using reversing fan blades

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CPC
F02K1/66

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FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02KJET-PROPULSION PLANTS F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle Jet pipes or nozzles peculiar thereto

Current Industry

F02K1/66using reversing fan blades

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Process for using an air input of a turboreactor nacelle comprising...
- Patent number 12,134,983
- Issue date Nov 5, 2024
- SAFRAN AIRCRAFT ENGINES
- Daniel-Ciprian Mincu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Air outlet for a nacelle for an aircraft bypass turbojet engine com...
- Patent number 12,110,842
- Issue date Oct 8, 2024
- SAFRAN AIRCRAFT ENGINES
- Eva Julie Lebeault
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Reverse thrust system and method
- Patent number 11,933,248
- Issue date Mar 19, 2024
- Pratt & Whitney Canada Corp.
- Jagoda Krzywon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nacelle air outlet for aircraft turbojet engine comprising a straig...
- Patent number 11,913,404
- Issue date Feb 27, 2024
- SAFRAN AIRCRAFT ENGINES
- Philippe Gérard Chanez
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust reverser interspatial blocker system
- Patent number 11,905,913
- Issue date Feb 20, 2024
- Spirit Aerosystems, Inc.
- Randall R. West
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
System and method for control for unducted engine
- Patent number 11,834,196
- Issue date Dec 5, 2023
- General Electric Company
- Sridhar Adibhatla
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Layered fuselage shield
- Patent number 11,814,174
- Issue date Nov 14, 2023
- General Electric Company
- David William Crall
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbofan comprising a series of rotary blades for closing off the d...
- Patent number 11,802,524
- Issue date Oct 31, 2023
- Airbus Operations (S.A.S.)
- Simon Vanderbauwede
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
System and method for providing in-flight reverse thrust for an air...
- Patent number 11,668,253
- Issue date Jun 6, 2023
- Pratt & Whitney Canada Corp.
- Charles Cormier
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Method for operating an air intake of a turbojet engine nacelle dur...
- Patent number 11,649,765
- Issue date May 16, 2023
- SAFRAN AIRCRAFT ENGINES
- Daniel-Ciprian Mincu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Air intake of a turbojet engine nacelle comprising guide vanes
- Patent number 11,614,051
- Issue date Mar 28, 2023
- SAFRAN AIRCRAFT ENGINES
- Anthony Binder
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine with clutch assembly
- Patent number 11,506,067
- Issue date Nov 22, 2022
- General Electric Company
- Brian Lewis Devendorf
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine outlet guide vane assembly
- Patent number 11,401,824
- Issue date Aug 2, 2022
- General Electric Company
- Andrew Breeze-Stringfellow
- B32 - LAYERED PRODUCTS
Information Patent Grant
Gas turbine engine with variable pitch fan and variable pitch compr...
- Patent number 11,286,865
- Issue date Mar 29, 2022
- Rolls-Royce North American Technologies Inc.
- Kyle Klein
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Propulsion assembly comprising a duct for feeding the gas generator...
- Patent number 11,255,295
- Issue date Feb 22, 2022
- SAFRAN AIRCRAFT ENGINES
- Guillaume Rodolphe Jacques Gerard Pouyau
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Method of providing turbine engines with different thrust ratings
- Patent number 11,225,913
- Issue date Jan 18, 2022
- Raytheon Technologies Corporation
- Frederick M. Schwarz
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Brake systems for aircraft and related methods
- Patent number 11,155,343
- Issue date Oct 26, 2021
- The Boeing Company
- Christopher T. Jasklowski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft comprising two contra-rotating fans to the rear of the fus...
- Patent number 11,125,186
- Issue date Sep 21, 2021
- SAFRAN AIRCRAFT ENGINES
- Francois Gallet
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fan cowl with a serrated trailing edge providing attached flow in r...
- Patent number 11,053,888
- Issue date Jul 6, 2021
- The Boeing Company
- John C. Vassberg
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Bellmouth nozzle assembly for a gas turbine engine
- Patent number 11,047,336
- Issue date Jun 29, 2021
- General Electric Company
- Tomasz Iglewski
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fan module with variable pitch blades
- Patent number 10,899,432
- Issue date Jan 26, 2021
- SAFRAN AIRCRAFT ENGINES
- Gilles Alain Marie Charier
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Method and system for limiting power of an engine
- Patent number 10,823,113
- Issue date Nov 3, 2020
- Pratt & Whitney Canada Corp.
- Sylvain Lamarre
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Hybrid aircraft propulsors having electrically-driven augmentor fans
- Patent number 10,710,734
- Issue date Jul 14, 2020
- The Boeing Company
- Mithra M. K. V. Sankrithi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Reverse thrust engine
- Patent number 10,502,160
- Issue date Dec 10, 2019
- General Electric Company
- Tsuguji Nakano
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine with reversible fan
- Patent number 10,465,538
- Issue date Nov 5, 2019
- General Electric Company
- Darek Tomasz Zatorski
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Variable pitch fan pitch range limiter
- Patent number 10,443,412
- Issue date Oct 15, 2019
- General Electric Company
- Daniel Alan Niergarth
