comprising de-icing means

Industry

CPC
B64D2033/0233

This industry / category may be too specific. Please go to a parent level for more data

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

B64D2033/0233comprising de-icing means

Industries

Patents Grantslast 30 patents

Information Patent Grant
Selectively meltable adhesives for bonding of deicers
- Patent number 12,104,090
- Issue date Oct 1, 2024
- Goodrich Corporation
- Nathaniel Ching
- B82 - NANO-TECHNOLOGY
Information Patent Grant
Inlet cone for an aircraft turbomachine
- Patent number 12,104,498
- Issue date Oct 1, 2024
- SAFRAN AIRCRAFT ENGINES
- Alban Francois Louis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Aircraft part anti-icing treatment method
- Patent number 12,104,526
- Issue date Oct 1, 2024
- SAFRAN NACELLES
- Audrey Riquet
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Aircraft equipped with a structurally integrated de-icing system
- Patent number 12,091,177
- Issue date Sep 17, 2024
- Politecnico Di Torino
- Paolo Maggiore
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Supersonic speed attenuator of an air intake of an aircraft propuls...
- Patent number 12,037,941
- Issue date Jul 16, 2024
- SAFRAN NACELLES
- Jean-Philippe Joret
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method for manufacturing deicing acoustic skin for an aircraft acou...
- Patent number 12,023,879
- Issue date Jul 2, 2024
- Airbus Operations SAS
- Alain Porte
- B32 - LAYERED PRODUCTS
Information Patent Grant
Integrated microwave thermal anti-icing system
- Patent number 12,017,779
- Issue date Jun 25, 2024
- Rohr, Inc.
- Steven M. Kestler
- B32 - LAYERED PRODUCTS
Information Patent Grant
Aircraft turboprop engine inlet compact profile configuration to im...
- Patent number 12,012,891
- Issue date Jun 18, 2024
- AMERICAN AVIATION, Inc
- Stephen R. Speer
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Microwave thermal anti-icing system for aircraft acoustic structure
- Patent number 12,012,212
- Issue date Jun 18, 2024
- Rohr, Inc.
- Steven M. Kestler
- B32 - LAYERED PRODUCTS
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
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
Auxiliary power unit startup condition prediction
- Patent number 11,854,383
- Issue date Dec 26, 2023
- The Boeing Company
- Omid B. Nakhjavani
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Grant
Vehicle provided, at the intake, with an heatable air filter provid...
- Patent number 11,845,034
- Issue date Dec 19, 2023
- BMC S.r.l.
- Gaetano Bergami
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Valve assembly
- Patent number 11,840,345
- Issue date Dec 12, 2023
- MICROTECNICA S.R.L.
- Giacomo Mezzino
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
Thermal management system for a gas turbine engine
- Patent number 11,788,469
- Issue date Oct 17, 2023
- General Electric Company
- Steven Douglas Johnson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Ice reduction mechanism for turbofan engine
- Patent number 11,739,689
- Issue date Aug 29, 2023
- General Electric Company
- Arthur William Sibbach
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft engine nacelle provided with an icing protection system an...
- Patent number 11,702,213
- Issue date Jul 18, 2023
- Airbus Operations SAS
- Alain Porte
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Pressure regulating valve assembly
- Patent number 11,697,503
- Issue date Jul 11, 2023
- Rolls-Royce Deutschland Ltd & Co KG
- Paul Julian Wells
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Method for manufacturing a cellular core for an acoustic panel
- Patent number 11,694,669
- Issue date Jul 4, 2023
- SAFRAN NACELLES
- Quentin Alban Guillaume Benard
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Aircraft engine nacelle comprising a system of ice protection
- Patent number 11,643,216
- Issue date May 9, 2023
- Airbus Operations SAS
- Alain Porte
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Icing detector
- Patent number 11,623,754
- Issue date Apr 11, 2023
- Israel Aerospace Industries Ltd.
- Daniel Marom
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Additively manufactured booster splitter with integral heating pass...
- Patent number 11,624,320
- Issue date Apr 11, 2023
- General Electric Company
- Nicholas Joseph Kray
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Selectively meltable adhesives for bonding of deicers
- Patent number 11,623,753
- Issue date Apr 11, 2023
- Goodrich Corporation
- Nathaniel Ching
- B82 - NANO-TECHNOLOGY
Information Patent Grant
Nozzle for a thermal anti-icing system
- Patent number 11,613,373
- Issue date Mar 28, 2023
- Rohr, Inc.
- Radhakrishna Chilukuri
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable diameter piccolo tube for anti-icing system
- Patent number 11,577,844
- Issue date Feb 14, 2023
- Rohr, Inc.
- Joewin Joy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft engine nacelle comprising an anti-icing protection system
- Patent number 11,518,526
- Issue date Dec 6, 2022
- Airbus Operations SAS
- Alain Porte
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotor blade retention system for a gas turbine engine
- Patent number 11,519,278
- Issue date Dec 6, 2022
- General Electric Company
- Nicholas Joseph Kray
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
SEGMENTED NACELLE INLET LIP WITH ELECTRIC THERMAL ANTI-ICING SYSTEM
- Publication number 20240367802
- Publication date Nov 7, 2024
- Rohr, Inc.
- Brian A. Sherman
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRCRAFT TURBOPROP ENGINE INLET COMPACT PROFILE CONFIGURATION
- Publication number 20240301826
- Publication date Sep 12, 2024
- American Aviation, Inc.
- Stephen R. Speer
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LIP SKIN FOR AN AIRCRAFT AEROSTRUCTURE
- Publication number 20240253790
- Publication date Aug 1, 2024
- Rohr, Inc.
- Xiaolan Hu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT ANTI-ICING SYSTEM
- Publication number 20240254894
- Publication date Aug 1, 2024
- Rohr, Inc.
- Pratap Mallampati
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ICE PROTECTION BACKUP TEMPERATURE CONTROL LOGIC
- Publication number 20240228046
- Publication date Jul 11, 2024
- GOODRICH CORPORATION
- Richard J. Carpino II
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT THERMAL ANTI-ICING SYSTEM
- Publication number 20240190573
- Publication date Jun 13, 2024
- Francois Belleville
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INLET CONE FOR AN AIRCRAFT TURBOMACHINE
- Publication number 20240167394
- Publication date May 23, 2024
- SAFRAN AIRCRAFT ENGINES
- Alban Francois LOUIS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ICE PROTECTION BACKUP TEMPERATURE CONTROL LOGIC
- Publication number 20240132219
- Publication date Apr 25, 2024
- GOODRICH CORPORATION
- Richard J. Carpino II
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
THERMAL ANTI-ICING SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM
- Publication number 20240077018
- Publication date Mar 7, 2024
- PramodaKumar Nayak
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SUPERSONIC SPEED ATTENUATOR OF AN AIR INTAKE OF AN AIRCRAFT PROPULS...
- Publication number 20240018903
- Publication date Jan 18, 2024
- SAFRAN NACELLES
- Jean-Philippe Joret
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT FLUID ICE PROTECTION SYSTEM
- Publication number 20240017839
- Publication date Jan 18, 2024
- The Boeing Company
- Charles William Rust
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE
- Publication number 20240003294
- Publication date Jan 4, 2024
- GENERAL ELECTRIC COMPANY
- Arthur William Sibbach
- 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
ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE
- Publication number 20230053554
- Publication date Feb 23, 2023
- GENERAL ELECTRIC COMPANY
- Arthur William Sibbach
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INTEGRATED MICROWAVE THERMAL ANTI-ICING SYSTEM
- Publication number 20230002064
- Publication date Jan 5, 2023
- Steven M. Kestler
- B32 - LAYERED PRODUCTS
Information Patent Application
VALVE ASSEMBLY
- Publication number 20220315227
- Publication date Oct 6, 2022
- MICROTECNICA S.R.L.
- Giacomo MEZZINO
- 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
AIR INTAKE LIP OF AN AIRCRAFT ENGINE NACELLE, COMPRISING AT LEAST O...
- Publication number 20220219831
- Publication date Jul 14, 2022
- SAFRAN NACELLES
- Patrick Gonidec
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIR INTAKE LIP OF A TURBOMACHINE NACELLE COMPRISING AN ACOUSTIC DEV...
- Publication number 20220212809
- Publication date Jul 7, 2022
- SAFRAN NACELLES
- Virginie Emmanuelle Anne-Marie Digeos
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ANTI-ICING SYSTEM WITH A FLOW-DEFLECTOR ASSEMBLY
- Publication number 20220195921
- Publication date Jun 23, 2022
- GENERAL ELECTRIC COMPANY
- Francisco Gomez
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ANTI-ICING FOR GAS TURBINE SYSTEM
- Publication number 20220195922
- Publication date Jun 23, 2022
- GENERAL ELECTRIC COMPANY
- Francisco Gomez
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PRESSURE REGULATING VALVE ASSEMBLY
- Publication number 20220127005
- Publication date Apr 28, 2022
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Paul Julian WELLS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ADDITIVELY MANUFACTURED BOOSTER SPLITTER WITH INTEGRAL HEATING PASS...
- Publication number 20220074344
- Publication date Mar 10, 2022
- GENERAL ELECTRIC COMPANY
- Nicholas Joseph Kray
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VEHICLE PROVIDED, AT THE INTAKE, WITH AN HEATABLE AIR FILTER PROVID...
- Publication number 20210394110
- Publication date Dec 23, 2021
- Gaetano Bergami
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
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
NOZZLE FOR A THERMAL ANTI-ICING SYSTEM
- Publication number 20210284351
- Publication date Sep 16, 2021
- Radhakrishna Chilukuri
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
VARIABLE DIAMETER PICCOLO TUBE FOR ANTI-ICING SYSTEM
- Publication number 20210284346
- Publication date Sep 16, 2021
- Rohr, Inc.
- Joewin Joy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT PART ANTI-ICING TREATMENT METHOD
- Publication number 20210156305
- Publication date May 27, 2021
- SAFRAN NACELLES
- Audrey RIQUET
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
AIR INLET, NACELLE, PROPULSIVE ASSEMBLY AND AIRCRAFT WITH GROOVED LIP
- Publication number 20210078718
- Publication date Mar 18, 2021
- Airbus Operations SAS
- Arnaud BOURHIS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ANTERIOR PART OF A NACELLE OF AN AIRCRAFT PROPULSION SYSTEM HAVING...
- Publication number 20210040867
- Publication date Feb 11, 2021
- AIRBUS OPERATIONS (SAS)
- Alain Porte
- B64 - AIRCRAFT AVIATION COSMONAUTICS

