for turbofan engines

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CPC
B64D2033/0286

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Parent Industries

BPERFORMING OPERATIONS TRANSPORTING B64Aviation B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT

Current Industry

B64D2033/0286for turbofan engines

Industries

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Patents Grantslast 30 patents

Information Patent Grant
System and method for cooling a fluid of a lubrication or cooling c...
- Patent number 12,172,769
- Issue date Dec 24, 2024
- Liebherr-Aerospace Toulouse SAS
- Laurent Fayolle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle air intake and nacelle comprising such an air intake
- Patent number 12,103,694
- Issue date Oct 1, 2024
- SAFRAN NACELLES
- Gina Ferrier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Multiple intake distortion adaptive fan for gas turbine engine
- Patent number 12,065,258
- Issue date Aug 20, 2024
- Rolls-Royce North American Technologies Inc.
- Robert W. Heeter
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Aircraft propulsion system inlet structure with variable airflow in...
- Patent number 11,993,389
- Issue date May 28, 2024
- Rohr, Inc.
- Timothy Gormley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft
- Patent number 11,988,141
- Issue date May 21, 2024
- Rolls-Royce PLC
- Natalie C Wong
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Fan arrangement for a gas turbine engine
- Patent number 11,988,169
- Issue date May 21, 2024
- Rolls-Royce PLC
- Richard G Stretton
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Advanced inlet design
- Patent number 11,982,229
- Issue date May 14, 2024
- The Boeing Company
- Holly J. Thomas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Assembly for a turbomachine
- Patent number 11,913,378
- Issue date Feb 27, 2024
- INSTITUT SUPERIEUR DE L'AÉRONAUTIQUE ET DE L'ESPACE
- Nicolas Jérôme Jean Tantot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Ice accumulation and shedding mitigation for sensor probe
- Patent number 11,885,261
- Issue date Jan 30, 2024
- Pratt & Whitney Canada Corp.
- Milos Ivankovic
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Supersonic aircraft turbofan engine
- Patent number 11,884,414
- Issue date Jan 30, 2024
- Rolls-Royce PLC
- Robert J Corin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Air intake of an aircraft turbine engine nacelle
- Patent number 11,866,178
- Issue date Jan 9, 2024
- SAFRAN NACELLES
- Alexis Yves-Marie Loncle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle air intake and nacelle comprising such an air intake
- Patent number 11,840,352
- Issue date Dec 12, 2023
- SAFRAN NACELLES
- Gina Ferrier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft having a single fluid inlet aperture
- Patent number 11,828,228
- Issue date Nov 28, 2023
- Rolls-Royce PLC
- Natalie C Wong
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbofan engine, nacelle thereof, and associated method of operation
- Patent number 11,807,379
- Issue date Nov 7, 2023
- Pratt & Whitney Canada Corp.
- Philippe-André Tetrault
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Propulsion unit with improved boundary layer ingestion
- Patent number 11,772,779
- Issue date Oct 3, 2023
- SAFRAN AIRCRAFT ENGINES
- Philippe Gérard Chanez
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbofan gas turbine engine
- Patent number 11,767,789
- Issue date Sep 26, 2023
- Rolls-Royce PLC
- Natalie C Wong
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Methods and apparatus to detect air flow separation of an engine
- Patent number 11,674,451
- Issue date Jun 13, 2023
- General Electric Company
- Sai Venkata Karthik Saripella
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Aircraft with a single fluid inlet aperture
- Patent number 11,649,764
- Issue date May 16, 2023
- Rolls-Royce PLC
- Natalie C Wong
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Heat exchanger
- Patent number 11,649,767
- Issue date May 16, 2023
- Rolls-Royce PLC
- Stephen J Bradbrook
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Ducted fan case attachment structure
- Patent number 11,613,372
- Issue date Mar 28, 2023
- Rohr, Inc.
- Michael Aten
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Hybrid propulsion for an aircraft
- Patent number 11,608,188
- Issue date Mar 21, 2023
- SAFRAN
- Gaetan Chesneau
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Nacelle forward part of a propulsion assembly comprising an incline...
- Patent number 11,591,098
- Issue date Feb 28, 2023
- Airbus Operations S.A.S.
- Frédéric Vinches
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
Aircraft nacelle having a fan ramp with articulated flaps
- Patent number 11,577,849
- Issue date Feb 14, 2023
- Airbus Operations SAS
- Fabien Menou
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nacelle
- Patent number 11,548,652
- Issue date Jan 10, 2023
- Raytheon Technologies Corporation
- Dmitriy B. Sidelkovskiy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nacelle for gas turbine engine
- Patent number 11,519,330
- Issue date Dec 6, 2022
- Rolls-Royce PLC
- Robert E Christie
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Engine enclosure air inlet section
- Patent number 11,486,308
- Issue date Nov 1, 2022
- Rohr, Inc.
- Jason K. Chen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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

