Issue date Oct 27, 2020
- General Electric Company
- Ronald Scott Bunker
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Convergent-divergent nozzle mechanism
- Patent number 10,815,932
- Issue date Oct 27, 2020
- Raytheon Technologies Corporation
- Brandon T. Slaney
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine airfoil component platform seal cooling
- Patent number 10,794,207
- Issue date Oct 6, 2020
- RATHEON TECHNOLOGIES CORPORATION
- Matthew Andrew Hough
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine assembly
- Patent number 10,738,700
- Issue date Aug 11, 2020
- General Electric Company
- Thomas Fauner
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Diffuser for a turbine engine and method of forming same
- Patent number 10,704,423
- Issue date Jul 7, 2020
- General Electric Company
- Deepesh D. Nanda
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbocharger
- Patent number 10,670,071
- Issue date Jun 2, 2020
- BMTS Technology GmbH & Co. KG
- Martin Berger
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...

Patents Applicationslast 30 patents

Information Patent Application
TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER
- Publication number 20240229658
- Publication date Jul 11, 2024
- GENERAL ELECTRIC COMPANY
- Antonio Guijarro Valencia
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER
- Publication number 20240133303
- Publication date Apr 25, 2024
- GENERAL ELECTRIC COMPANY
- Antonio Guijarro Valencia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
LAST CHANCE SCREEN FOR AIRCRAFT FUEL SYSTEM
- Publication number 20230098079
- Publication date Mar 30, 2023
- HAMILTON SUNDSTRAND CORPORATION
- Murtuza Lokhandwalla
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CARTRIDGE TIP FOR TURBOMACHINE COMBUSTOR
- Publication number 20230022306
- Publication date Jan 26, 2023
- GENERAL ELECTRIC COMPANY
- Dana Morgan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SEGMENTED AUGMENTED TURBINE ASSEMBLY
- Publication number 20220389824
- Publication date Dec 8, 2022
- ORGANOWORLD INC.
- Frederick CHURCHILL
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE WITH FLUID CIRCUIT AND EJECTOR
- Publication number 20220372885
- Publication date Nov 24, 2022
- General Electric Company Polska sp. z o.o
- Tomasz Edward Berdowski
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...
- Publication number 20220290631
- Publication date Sep 15, 2022
- SAFRAN AIRCRAFT ENGINES
- Thierry KOHN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...
- Publication number 20220275771
- Publication date Sep 1, 2022
- SAFRAN AIRCRAFT ENGINES
- François LEGLAYE
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
DE-ICING DEVICE FOR AN AIR INTAKE OF AN AIRCRAFT TURBOJET ENGINE NA...
- Publication number 20220170418
- Publication date Jun 2, 2022
- SAFRAN NACELLES
- Thierry Jacques Albert Le Docte
- 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
HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING...
- Publication number 20200392853
- Publication date Dec 17, 2020
- GENERAL ELECTRIC COMPANY
- Benjamin Paul Lacy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THRUST NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT
- Publication number 20200332741
- Publication date Oct 22, 2020
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Turbocharger
- Publication number 20200256380
- Publication date Aug 13, 2020
- BMTS Technology GmbH & Co. KG
- Martin Berger
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
CONVERGENT-DIVERGENT NOZZLE MECHANISM
- Publication number 20190345894
- Publication date Nov 14, 2019
- United Technologies Corporation
- Brandon T. Slaney
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NOZZLE OF A TURBOMACHINE PROVIDED WITH CHEVRONS WITH A NON-AXISYMME...
- Publication number 20190234345
- Publication date Aug 1, 2019
- SAFRAN AIRCRAFT ENGINES
- Jonathan Langridge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CENTRIFUGAL COMPRESSOR WITH DIFFUSER WITH THROAT
- Publication number 20190219057
- Publication date Jul 18, 2019
- Cummins Ltd.
- Subenuka Sivagnanasundaram
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
COMBUSTOR LINER PANEL WITH A MULTIPLE OF HEAT TRANSFER RIBS FOR A G...
- Publication number 20190041059
- Publication date Feb 7, 2019
- United Technologies Corporation
- Thomas N. Slavens
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
SUPPLY DUCT OF A COMPRESSOR OF A TURBINE ENGINE
- Publication number 20190024586
- Publication date Jan 24, 2019
- SAFRAN AIRCRAFT ENGINES
- Jacky Novi MARDJONO
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONVERGENT-DIVERGENT NOZZLE FOR A TURBOFAN ENGINE OF A SUPERSONIC A...
- Publication number 20180245540
- Publication date Aug 30, 2018
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
CONVERGENT-DIVERGENT NOZZLE
- Publication number 20160305368
- Publication date Oct 20, 2016
- Rolls-Royce plc
- Zahid M HUSSAIN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COOLING PASSAGES FOR TURBINE BUCKETS OF A GAS TURBINE ENGINE
- Publication number 20140286771
- Publication date Sep 25, 2014
- GENERAL ELECTRIC COMPANY
- Benjamin Paul Lacy
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
CASING COOLING DUCT
- Publication number 20140234073
- Publication date Aug 21, 2014
- Kevin Moreton
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE COMPONENT HAVING COOLING PASSAGES WITH VARYING DIAMETER
- Publication number 20140161625
- Publication date Jun 12, 2014
- GENERAL ELECTRIC COMPANY
- Xiuzhang James Zhang
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOFAN ENGINE WITH CONVERGENT - DIVERGENT EXHAUST NOZZLE
- Publication number 20140130503
- Publication date May 15, 2014
- Cor Leep
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REFLEX ANNULAR VENT NOZZLE
- Publication number 20140037443
- Publication date Feb 6, 2014
- Wasif Khan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COMBUSTOR TRANSITION DUCT ASSEMBLY WITH INNER LINER
- Publication number 20140010644
- Publication date Jan 9, 2014
- Richard C. Charron
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE AIRFOIL TRAILING EDGE BIFURCATED COOLING HOLES
- Publication number 20130302177
- Publication date Nov 14, 2013
- Robert Frederick Bergholz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
ASYMMETRICALLY SHAPED TRAILING EDGE COOLING HOLES
- Publication number 20130302178
- Publication date Nov 14, 2013
- Robert Frederick Bergholz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
METHOD FOR DEFINING THE SHAPE OF A TURBOMACHINE CONVERGENT-DIVERGEN...
- Publication number 20130206865
- Publication date Aug 15, 2013
- SNECMA
- Julien SZYDLOWSKI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND METHOD FOR COOLING TURBINE BLADES
- Publication number 20130177446
- Publication date Jul 11, 2013
- GENERAL ELECTRIC COMPANY
- Aaron Ezekiel Smith
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Turbine engine having a compressor with an inducer

