being characterised by a short axial length relative to the diameter

Industry

CPC
F02K3/068

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Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02KJET-PROPULSION PLANTS F02K3/00Plants including a gas turbine driving a compressor or a ducted fan

Current Industry

F02K3/068being characterised by a short axial length relative to the diameter

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine compression system with core compressor pressure...
- Patent number 12,024,301
- Issue date Jul 2, 2024
- Rolls-Royce PLC
- Gareth M Armstrong
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Efficient gas turbine engine installation and operation
- Patent number 12,006,835
- Issue date Jun 11, 2024
- Rolls-Royce PLC
- Nicholas Howarth
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 11,781,505
- Issue date Oct 10, 2023
- RTX Corporation
- Wesley K. Lord
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Aircraft engine
- Patent number 11,692,454
- Issue date Jul 4, 2023
- Rolls-Royce plc
- Benjamin Mohankumar
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Variable geometry inlet system
- Patent number 11,661,887
- Issue date May 30, 2023
- Pratt & Whitney Canada Corp.
- Michel Labrecque
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine compression system with core compressor pressure...
- Patent number 11,584,532
- Issue date Feb 21, 2023
- Rolls-Royce PLC
- Gareth M Armstrong
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Efficient gas turbine engine installation and operation
- Patent number 11,459,893
- Issue date Oct 4, 2022
- Rolls-Royce PLC
- Nicholas Howarth
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Nacelle for gas turbine engine
- Patent number 11,415,048
- Issue date Aug 16, 2022
- Rolls-Royce PLC
- Robert E Christie
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Elongated geared turbofan with high bypass ratio
- Patent number 11,391,216
- Issue date Jul 19, 2022
- Raytheon Technologies Corporation
- Frederick M. Schwarz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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 engine compression system
- Patent number 11,242,155
- Issue date Feb 8, 2022
- Rolls-Royce PLC
- Gareth M Armstrong
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with optimized fan, core passage inlet, and comp...
- Patent number 11,047,339
- Issue date Jun 29, 2021
- Rolls-Royce PLC
- James M. Pointon
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 11,015,550
- Issue date May 25, 2021
- Raytheon Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Efficient gas turbine engine installation and operation
- Patent number 10,982,550
- Issue date Apr 20, 2021
- Rolls-Royce PLC
- Nicholas Howarth
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fan case for use in a turbofan engine, and method of assembling a t...
- Patent number 10,830,136
- Issue date Nov 10, 2020
- General Electric Company
- Alan Roy Stuart
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Counter rotating turbine with reversing speed reduction assembly
- Patent number 10,815,881
- Issue date Oct 27, 2020
- General Electric Company
- Jeffrey Donald Clements
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Tip turbine engine composite tailcone
- Patent number 10,760,483
- Issue date Sep 1, 2020
- Raytheon Technologies Corporation
- Brian Merry
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Architecture for an axially compact, high performance propulsion sy...
- Patent number 10,550,764
- Issue date Feb 4, 2020
- United Technologies Corporation
- Gary D. Roberge
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Efficient gas turbine engine installation and operation
- Patent number 10,550,700
- Issue date Feb 4, 2020
- Rolls-Royce PLC
- Nicholas Howarth
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Load balanced journal bearing pin
- Patent number 10,533,522
- Issue date Jan 14, 2020
- United Technologies Corporation
- William G. Sheridan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Anti-rotation feature for wear liners
- Patent number 10,451,082
- Issue date Oct 22, 2019
- United Technologies Corporation
- Thomas Freeman
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
High compressor build clearance reduction
- Patent number 10,443,543
- Issue date Oct 15, 2019
- United Technologies Corporation
- John P. Virtue
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Exhaust nozzle for an elongated gear turbofan with high bypass ratio
- Patent number 10,436,120
- Issue date Oct 8, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Translating turning vanes for a nacelle inlet
- Patent number 10,436,112
- Issue date Oct 8, 2019
- The Boeing Company
- Zachary C. Hoisington
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Elongated geared turbofan with high bypass ratio
- Patent number 10,436,121
- Issue date Oct 8, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Exhaust nozzle arrangement for geared turbofan
- Patent number 10,316,757
- Issue date Jun 11, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Exhaust nozzle arrangement for geared turbofan
- Patent number 10,294,871
- Issue date May 21, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with twin offset gas generators
- Patent number 10,094,281
- Issue date Oct 9, 2018
- United Technologies Corporation
- Jesse M. Chandler
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbofan bypass air cooled oil cooler fairings
- Patent number 9,982,630
- Issue date May 29, 2018
- Pratt & Whitney Canada Corp.
- Remo Marini
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 9,932,933