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Multi-stage co-rotating variable pitch fan
- Patent number 10,253,784
- Issue date Apr 9, 2019
- Rolls-Royce Corporation
- Roy D. Fulayter
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Pivoting blocker door
- Patent number 10,156,206
- Issue date Dec 18, 2018
- United Technologies Corporation
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine and method of assembling the same
- Patent number 10,113,508
- Issue date Oct 30, 2018
- General Electric Company
- Alan Roy Stuart
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Pitch change mechanism for shrouded fan with low fan pressure ratio
- Patent number 9,963,981
- Issue date May 8, 2018
- General Electric Company
- Narendra Digamber Joshi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
TURBINE ENGINE HAVING A THRUST REVERSER SYSTEM
- Publication number 20240401546
- Publication date Dec 5, 2024
- GENERAL ELECTRIC COMPANY
- Scott D. Hunter
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION SYSTEM AND METHOD FOR OPERATION
- Publication number 20240401490
- Publication date Dec 5, 2024
- GENERAL ELECTRIC COMPANY
- Sridhar Adibhatla
- B32 - LAYERED PRODUCTS
Information Patent Application
ADVANCE RATIO FOR SINGLE UNDUCTED ROTOR ENGINE
- Publication number 20230415914
- Publication date Dec 28, 2023
- GENERAL ELECTRIC COMPANY
- Syed Arif Khalid
- B32 - LAYERED PRODUCTS
Information Patent Application
AIRCRAFT DUAL-FLOW TURBINE ENGINE ASSEMBLY, THE ASSEMBLY BEING EQUI...
- Publication number 20230407797
- Publication date Dec 21, 2023
- SAFRAN AIRCRAFT ENGINES
- Eva Julie LEBEAULT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REVERSE THRUST TURBOFAN ENGINE
- Publication number 20230340927
- Publication date Oct 26, 2023
- GENERAL ELECTRIC COMPANY
- Trevor Howard Wood
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIR OUTLET FOR A NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE COM...
- Publication number 20230090029
- Publication date Mar 23, 2023
- SAFRAN AIRCRAFT ENGINES
- Eva Julie Lebeault
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE PITCH FAN THRUST REVERSER
- Publication number 20230027032
- Publication date Jan 26, 2023
- Rolls-Royce plc
- Vasileios PACHIDIS
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOFAN COMPRISING A SERIES OF ROTARY BLADES FOR CLOSING OFF THE D...
- Publication number 20230008832
- Publication date Jan 12, 2023
- AIRBUS OPERATIONS (SAS)
- Simon Vanderbauwede
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BYPASS TURBOMACHINE FOR AN AIRCRAFT
- Publication number 20220333495
- Publication date Oct 20, 2022
- SAFRAN AIRCRAFT ENGINES
- Eva Julie LEBEAULT
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
METHOD FOR OPERATING AN AIR INTAKE OF A TURBOJET ENGINE NACELLE DUR...
- Publication number 20220186663
- Publication date Jun 16, 2022
- SAFRAN AIRCRAFT ENGINES
- Daniel-Ciprian Mincu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIR INTAKE OF A TURBOJET ENGINE NACELLE COMPRISING GUIDE VANES
- Publication number 20220170430
- Publication date Jun 2, 2022
- SAFRAN AIRCRAFT ENGINES
- Anthony Binder
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BRAKE SYSTEMS FOR AIRCRAFT AND RELATED METHODS
- Publication number 20200189725
- Publication date Jun 18, 2020
- The Boeing Company
- Christopher T. Jasklowski
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FAN COWL WITH A SERRATED TRAILING EDGE PROVIDING ATTACHED FLOW IN R...
- Publication number 20190128214
- Publication date May 2, 2019
- The Boeing Company
- John C. Vassberg
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
FLOW PATH SPLITTER FOR TURBOFAN GAS TURBINE ENGINES
- Publication number 20190078536
- Publication date Mar 14, 2019
- Rolls-Royce North American Technologies Inc.
- Benjamin M. Iwrey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD AND SYSTEM FOR LIMITING POWER OF AN ENGINE
- Publication number 20190055901
- Publication date Feb 21, 2019
- Pratt & Whitney Canada Corp.
- Sylvain LAMARRE
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
AIRCRAFT COMPRISING TWO CONTRA-ROTATING FANS TO THE REAR OF THE FUS...
- Publication number 20180209380
- Publication date Jul 26, 2018
- SAFRAN AIRCRAFT ENGINES
- Francois GALLET
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION ASSEMBLY COMPRISING A DUCT FOR FEEDING THE GAS GENERATOR...
- Publication number 20180135557
- Publication date May 17, 2018
- SAFRAN AIRCRAFT ENGINES
- Guillaume Rodolphe Jacques Gerard POUYAU
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
THRUST SCHEDULING METHOD FOR VARIABLE PITCH FAN ENGINES AND TURBO-S...
- Publication number 20170107914
- Publication date Apr 20, 2017
- Manxue Lu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AFT COUNTER-ROTATING SHROUDED GEARED TURBOFAN
- Publication number 20150211444
- Publication date Jul 30, 2015
- United Technologies Corporation
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MOVABLE ACTUATOR DEVICE FOR CONTROLLING THE PITCH OF FAN BLADES OF...
- Publication number 20120070292
- Publication date Mar 22, 2012
- SNECMA
- Wouter Balk
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
DEVICE FOR CONTROLLING THE PITCH OF FAN BLADES OF A TURBOPROP
- Publication number 20120070290
- Publication date Mar 22, 2012
- SNECMA
- Wouter Balk
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Internal duct VTOL aircraft propulsion system
- Publication number 20060027704
- Publication date Feb 9, 2006
- John Eugene Dickau
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VTOL aircraft propulsion systems and forward flight thrust vectoring
- Publication number 20030033798
- Publication date Feb 20, 2003
- John Eugene Dickau
- B64 - AIRCRAFT AVIATION COSMONAUTICS