Patents Applicationslast 30 patents

Information Patent Application
NACELLE INLET STRUCTURE WITH FOAM CORE
- Publication number 20240400218
- Publication date Dec 5, 2024
- Rohr, Inc.
- Brian A. Sherman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
AFT AIR INLET PARTICLE SEPARATOR FOR TURBINE ENGINE
- Publication number 20240262523
- Publication date Aug 8, 2024
- RTX Corporation
- Neil J. Terwilliger
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VARIABLE COMPRESSION AIR INTAKES FOR AIRCRAFT PROPULSION SYSTEMS AN...
- Publication number 20240253800
- Publication date Aug 1, 2024
- The Boeing Company
- Thomas R. Smith
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
MULTIPLE INTAKE DISTORTION ADAPTIVE FAN FOR GAS TURBINE ENGINE
- Publication number 20240246688
- Publication date Jul 25, 2024
- Rolls-Royce North American Technologies Inc.
- Robert W. Heeter
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET
- Publication number 20240229713
- Publication date Jul 11, 2024
- Rohr, Inc.
- Timothy Gormley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Cowl Seal Assembly for an Aircraft Propulsion System
- Publication number 20240101263
- Publication date Mar 28, 2024
- Pratap MALLAMPATI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ASSEMBLY FOR A TURBOMACHINE
- Publication number 20230349323
- Publication date Nov 2, 2023
- INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPACE
- Nicolas Jérôme Jean TANTOT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
AIRCRAFT HAVING A SINGLE FLUID INLET APERTURE
- Publication number 20230193822
- Publication date Jun 22, 2023
- Rolls-Royce plc
- Natalie C. WONG
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET
- Publication number 20230080020
- Publication date Mar 16, 2023
- Jose S. Alonso-Miralles
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE INLET
- Publication number 20230025200
- Publication date Jan 26, 2023
- Raytheon Technologies Corporation
- Yuan J. Qiu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
METHODS AND APPARATUS TO DETECT AIR FLOW SEPARATION OF AN ENGINE
- Publication number 20220412271
- Publication date Dec 29, 2022
- GENERAL ELECTRIC COMPANY
- Sai Venkata Karthik Saripella
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIR INTAKE OF AN AIRCRAFT TURBINE ENGINE NACELLE
- Publication number 20220267019
- Publication date Aug 25, 2022
- SAFRAN NACELLES
- Alexis Yves-Marie Loncle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
REMOTE MOUNT OF ENGINE ACCESSORIES
- Publication number 20220250758
- Publication date Aug 11, 2022
- GENERAL ELECTRIC COMPANY
- Brian Lewis Devendorf
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT PROPULSION SYSTEM INLET STRUCTURE WITH VARIABLE AIRFLOW IN...
- Publication number 20220242586
- Publication date Aug 4, 2022
- Timothy Gormley
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT
- Publication number 20220205388
- Publication date Jun 30, 2022
- Rolls-Royce plc
- Natalie C. WONG
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DUCTED FAN CASE ATTACHMENT STRUCTURE
- Publication number 20220144442
- Publication date May 12, 2022
- Rohr, Inc.
- Michael Aten
- B64 - AIRCRAFT AVIATION COSMONAUTICS
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
HEAT EXCHANGER
- Publication number 20220112845
- Publication date Apr 14, 2022
- Rolls-Royce plc
- Stephen J. BRADBROOK
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
AIRCRAFT
- Publication number 20220112842
- Publication date Apr 14, 2022
- Rolls-Royce plc
- Natalie C. WONG
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE
- Publication number 20220063823
- Publication date Mar 3, 2022
- RAYTHEON TECHNOLOGIES CORPORATION
- DMITRIY B. SIDELKOVSKIY
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
NACELLE AIR INTAKE AND NACELLE COMPRISING SUCH AN AIR INTAKE
- Publication number 20220041295
- Publication date Feb 10, 2022
- SAFRAN NACELLES
- Gina FERRIER
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE AIR INTAKE AND NACELLE COMPRISING SUCH AN AIR INTAKE
- Publication number 20220041296
- Publication date Feb 10, 2022
- SAFRAN NACELLES
- Gina FERRIER
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ADVANCED INLET DESIGN
- Publication number 20210363921
- Publication date Nov 25, 2021
- The Boeing Company
- Holly J. Thomas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE FOR GAS TURBINE ENGINE
- Publication number 20210355873
- Publication date Nov 18, 2021
- Rolls-Royce plc
- Robert E CHRISTIE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHODS AND APPARATUS TO DETECT AIR FLOW SEPARATION OF AN ENGINE
- Publication number 20210332763
- Publication date Oct 28, 2021
- GENERAL ELECTRIC COMPANY
- Sai Venkata Kathik Saripella
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS
- Publication number 20210300542
- Publication date Sep 30, 2021
- Boom Technology, Inc.
- Nathaniel Blake Scholl
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS
- Publication number 20210300543
- Publication date Sep 30, 2021
- Boom Technology, Inc.
- Nathaniel Blake Scholl
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS
- Publication number 20210300544
- Publication date Sep 30, 2021
- Boom Technology, Inc.
- Nathaniel Blake Scholl
- B64 - AIRCRAFT AVIATION COSMONAUTICS