- Issue date Apr 3, 2018
- United Technologies Corporation
- Wesley K. Lord
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE...
- Publication number 20240317411
- Publication date Sep 26, 2024
- Rolls-Royce plc
- Gareth M ARMSTRONG
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE...
- Publication number 20230242264
- Publication date Aug 3, 2023
- Rolls-Royce plc
- Gareth M ARMSTRONG
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Improved gas turbine engine
- Publication number 20230184197
- Publication date Jun 15, 2023
- Rolls-Royce plc
- Benjamin J. SELLERS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EFFICIENT GAS TURBINE ENGINE INSTALLATION AND OPERATION
- Publication number 20220403743
- Publication date Dec 22, 2022
- Rolls-Royce plc
- Nicholas HOWARTH
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE COMPRESSION SYSTEM
- Publication number 20220119120
- Publication date Apr 21, 2022
- Rolls-Royce plc
- Gareth M ARMSTRONG
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20210285403
- Publication date Sep 16, 2021
- Raytheon Technologies Corporation
- Wesley K. Lord
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
EFFICIENT GAS TURBINE ENGINE INSTALLATION AND OPERATION
- Publication number 20210207483
- Publication date Jul 8, 2021
- Rolls-Royce plc
- Nicholas HOWARTH
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
METHOD FOR CONSTRUCTING ENGINES OR MOTORS CONTAINED IN A CYLINDRICA...
- Publication number 20200325779
- Publication date Oct 15, 2020
- CARPYZ SAS
- Pierre CARROUSET
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EFFICIENT GAS TURBINE ENGINE INSTALLATION AND OPERATION
- Publication number 20200291785
- Publication date Sep 17, 2020
- Rolls-Royce plc
- Nicholas HOWARTH
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
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
ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO
- Publication number 20190271269
- Publication date Sep 5, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE
- Publication number 20190048826
- Publication date Feb 14, 2019
- Rolls-Royce plc
- James M. POINTON
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
HIGH COMPRESSOR BUILD CLEARANCE REDUCTION
- Publication number 20180230946
- Publication date Aug 16, 2018
- United Technologies Corporation
- John P. Virtue
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20180209379
- Publication date Jul 26, 2018
- United Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TIP TURBINE ENGINE COMPOSITE TAILCONE
- Publication number 20180106194
- Publication date Apr 19, 2018
- United Technologies Corporation
- Brian Merry
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ANTI-ROTATION FEATURE FOR WEAR LINERS
- Publication number 20180051713
- Publication date Feb 22, 2018
- United Technologies Corporation
- Thomas Freeman
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
LOAD BALANCED JOURNAL BEARING PIN
- Publication number 20170356388
- Publication date Dec 14, 2017
- United Technologies Corporation
- William G. Sheridan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOFAN AIRCRAFT ENGINE WITH REDUCED NOISE EMISSION
- Publication number 20170159609
- Publication date Jun 8, 2017
- MTU AERO ENGINES AG
- Carsten SCHOENHOFF
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Elongated Geared Turbofan With High Bypass Ratio
- Publication number 20140286754
- Publication date Sep 25, 2014
- United Technologies Corporation
- Frederick M. Schwarz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO
- Publication number 20140283501
- Publication date Sep 25, 2014
- United Technologies Corporation
- Frederick M. Schwarz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DE-COUPLE GEARED TURBO-FAN ENGINE AND AIRCRAFT
- Publication number 20140252161
- Publication date Sep 11, 2014
- United Technologies Corporation
- Robert L. Gukeisen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COUNTER-ROTATING LOW PRESSURE TURBINE WITH GEAR SYSTEM MOUNTED TO T...
- Publication number 20130223992
- Publication date Aug 29, 2013
- Gabriel L. Suciu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE BEARING ARRANGEMENT INCLUDING AFT BEARING HUB GE...
- Publication number 20130195647
- Publication date Aug 1, 2013
- Marc J. Muldoon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE FAN INLET GUIDE VANE FOR TURBINE ENGINE
- Publication number 20130019585
- Publication date Jan 24, 2013
- Brian Merry
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TANDEM FAN-TURBINE ROTOR FOR A TIP TURBINE ENGINE
- Publication number 20120324901
- Publication date Dec 27, 2012
- United Technologies Corporation
- Mahdy A. Allam
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TAPERED BEARINGS
- Publication number 20120167593
- Publication date Jul 5, 2012
- Gabriel L. Suciu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
VARIABLE FAN INLET GUIDE VANE ASSEMBLY, TURBINE ENGINE WITH SUCH AN...
- Publication number 20120121375
- Publication date May 17, 2012
- Gabriel L. Suciu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Absolute universal engine, one from ground to orbit
- Publication number 20120110978
- Publication date May 10, 2012
- Marius Angelo Paul
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TIP TURBINE ENGINE WITH REVERSE CORE AIRFLOW
- Publication number 20120111018
- Publication date May 10, 2012
- James W. Norris
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Universal aero space , naval eternal technology systems
- Publication number 20120110976
- Publication date May 10, 2012
- Marius Angelo Paul
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

