the by-pass flow being at least partly used to create an independent thrust component

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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

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F02K3/025the by-pass flow being at least partly used to create an independent thrust component

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Patents Grantslast 30 patents

Information Patent Grant
Turbine engine with fan bypass water injection to augment thrust
- Patent number 12,173,669
- Issue date Dec 24, 2024
- General Electric Company
- Brandon W. Miller
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine compressor arrangement
- Patent number 12,085,025
- Issue date Sep 10, 2024
- RTX Corporation
- Karl L. Hasel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rotating detonation augmentors with adjustable throats for gas turb...
- Patent number 12,065,965
- Issue date Aug 20, 2024
- Rolls-Royce North American Technologies Inc.
- Victor L. Oechsle
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Propulsion system architecture
- Patent number 12,044,194
- Issue date Jul 23, 2024
- General Electric Company
- David Marion Ostdiek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Inlet for unducted propulsion system
- Patent number 12,017,751
- Issue date Jun 25, 2024
- General Electric Company
- Brandon Wayne Miller
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Unducted thrust producing system architecture
- Patent number 11,988,099
- Issue date May 21, 2024
- General Electric Company
- Darek Tomasz Zatorski
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Aircraft heat exchangers
- Patent number 11,982,232
- Issue date May 14, 2024
- RTX Corporation
- James F. Wiedenhoefer
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Geared architecture gas turbine engine with planetary gear oil scav...
- Patent number 11,946,540
- Issue date Apr 2, 2024
- RTX Corporation
- Janice Jabido
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Dual power lift system
- Patent number 11,859,542
- Issue date Jan 2, 2024
- Rolls-Royce North American Technologies, Inc.
- Richard K Keller
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine compressor arrangement
- Patent number 11,846,238
- Issue date Dec 19, 2023
- RTX Corporation
- Karl L. Hasel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine with third stream
- Patent number 11,834,954
- Issue date Dec 5, 2023
- General Electric Company
- David Marion Ostdiek
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Centrifugal compressor assembly for a gas turbine engine with deswi...
- Patent number 11,815,047
- Issue date Nov 14, 2023
- Rolls-Royce North American Technologies Inc.
- Ryan C. Humes
- 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 and method of creating classes of same
- Patent number 11,629,665
- Issue date Apr 18, 2023
- Pratt & Whitney Canada Corp.
- Ghislain Plante
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft heat exchangers
- Patent number 11,585,273
- Issue date Feb 21, 2023
- Raytheon Technologies Corporation
- James F. Wiedenhoefer
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Outer shroud of an intermediate casing for a dual flow turbine engi...
- Patent number 11,585,292
- Issue date Feb 21, 2023
- SAFRAN AIRCRAFT ENGINES
- Bruno Alexandre Didier Jacon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Geared architecture gas turbine engine with planetary gear oil scav...
- Patent number 11,448,309
- Issue date Sep 20, 2022
- Raytheon Technologies Corporation
- Janice Jabido
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Centrifugal compressor assembly for a gas turbine engine with deswi...
- Patent number 11,441,516
- Issue date Sep 13, 2022
- Rolls-Royce North American Technologies Inc.
- Ryan Humes
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbine section of high bypass turbofan
- Patent number 11,346,289
- Issue date May 31, 2022
- Raytheon Technologies Corporation
- Paul R. Adams
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
System and method of transferring power in a gas turbine engine
- Patent number 11,333,080
- Issue date May 17, 2022
- Rolls-Royce North American Technologies Inc.
- Charles L. McNeil
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Module of an aircraft bypass engine of which one arm integrates a s...
- Patent number 11,319,899
- Issue date May 3, 2022
- SAFRAN AIRCRAFT ENGINES
- Paul Antoine Foresto
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Unducted thrust producing system
- Patent number 11,300,003
- Issue date Apr 12, 2022
- General Electric Company
- Andrew Breeze-Stringfellow
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Hybrid propulsion cooling system
- Patent number 11,261,791
- Issue date Mar 1, 2022
- Rolls-Royce Corporation
- Robert T. Duge
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbojet with bearing architecture optimised for the support of a l...
- Patent number 11,187,107
- Issue date Nov 30, 2021
- SAFRAN AIRCRAFT ENGINES
- Antoine Jean-Philippe Beaujard
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Bypass duct conformal heat exchanger array
- Patent number 11,174,816
- Issue date Nov 16, 2021
- Rolls-Royce Corporation
- Christopher Banham
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Thermal management system using shape memory alloy actuator
- Patent number 11,168,584
- Issue date Nov 9, 2021
- The Boeing Company
- David W. Foutch
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Airfoil assembly with ceramic airfoil pieces and seal
- Patent number 11,162,368
- Issue date Nov 2, 2021
- Raytheon Technologies Corporation
- Adam P. Generale
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Variable geometry inlet system
- Patent number 11,066,993
- Issue date Jul 20, 2021
- Pratt & Whitney Canada Corp.
- Michel Labrecque
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Propulsion system using large scale vortex generators for flow redi...
- Patent number 10,981,659