for turbofan engines

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

System and method for cooling a fluid of a lubrication or cooling c...

Nacelle air intake and nacelle comprising such an air intake

Multiple intake distortion adaptive fan for gas turbine engine

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

Aircraft propulsion system inlet structure with variable airflow in...

Aircraft

Fan arrangement for a gas turbine engine

Advanced inlet design

Assembly for a turbomachine

Ice accumulation and shedding mitigation for sensor probe

Supersonic aircraft turbofan engine

Air intake of an aircraft turbine engine nacelle

Nacelle air intake and nacelle comprising such an air intake

Aircraft having a single fluid inlet aperture

Turbofan engine, nacelle thereof, and associated method of operation

Propulsion unit with improved boundary layer ingestion

Turbofan gas turbine engine

Methods and apparatus to detect air flow separation of an engine

Variable geometry inlet system

Aircraft with a single fluid inlet aperture

Heat exchanger

Ducted fan case attachment structure

Hybrid propulsion for an aircraft

Nacelle forward part of a propulsion assembly comprising an incline...

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

Aircraft nacelle having a fan ramp with articulated flaps

Nacelle

Nacelle for gas turbine engine

Engine enclosure air inlet section

Gas turbine engine inlet

Patents Applicationslast 30 patents

NACELLE INLET STRUCTURE WITH FOAM CORE

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

AFT AIR INLET PARTICLE SEPARATOR FOR TURBINE ENGINE

VARIABLE COMPRESSION AIR INTAKES FOR AIRCRAFT PROPULSION SYSTEMS AN...

MULTIPLE INTAKE DISTORTION ADAPTIVE FAN FOR GAS TURBINE ENGINE

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET

Cowl Seal Assembly for an Aircraft Propulsion System

ASSEMBLY FOR A TURBOMACHINE

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

AIRCRAFT HAVING A SINGLE FLUID INLET APERTURE

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET

GAS TURBINE ENGINE INLET

METHODS AND APPARATUS TO DETECT AIR FLOW SEPARATION OF AN ENGINE

AIR INTAKE OF AN AIRCRAFT TURBINE ENGINE NACELLE

REMOTE MOUNT OF ENGINE ACCESSORIES

AIRCRAFT PROPULSION SYSTEM INLET STRUCTURE WITH VARIABLE AIRFLOW IN...

AIRCRAFT

DUCTED FAN CASE ATTACHMENT STRUCTURE

GAS TURBINE ENGINE COMPRESSION SYSTEM

HEAT EXCHANGER

AIRCRAFT

NACELLE

NACELLE AIR INTAKE AND NACELLE COMPRISING SUCH AN AIR INTAKE

NACELLE AIR INTAKE AND NACELLE COMPRISING SUCH AN AIR INTAKE

ADVANCED INLET DESIGN

NACELLE FOR GAS TURBINE ENGINE

METHODS AND APPARATUS TO DETECT AIR FLOW SEPARATION OF AN ENGINE

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS