Frédéric PIARD

Person

TOURNEFEUILLE, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Assembly for an aircraft nacelle and comprising a support panel, a...
- Patent number 12,139,267
- Issue date Nov 12, 2024
- Airbus Operations SAS
- Frédéric Piard
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft nacelle comprising a connection between ducts comprising f...
- Patent number 11,975,858
- Issue date May 7, 2024
- Airbus Operations SAS
- Lionel Czapla
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbofan comprising a nacelle equipped with a reverser system and a...
- Patent number 11,255,293
- Issue date Feb 22, 2022
- Airbus Operations SAS
- Pascal Gardes
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbojet including a nacelle equipped with a thrust reverser system...
- Patent number 11,187,188
- Issue date Nov 30, 2021
- Airbus Operations SAS
- Frédéric Ridray
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Jet engine comprising a nacelle equipped with a reverser system com...
- Patent number 11,168,644
- Issue date Nov 9, 2021
- Airbus Operations (S.A.S.)
- Laurent Presseq
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbojet engine comprising a nacelle equipped with a fan case and w...
- Patent number 11,161,619
- Issue date Nov 2, 2021
- Airbus Operations SAS
- Pascal Gardes
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Nacelle equipped with a thrust-reversing system comprising doors an...
- Patent number 11,143,141
- Issue date Oct 12, 2021
- Airbus Operations SAS
- Frédéric Ridray
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft cowl locking system
- Patent number 11,072,433
- Issue date Jul 27, 2021
- Airbus Operations (S.A.S.)
- Thierry Gaches
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Jet engine comprising a nacelle equipped with reverser flaps
- Patent number 10,995,700
- Issue date May 4, 2021
- Airbus Operations (S.A.S.)
- Frédéric Ridray
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Air intake structure for an aircraft nacelle
- Patent number 10,836,503
- Issue date Nov 17, 2020
- Airbus Operations (S.A.S.)
- Alain Porte
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turbofan comprising a series of rotatable blades for blocking off t...
- Patent number 10,830,089
- Issue date Nov 10, 2020
- Airbus Operations SAS
- Pascal Gardes
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet engine comprising a nacelle equipped with reverser flaps
- Patent number 10,690,088
- Issue date Jun 23, 2020
- Airbus Operations (S.A.S.)
- Frédéric Ridray
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbofan nacelle including a reverser flap
- Patent number 10,655,563
- Issue date May 19, 2020
- Airbus Operations (S.A.S.)
- Thierry Surply
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbojet engine comprising a nacelle equipped with reverser flaps
- Patent number 10,550,796
- Issue date Feb 4, 2020
- Airbus Operations SAS
- Olivier Pautis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
AIRCRAFT NACELLE COMPRISING A CONNECTION BETWEEN DUCTS COMPRISING F...
- Publication number 20230132103
- Publication date Apr 27, 2023
- Airbus Operations SAS
- Lionel CZAPLA
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ASSEMBLY FOR AN AIRCRAFT NACELLE AND COMPRISING A SUPPORT PANEL, A...
- Publication number 20230084689
- Publication date Mar 16, 2023
- Airbus Operations SAS
- Frédéric PIARD
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
COWL LOCKING SYSTEM
- Publication number 20200079516
- Publication date Mar 12, 2020
- AIRBUS OPERATIONS (SAS)
- Thierry Gaches
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
JET ENGINE COMPRISING A NACELLE EQUIPPED WITH A REVERSER SYSTEM COM...
- Publication number 20200080513
- Publication date Mar 12, 2020
- AIRBUS OPERATIONS (SAS)
- Laurent Presseq
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
JET ENGINE COMPRISING A NACELLE EQUIPPED WITH A THRUST REVERSING SY...
- Publication number 20200025139
- Publication date Jan 23, 2020
- Airbus Operations SAS
- Frédéric RIDRAY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOJET INCLUDING A NACELLE EQUIPPED WITH A THRUST REVERSER SYSTEM...
- Publication number 20190309704
- Publication date Oct 10, 2019
- Airbus Operations SAS
- Frédéric RIDRAY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE EQUIPPED WITH A REVERSER SYSTEM COMPRISING DOORS AND SYSTEM...
- Publication number 20190293019
- Publication date Sep 26, 2019
- Airbus Operations SAS
- Frédéric RIDRAY
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
NACELLE EQUIPPED WITH A THRUST-REVERSING SYSTEM COMPRISING DOORS AN...
- Publication number 20190293021
- Publication date Sep 26, 2019
- Airbus Operations SAS
- Frédéric RIDRAY
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBOFAN COMPRISING A SERIES OF ROTATABLE BLADES FOR BLOCKING OFF T...
- Publication number 20190284952
- Publication date Sep 19, 2019
- Airbus Operations SAS
- Pascal GARDES
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBOJET ENGINE COMPRISING A NACELLE EQUIPPED WITH A FAN CASE AND W...
- Publication number 20190283892
- Publication date Sep 19, 2019
- Airbus Operations SAS
- Pascal GARDES
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
JET ENGINE COMPRISING A NACELLE EQUIPPED WITH A THRUST REVERSING SY...
- Publication number 20190178206
- Publication date Jun 13, 2019
- Airbus Operations SAS
- Frédéric RIDRAY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOJET ENGINE COMPRISING A NACELLE EQUIPPED WITH REVERSER FLAPS
- Publication number 20190003421
- Publication date Jan 3, 2019
- Airbus Operations SAS
- Olivier PAUTIS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
JET ENGINE COMPRISING A NACELLE EQUIPPED WITH REVERSER FLAPS
- Publication number 20180372025
- Publication date Dec 27, 2018
- AIRBUS OPERATIONS (SAS)
- Frédéric Ridray
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT PROPULSION SYSTEM COMPRISING A NACELLE WITH AN ENHANCED OP...
- Publication number 20180346138
- Publication date Dec 6, 2018
- Airbus Operations SAS
- Frédéric RIDRAY
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
JET ENGINE COMPRISING A NACELLE EQUIPPED WITH REVERSER FLAPS
- Publication number 20180274484
- Publication date Sep 27, 2018
- AIRBUS OPERATIONS (SAS)
- Frédéric Ridray
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
AIR INTAKE STRUCTURE FOR AN AIRCRAFT NACELLE
- Publication number 20180201387
- Publication date Jul 19, 2018
- Airbus (S.A.S.)
- Alain Porte
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOFAN NACELLE INCLUDING A REVERSER FLAP
- Publication number 20180149113
- Publication date May 31, 2018
- AIRBUS OPERATIONS (SAS)
- Thierry Surply
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE OF A TURBOJET ENGINE COMPRISING AN INVERTER FLAP
- Publication number 20180106216
- Publication date Apr 19, 2018
- Airbus Operations SAS
- Nicolas JOLIVET
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Frédéric PIARD

