of the centripetal type

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CPC
F02C3/09

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FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02CGAS-TURBINE PLANTS AIR INTAKES FOR JET-PROPULSION PLANTS CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid

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F02C3/09of the centripetal type

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Patents Grantslast 30 patents

Information Patent Grant
Removable mechanical part for acoustic insulation of an air inlet c...
- Patent number 12,297,773
- Issue date May 13, 2025
- SAFRAN POWER UNITS
- Laurent Stéphane Tardy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft engine having two radially offset turbines
- Patent number 12,116,928
- Issue date Oct 15, 2024
- Pratt & Whitney Canada Corp.
- David Menheere
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet engine having fan blades with air and exhaust gas flow channels
- Patent number 11,313,326
- Issue date Apr 26, 2022
- Finn Schöning
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine auxiliary power unit
- Patent number 11,008,116
- Issue date May 18, 2021
- Pratt & Whitney Canada Corp.
- Andreas Eleftheriou
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Forward-swept impellers and gas turbine engines employing the same
- Patent number 9,970,452
- Issue date May 15, 2018
- Honeywell International Inc.
- Richard David Conner
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Bi-directional compression fan rotor for a gas turbine engine
- Patent number 9,915,199
- Issue date Mar 13, 2018
- United Technologies Corporation
- Sohail Mohammed
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Combined pump system for engine TMS AOC reduction and ECS loss elim...
- Patent number 9,470,153
- Issue date Oct 18, 2016
- United Technologies Corporation
- Gabriel L. Suciu
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Gas turbine fuel injector having flow guide for receiving air flow
- Patent number 9,404,422
- Issue date Aug 2, 2016
- Honeywell International Inc.
- Frank J. Zupanc
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Integrated gearless and nonlubricated auxiliary power unit
- Patent number 7,251,942
- Issue date Aug 7, 2007
- Honeywell International Inc.
- Kevin S. Dittmar
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Combined stage single shaft turbofan engine
- Patent number 7,055,306
- Issue date Jun 6, 2006
- Hamilton Sundstrand Corporation
- Anthony Jones
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Turbomachine with a vaneless rotating diffuser and nozzle
- Patent number 6,712,588
- Issue date Mar 30, 2004
- Onera (Office National D'Etudes et de Recherches Aerospatiales)
- Yves Ribaud
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Gas turbine engine with offset shroud
- Patent number 6,571,563
- Issue date Jun 3, 2003
- Honeywell Power Systems, Inc.
- Thomas K. Yim
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Advanced thermo-electronic systems for hybrid electric vehicles
- Patent number 6,282,897
- Issue date Sep 4, 2001
- Marius A. Paul
- B60 - VEHICLES IN GENERAL
Information Patent Grant
Bi-metallic tie-bolt for microturbine power generating system
- Patent number 6,276,124
- Issue date Aug 21, 2001
- AlliedSignal Inc.
- Jemeng Soh
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine
- Patent number 5,727,378
- Issue date Mar 17, 1998
- Great Lakes Helicopters Inc.
- Jeffrey L. Seymour
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine including a bearing support tube cantilevered fr...
- Patent number 5,526,640
- Issue date Jun 18, 1996
- Technical Directions, Inc.
- Vern E. Brooks
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbine nozzle cooling
- Patent number 5,280,703
- Issue date Jan 25, 1994
- Sundstrand Corporation
- John Corrado
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Volume enhanced turbine engine combustion zone
- Patent number 5,207,055
- Issue date May 4, 1993
- Sundstrand Corporation
- Jack R. Shekleton
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Volume enhanced turbine engine combustion zone
- Patent number 5,172,546
- Issue date Dec 22, 1992
- Sundstrand Corporation
- Jack R. Shekleton
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
High efficiency, twin spool, radial-high pressure, gas turbine engine
- Patent number 5,081,832
- Issue date Jan 21, 1992
- Mowill; Rolf Jan
- Rolf J. Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbocharger-gas turbine
- Patent number 4,936,097
- Issue date Jun 26, 1990
- Sundstrand Corporation
- Colin Rodgers
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Segmented seal plate for a turbine engine
- Patent number 4,932,207
- Issue date Jun 12, 1990
- Sundstrand Corporation
- Derek P. Harris
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3898793
- Patent number 3,898,793
- Issue date Aug 12, 1975
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3460806
- Patent number 3,460,806
- Issue date Aug 12, 1969
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3052096
- Patent number 3,052,096
- Issue date Sep 4, 1962
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
2804747
- Patent number 2,804,747
- Issue date Sep 3, 1957
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
2748568
- Patent number 2,748,568
- Issue date Jun 5, 1956
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
2651910
- Patent number 2,651,910
- Issue date Sep 15, 1953
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
2477683
- Patent number 2,477,683
- Issue date Aug 2, 1949
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
AIRCRAFT ENGINE HAVING TWO RADIALLY OFFSET TURBINES
- Publication number 20240309803
- Publication date Sep 19, 2024
- Pratt & Whitney Canada Corp.
- David MENHEERE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MULTISTAGE COMPRESSOR-EXPANDER TURBOMACHINE CONFIGURATION
- Publication number 20220154638
- Publication date May 19, 2022
- Nuovo Pignone Tecnologie S.r.l.
- Francesco CANGIOLI
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE AUXILIARY POWER UNIT
- Publication number 20200324909
- Publication date Oct 15, 2020
- Pratt & Whitney Canada Corp.
- Andreas ELEFTHERIOU
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
JET ENGINE
- Publication number 20200248649
- Publication date Aug 6, 2020
- Finn Schöning
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REVERSE-FLOW GAS TURBINE ENGINE
- Publication number 20180073428
- Publication date Mar 15, 2018
- Pratt & Whitney Canada Corp.
- Keith MORGAN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINES WITH FUEL INJECTOR ASSEMBLIES
- Publication number 20140345286
- Publication date Nov 27, 2014
- Honeywell International Inc.
- Frank J. Zupanc
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Bi-Directional Compression Fan Rotor for a Gas Turbine Engine
- Publication number 20140096507
- Publication date Apr 10, 2014
- United Technologies Corporation
- Sohail Mohammed
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Turbine Wheel Arrangement For A Gas Turbine
- Publication number 20130192231
- Publication date Aug 1, 2013
- BaltiCo GmbH
- Dirk Buchler
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Combined Pump System for Engine TMS AOC Reduction and ECS Loss Elim...
- Publication number 20130086922
- Publication date Apr 11, 2013
- PRATT & WHITNEY
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BOUNDARY LAYER EFFECT TURBINE
- Publication number 20110097189
- Publication date Apr 28, 2011
- Aaron Sandoval
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Engine
- Publication number 20070068135
- Publication date Mar 29, 2007
- Bernard Gill
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Integrated gearless and nonlubricated auxiliary power unit
- Publication number 20050284150
- Publication date Dec 29, 2005
- Kevin S. Dittmar
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Combined stage single shaft turbofan engine
- Publication number 20040216445
- Publication date Nov 4, 2004
- Anthony Jones
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbine engine
- Publication number 20040154309
- Publication date Aug 12, 2004
- Gill Bernard
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Gas turbine engine with offset shroud
- Publication number 20020073714
- Publication date Jun 20, 2002
- Thomas K. Yim
- Y10 - TECHNICAL SUBJECTS COVERED BY FORMER USPC