- Issue date Apr 20, 2021
- Gulfstream Aerospace Corporation
- Michael Rybalko
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Duct assembly for a gas turbine engine
- Patent number 10,975,730
- Issue date Apr 13, 2021
- Raytheon Technologies Corporation
- Jonas S. Banhos
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
GEARED ARCHITECTURE GAS TURBINE ENGINE WITH PLANETARY GEAR OIL SCAV...
- Publication number 20250116327
- Publication date Apr 10, 2025
- RTX Corporation
- Janice Jabido
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROTATING DETONATION AUGMENTORS WITH FLOW RESTRICTION CONTROL FOR GA...
- Publication number 20250059932
- Publication date Feb 20, 2025
- Rolls-Royce North American Technologies Inc.
- Victor L. Oechsle
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
- Publication number 20240410320
- Publication date Dec 12, 2024
- RTX Corporation
- Karl L. Hasel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
UNDUCTED THRUST PRODUCING SYSTEM ARCHITECTURE
- Publication number 20240368997
- Publication date Nov 7, 2024
- GENERAL ELECTRIC COMPANY
- Darek Tomasz Zatorski
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
PROPULSION SYSTEM ARCHITECTURE
- Publication number 20240344487
- Publication date Oct 17, 2024
- GENERAL ELECTRIC COMPANY
- David Marion Ostdiek
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST MIXER WITH PROTRUSIONS
- Publication number 20240229740
- Publication date Jul 11, 2024
- Pratt & Whitney Canada Corp.
- Metin Ilbay YARAS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
- Publication number 20240068411
- Publication date Feb 29, 2024
- Karl L. Hasel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
APPARATUS AND METHOD FOR FLUID MANIPULATION
- Publication number 20230303239
- Publication date Sep 28, 2023
- Paul Neiser
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Aircraft Heat Exchangers
- Publication number 20230160342
- Publication date May 25, 2023
- Raytheon Technologies Corporation
- James F. Wiedenhoefer
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
GEARED ARCHITECTURE GAS TURBINE ENGINE WITH PLANETARY GEAR OIL SCAV...
- Publication number 20230160466
- Publication date May 25, 2023
- Raytheon Technologies Corporation
- Janice Jabido
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
INLET FOR UNDUCTED PROPULSION SYSTEM
- Publication number 20230085244
- Publication date Mar 16, 2023
- GENERAL ELECTRIC COMPANY
- Brandon Wayne Miller
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CENTRIFUGAL COMPRESSOR ASSEMBLY FOR A GAS TURBINE ENGINE WITH DESWI...
- Publication number 20220372931
- Publication date Nov 24, 2022
- Rolls-Royce North American Technologies, Inc.
- Ryan C. Humes
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
EFFICIENT GAS TURBINE ENGINE
- Publication number 20220307448
- Publication date Sep 29, 2022
- Rolls-Royce plc
- Roderick M. TOWNES
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Modular Device For Propulsion In A Vehicle
- Publication number 20220144422
- Publication date May 12, 2022
- Hugh Bryan Welcel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
CENTRIFUGAL COMPRESSOR ASSEMBLY FOR A GAS TURBINE ENGINE WITH DESWI...
- Publication number 20220018310
- Publication date Jan 20, 2022
- Rolls-Royce North American Technologies Inc.
- Ryan Humes
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GEARED ARCHITECTURE GAS TURBINE ENGINE WITH PLANETARY GEAR OIL SCAV...
- Publication number 20210222767
- Publication date Jul 22, 2021
- United Technologies Corporation
- Janice Jabido
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION SYSTEM ARCHITECTURE
- Publication number 20210108597
- Publication date Apr 15, 2021
- GENERAL ELECTRIC COMPANY
- David Marion Ostdiek
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE
- Publication number 20210062757
- Publication date Mar 4, 2021
- Rolls-Royce plc
- Chia Hui LIM
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE
- Publication number 20210062758
- Publication date Mar 4, 2021
- Rolls-Royce plc
- Christopher T. J. SHEAF
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
- Publication number 20210062725
- Publication date Mar 4, 2021
- Raytheon Technologies Corporation
- Karl L. Hasel
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE
- Publication number 20210062761
- Publication date Mar 4, 2021
- Rolls-Royce plc
- Chia Hui LIM
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE
- Publication number 20210062759
- Publication date Mar 4, 2021
- Rolls-Royce plc
- Chia Hui LIM
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE
- Publication number 20210062760
- Publication date Mar 4, 2021
- Rolls-Royce plc
- Christopher T. J. SHEAF
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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TURBINE SECTION OF HIGH BYPASS TURBOFAN
- Publication number 20210040898
- Publication date Feb 11, 2021
- Raytheon Technologies Corporation
- Paul R. Adams
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
OUTER SHROUD OF AN INTERMEDIATE CASING FOR A DUAL FLOW TURBINE ENGI...
- Publication number 20210003098
- Publication date Jan 7, 2021
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- Bruno Alexandre Didier JACON
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DUCT ASSEMBLY FOR A GAS TURBINE ENGINE
- Publication number 20210003038
- Publication date Jan 7, 2021
- United Technologies Corporation
- Jonas S. Banhos
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
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THERMAL MANAGEMENT SYSTEMS
- Publication number 20200408107
- Publication date Dec 31, 2020
- The Boeing Company
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- GENERAL ELECTRIC COMPANY
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MODULE OF AN AIRCRAFT BYPASS ENGINE OF WHICH ONE ARM INTEGRATES A S...
- Publication number 20200332743
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- SAFRAN AIRCRAFT ENGINES
- Paul Antoine FORESTO
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