using reversing fan blades

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Process for using an air input of a turboreactor nacelle comprising...

Air outlet for a nacelle for an aircraft bypass turbojet engine com...

Reverse thrust system and method

Nacelle air outlet for aircraft turbojet engine comprising a straig...

Thrust reverser interspatial blocker system

System and method for control for unducted engine

Layered fuselage shield

Turbofan comprising a series of rotary blades for closing off the d...

System and method for providing in-flight reverse thrust for an air...

Method for operating an air intake of a turbojet engine nacelle dur...

Air intake of a turbojet engine nacelle comprising guide vanes

Gas turbine engine with clutch assembly

Gas turbine engine outlet guide vane assembly

Gas turbine engine with variable pitch fan and variable pitch compr...

Propulsion assembly comprising a duct for feeding the gas generator...

Method of providing turbine engines with different thrust ratings

Brake systems for aircraft and related methods

Aircraft comprising two contra-rotating fans to the rear of the fus...

Fan cowl with a serrated trailing edge providing attached flow in r...

Bellmouth nozzle assembly for a gas turbine engine

Fan module with variable pitch blades

Method and system for limiting power of an engine

Hybrid aircraft propulsors having electrically-driven augmentor fans

Reverse thrust engine

Gas turbine engine with reversible fan

Variable pitch fan pitch range limiter

Multi-stage co-rotating variable pitch fan

Pivoting blocker door

Gas turbine engine and method of assembling the same

Pitch change mechanism for shrouded fan with low fan pressure ratio

Patents Applicationslast 30 patents

TURBINE ENGINE HAVING A THRUST REVERSER SYSTEM

PROPULSION SYSTEM AND METHOD FOR OPERATION

ADVANCE RATIO FOR SINGLE UNDUCTED ROTOR ENGINE

AIRCRAFT DUAL-FLOW TURBINE ENGINE ASSEMBLY, THE ASSEMBLY BEING EQUI...

REVERSE THRUST TURBOFAN ENGINE

AIR OUTLET FOR A NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE COM...

VARIABLE PITCH FAN THRUST REVERSER

TURBOFAN COMPRISING A SERIES OF ROTARY BLADES FOR CLOSING OFF THE D...

BYPASS TURBOMACHINE FOR AN AIRCRAFT

METHOD FOR OPERATING AN AIR INTAKE OF A TURBOJET ENGINE NACELLE DUR...

AIR INTAKE OF A TURBOJET ENGINE NACELLE COMPRISING GUIDE VANES

BRAKE SYSTEMS FOR AIRCRAFT AND RELATED METHODS

FAN COWL WITH A SERRATED TRAILING EDGE PROVIDING ATTACHED FLOW IN R...

FLOW PATH SPLITTER FOR TURBOFAN GAS TURBINE ENGINES

METHOD AND SYSTEM FOR LIMITING POWER OF AN ENGINE

AIRCRAFT COMPRISING TWO CONTRA-ROTATING FANS TO THE REAR OF THE FUS...

PROPULSION ASSEMBLY COMPRISING A DUCT FOR FEEDING THE GAS GENERATOR...

THRUST SCHEDULING METHOD FOR VARIABLE PITCH FAN ENGINES AND TURBO-S...

AFT COUNTER-ROTATING SHROUDED GEARED TURBOFAN

MOVABLE ACTUATOR DEVICE FOR CONTROLLING THE PITCH OF FAN BLADES OF...

DEVICE FOR CONTROLLING THE PITCH OF FAN BLADES OF A TURBOPROP

Internal duct VTOL aircraft propulsion system

VTOL aircraft propulsion systems and forward flight thrust vectoring