Gas turbine engine with fluid circuit and ejector

De-icing device for an air intake of an aircraft turbojet engine na...

Segmented augmented turbine assembly

Aircraft propulsion system exhaust nozzle with ejector passage(s)

Convergent-divergent flap pair for a variable-geometry turbojet eng...

Convergent-divergent flap pair for a variable-geometry turbojet eng...

Last chance screen for aircraft fuel system

2D variable-area plug nozzle

Compressor bleed apparatus for a turbine engine

High bypass ratio engine bypass duct nozzle with controlled nozzle...

Generalized jet-effect and fluid-repellent corpus

Gas turbine engine inlet

Nozzle of a turbomachine provided with chevrons with a non-axisymme...

Gas turbine component with cooling aperture having shaped inlet and...

Gas turbine component with cooling aperture having shaped inlet and...

Turbocharger

Exhaust nozzle of a gas turbine engine

Centrifugal compressor with diffuser with throat

Acoustic liners with oblique cellular structures

Supply duct of a compressor of a turbine engine

Turbomachine airfoil

Gas turbine component with cooling aperture having shaped inlet and...

Variable thickness core for gas turbine engine component

Impingement holes for a turbine engine component

Convergent-divergent nozzle mechanism

Gas turbine engine airfoil component platform seal cooling

Turbine assembly

Diffuser for a turbine engine and method of forming same

Turbocharger

Patents Applicationslast 30 patents

TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER

TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER

LAST CHANCE SCREEN FOR AIRCRAFT FUEL SYSTEM

CARTRIDGE TIP FOR TURBOMACHINE COMBUSTOR

SEGMENTED AUGMENTED TURBINE ASSEMBLY

GAS TURBINE ENGINE WITH FLUID CIRCUIT AND EJECTOR

CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...

CONVERGENT-DIVERGENT FLAP PAIR FOR A VARIABLE-GEOMETRY TURBOJET ENG...

DE-ICING DEVICE FOR AN AIR INTAKE OF AN AIRCRAFT TURBOJET ENGINE NA...

HIGH BYPASS RATIO ENGINE BYPASS DUCT NOZZLE WITH CONTROLLED NOZZLE...

HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING...

THRUST NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT

Turbocharger

CONVERGENT-DIVERGENT NOZZLE MECHANISM

NOZZLE OF A TURBOMACHINE PROVIDED WITH CHEVRONS WITH A NON-AXISYMME...

CENTRIFUGAL COMPRESSOR WITH DIFFUSER WITH THROAT

COMBUSTOR LINER PANEL WITH A MULTIPLE OF HEAT TRANSFER RIBS FOR A G...

SUPPLY DUCT OF A COMPRESSOR OF A TURBINE ENGINE

CONVERGENT-DIVERGENT NOZZLE FOR A TURBOFAN ENGINE OF A SUPERSONIC A...

CONVERGENT-DIVERGENT NOZZLE

COOLING PASSAGES FOR TURBINE BUCKETS OF A GAS TURBINE ENGINE

CASING COOLING DUCT

TURBINE COMPONENT HAVING COOLING PASSAGES WITH VARYING DIAMETER

TURBOFAN ENGINE WITH CONVERGENT - DIVERGENT EXHAUST NOZZLE

REFLEX ANNULAR VENT NOZZLE

COMBUSTOR TRANSITION DUCT ASSEMBLY WITH INNER LINER

TURBINE AIRFOIL TRAILING EDGE BIFURCATED COOLING HOLES

ASYMMETRICALLY SHAPED TRAILING EDGE COOLING HOLES

METHOD FOR DEFINING THE SHAPE OF A TURBOMACHINE CONVERGENT-DIVERGEN...

SYSTEM AND METHOD FOR COOLING TURBINE BLADES