the by-pass flow being at least partly used to create an independent thrust component

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Turbine engine with fan bypass water injection to augment thrust

Gas turbine engine compressor arrangement

Rotating detonation augmentors with adjustable throats for gas turb...

Propulsion system architecture

Inlet for unducted propulsion system

Unducted thrust producing system architecture

Aircraft heat exchangers

Geared architecture gas turbine engine with planetary gear oil scav...

Dual power lift system

Gas turbine engine compressor arrangement

Gas turbine engine with third stream

Centrifugal compressor assembly for a gas turbine engine with deswi...

Variable geometry inlet system

Gas turbine engine and method of creating classes of same

Aircraft heat exchangers

Outer shroud of an intermediate casing for a dual flow turbine engi...

Geared architecture gas turbine engine with planetary gear oil scav...

Centrifugal compressor assembly for a gas turbine engine with deswi...

Turbine section of high bypass turbofan

System and method of transferring power in a gas turbine engine

Module of an aircraft bypass engine of which one arm integrates a s...

Unducted thrust producing system

Hybrid propulsion cooling system

Turbojet with bearing architecture optimised for the support of a l...

Bypass duct conformal heat exchanger array

Thermal management system using shape memory alloy actuator

Airfoil assembly with ceramic airfoil pieces and seal

Variable geometry inlet system

Propulsion system using large scale vortex generators for flow redi...

Duct assembly for a gas turbine engine

Patents Applicationslast 30 patents

GEARED ARCHITECTURE GAS TURBINE ENGINE WITH PLANETARY GEAR OIL SCAV...

ROTATING DETONATION AUGMENTORS WITH FLOW RESTRICTION CONTROL FOR GA...

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

UNDUCTED THRUST PRODUCING SYSTEM ARCHITECTURE

PROPULSION SYSTEM ARCHITECTURE

EXHAUST MIXER WITH PROTRUSIONS

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

APPARATUS AND METHOD FOR FLUID MANIPULATION

Aircraft Heat Exchangers

GEARED ARCHITECTURE GAS TURBINE ENGINE WITH PLANETARY GEAR OIL SCAV...

INLET FOR UNDUCTED PROPULSION SYSTEM

CENTRIFUGAL COMPRESSOR ASSEMBLY FOR A GAS TURBINE ENGINE WITH DESWI...

EFFICIENT GAS TURBINE ENGINE

Modular Device For Propulsion In A Vehicle

CENTRIFUGAL COMPRESSOR ASSEMBLY FOR A GAS TURBINE ENGINE WITH DESWI...

GEARED ARCHITECTURE GAS TURBINE ENGINE WITH PLANETARY GEAR OIL SCAV...

PROPULSION SYSTEM ARCHITECTURE

GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE

GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE

GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE

GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE

TURBINE SECTION OF HIGH BYPASS TURBOFAN

OUTER SHROUD OF AN INTERMEDIATE CASING FOR A DUAL FLOW TURBINE ENGI...

DUCT ASSEMBLY FOR A GAS TURBINE ENGINE

THERMAL MANAGEMENT SYSTEMS

AIRFOIL ASSEMBLY WITH CERAMIC AIRFOIL PIECES AND SEAL

High Speed Aircraft Flight Technologies

MODULE OF AN AIRCRAFT BYPASS ENGINE OF WHICH ONE ARM INTEGRATES A S...