of the centripetal type

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Removable mechanical part for acoustic insulation of an air inlet c...

Aircraft engine having two radially offset turbines

Jet engine having fan blades with air and exhaust gas flow channels

Gas turbine auxiliary power unit

Forward-swept impellers and gas turbine engines employing the same

Bi-directional compression fan rotor for a gas turbine engine

Combined pump system for engine TMS AOC reduction and ECS loss elim...

Gas turbine fuel injector having flow guide for receiving air flow

Integrated gearless and nonlubricated auxiliary power unit

Combined stage single shaft turbofan engine

Turbomachine with a vaneless rotating diffuser and nozzle

Gas turbine engine with offset shroud

Advanced thermo-electronic systems for hybrid electric vehicles

Bi-metallic tie-bolt for microturbine power generating system

Gas turbine engine

Gas turbine engine including a bearing support tube cantilevered fr...

Turbine nozzle cooling

Volume enhanced turbine engine combustion zone

Volume enhanced turbine engine combustion zone

High efficiency, twin spool, radial-high pressure, gas turbine engine

Turbocharger-gas turbine

Segmented seal plate for a turbine engine

3898793

3460806

3052096

2804747

2748568

2651910

2477683

Patents Applicationslast 30 patents

AIRCRAFT ENGINE HAVING TWO RADIALLY OFFSET TURBINES

MULTISTAGE COMPRESSOR-EXPANDER TURBOMACHINE CONFIGURATION

GAS TURBINE AUXILIARY POWER UNIT

JET ENGINE

REVERSE-FLOW GAS TURBINE ENGINE

GAS TURBINE ENGINES WITH FUEL INJECTOR ASSEMBLIES

Bi-Directional Compression Fan Rotor for a Gas Turbine Engine

Turbine Wheel Arrangement For A Gas Turbine

Combined Pump System for Engine TMS AOC Reduction and ECS Loss Elim...

BOUNDARY LAYER EFFECT TURBINE

Engine

Integrated gearless and nonlubricated auxiliary power unit

Combined stage single shaft turbofan engine

Turbine engine

Gas turbine engine with offset shroud