being characterised by a short axial length relative to the diameter

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Gas turbine engine compression system with core compressor pressure...

Efficient gas turbine engine installation and operation

Low pressure ratio fan engine having a dimensional relationship bet...

Aircraft engine

Variable geometry inlet system

Gas turbine engine compression system with core compressor pressure...

Efficient gas turbine engine installation and operation

Nacelle for gas turbine engine

Elongated geared turbofan with high bypass ratio

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

Gas turbine engine compression system

Gas turbine engine with optimized fan, core passage inlet, and comp...

Low pressure ratio fan engine having a dimensional relationship bet...

Efficient gas turbine engine installation and operation

Fan case for use in a turbofan engine, and method of assembling a t...

Counter rotating turbine with reversing speed reduction assembly

Tip turbine engine composite tailcone

Architecture for an axially compact, high performance propulsion sy...

Efficient gas turbine engine installation and operation

Load balanced journal bearing pin

Anti-rotation feature for wear liners

High compressor build clearance reduction

Exhaust nozzle for an elongated gear turbofan with high bypass ratio

Translating turning vanes for a nacelle inlet

Elongated geared turbofan with high bypass ratio

Exhaust nozzle arrangement for geared turbofan

Exhaust nozzle arrangement for geared turbofan

Gas turbine engine with twin offset gas generators

Turbofan bypass air cooled oil cooler fairings

Low pressure ratio fan engine having a dimensional relationship bet...

Patents Applicationslast 30 patents

GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE...

GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE...

Improved gas turbine engine

EFFICIENT GAS TURBINE ENGINE INSTALLATION AND OPERATION

GAS TURBINE ENGINE COMPRESSION SYSTEM

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

EFFICIENT GAS TURBINE ENGINE INSTALLATION AND OPERATION

METHOD FOR CONSTRUCTING ENGINES OR MOTORS CONTAINED IN A CYLINDRICA...

EFFICIENT GAS TURBINE ENGINE INSTALLATION AND OPERATION

JET ENGINE

ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO

GAS TURBINE ENGINE

HIGH COMPRESSOR BUILD CLEARANCE REDUCTION

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

TIP TURBINE ENGINE COMPOSITE TAILCONE

ANTI-ROTATION FEATURE FOR WEAR LINERS

LOAD BALANCED JOURNAL BEARING PIN

TURBOFAN AIRCRAFT ENGINE WITH REDUCED NOISE EMISSION

Elongated Geared Turbofan With High Bypass Ratio

ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO

DE-COUPLE GEARED TURBO-FAN ENGINE AND AIRCRAFT

COUNTER-ROTATING LOW PRESSURE TURBINE WITH GEAR SYSTEM MOUNTED TO T...

GAS TURBINE ENGINE BEARING ARRANGEMENT INCLUDING AFT BEARING HUB GE...

VARIABLE FAN INLET GUIDE VANE FOR TURBINE ENGINE

TANDEM FAN-TURBINE ROTOR FOR A TIP TURBINE ENGINE

TAPERED BEARINGS

VARIABLE FAN INLET GUIDE VANE ASSEMBLY, TURBINE ENGINE WITH SUCH AN...

Absolute universal engine, one from ground to orbit

TIP TURBINE ENGINE WITH REVERSE CORE AIRFLOW

Universal aero space , naval eternal technology systems