comprising de-icing means

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Selectively meltable adhesives for bonding of deicers

Inlet cone for an aircraft turbomachine

Aircraft part anti-icing treatment method

Aircraft equipped with a structurally integrated de-icing system

Supersonic speed attenuator of an air intake of an aircraft propuls...

Method for manufacturing deicing acoustic skin for an aircraft acou...

Integrated microwave thermal anti-icing system

Aircraft turboprop engine inlet compact profile configuration to im...

Microwave thermal anti-icing system for aircraft acoustic structure

Advanced inlet design

Assembly for a turbomachine

Ice accumulation and shedding mitigation for sensor probe

Air intake of an aircraft turbine engine nacelle

Auxiliary power unit startup condition prediction

Vehicle provided, at the intake, with an heatable air filter provid...

Valve assembly

Turbofan engine, nacelle thereof, and associated method of operation

Thermal management system for a gas turbine engine

Ice reduction mechanism for turbofan engine

Aircraft engine nacelle provided with an icing protection system an...

Pressure regulating valve assembly

Method for manufacturing a cellular core for an acoustic panel

Aircraft engine nacelle comprising a system of ice protection

Icing detector

Additively manufactured booster splitter with integral heating pass...

Selectively meltable adhesives for bonding of deicers

Nozzle for a thermal anti-icing system

Variable diameter piccolo tube for anti-icing system

Aircraft engine nacelle comprising an anti-icing protection system

Rotor blade retention system for a gas turbine engine

Patents Applicationslast 30 patents

SEGMENTED NACELLE INLET LIP WITH ELECTRIC THERMAL ANTI-ICING SYSTEM

AIRCRAFT TURBOPROP ENGINE INLET COMPACT PROFILE CONFIGURATION

LIP SKIN FOR AN AIRCRAFT AEROSTRUCTURE

AIRCRAFT ANTI-ICING SYSTEM

ICE PROTECTION BACKUP TEMPERATURE CONTROL LOGIC

AIRCRAFT THERMAL ANTI-ICING SYSTEM

INLET CONE FOR AN AIRCRAFT TURBOMACHINE

ICE PROTECTION BACKUP TEMPERATURE CONTROL LOGIC

THERMAL ANTI-ICING SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM

SUPERSONIC SPEED ATTENUATOR OF AN AIR INTAKE OF AN AIRCRAFT PROPULS...

AIRCRAFT FLUID ICE PROTECTION SYSTEM

ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE

ASSEMBLY FOR A TURBOMACHINE

ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE

INTEGRATED MICROWAVE THERMAL ANTI-ICING SYSTEM

VALVE ASSEMBLY

AIR INTAKE OF AN AIRCRAFT TURBINE ENGINE NACELLE

AIR INTAKE LIP OF AN AIRCRAFT ENGINE NACELLE, COMPRISING AT LEAST O...

AIR INTAKE LIP OF A TURBOMACHINE NACELLE COMPRISING AN ACOUSTIC DEV...

ANTI-ICING SYSTEM WITH A FLOW-DEFLECTOR ASSEMBLY

ANTI-ICING FOR GAS TURBINE SYSTEM

PRESSURE REGULATING VALVE ASSEMBLY

ADDITIVELY MANUFACTURED BOOSTER SPLITTER WITH INTEGRAL HEATING PASS...

VEHICLE PROVIDED, AT THE INTAKE, WITH AN HEATABLE AIR FILTER PROVID...

ADVANCED INLET DESIGN

NOZZLE FOR A THERMAL ANTI-ICING SYSTEM

VARIABLE DIAMETER PICCOLO TUBE FOR ANTI-ICING SYSTEM

AIRCRAFT PART ANTI-ICING TREATMENT METHOD

AIR INLET, NACELLE, PROPULSIVE ASSEMBLY AND AIRCRAFT WITH GROOVED LIP

ANTERIOR PART OF A NACELLE OF AN AIRCRAFT PROPULSION SYSTEM HAVING...