Person

Patents Grantslast 30 patents

Assembly for an aircraft nacelle and comprising a support panel, a...

Aircraft nacelle comprising a connection between ducts comprising f...

Turbofan comprising a nacelle equipped with a reverser system and a...

Turbojet including a nacelle equipped with a thrust reverser system...

Jet engine comprising a nacelle equipped with a reverser system com...

Turbojet engine comprising a nacelle equipped with a fan case and w...

Nacelle equipped with a thrust-reversing system comprising doors an...

Aircraft cowl locking system

Jet engine comprising a nacelle equipped with reverser flaps

Air intake structure for an aircraft nacelle

Turbofan comprising a series of rotatable blades for blocking off t...

Jet engine comprising a nacelle equipped with reverser flaps

Turbofan nacelle including a reverser flap

Turbojet engine comprising a nacelle equipped with reverser flaps

Patents Applicationslast 30 patents

AIRCRAFT NACELLE COMPRISING A CONNECTION BETWEEN DUCTS COMPRISING F...

ASSEMBLY FOR AN AIRCRAFT NACELLE AND COMPRISING A SUPPORT PANEL, A...

COWL LOCKING SYSTEM

JET ENGINE COMPRISING A NACELLE EQUIPPED WITH A REVERSER SYSTEM COM...

JET ENGINE COMPRISING A NACELLE EQUIPPED WITH A THRUST REVERSING SY...

TURBOJET INCLUDING A NACELLE EQUIPPED WITH A THRUST REVERSER SYSTEM...

NACELLE EQUIPPED WITH A REVERSER SYSTEM COMPRISING DOORS AND SYSTEM...

NACELLE EQUIPPED WITH A THRUST-REVERSING SYSTEM COMPRISING DOORS AN...

TURBOFAN COMPRISING A SERIES OF ROTATABLE BLADES FOR BLOCKING OFF T...

TURBOJET ENGINE COMPRISING A NACELLE EQUIPPED WITH A FAN CASE AND W...

JET ENGINE COMPRISING A NACELLE EQUIPPED WITH A THRUST REVERSING SY...

TURBOJET ENGINE COMPRISING A NACELLE EQUIPPED WITH REVERSER FLAPS

JET ENGINE COMPRISING A NACELLE EQUIPPED WITH REVERSER FLAPS

AIRCRAFT PROPULSION SYSTEM COMPRISING A NACELLE WITH AN ENHANCED OP...

JET ENGINE COMPRISING A NACELLE EQUIPPED WITH REVERSER FLAPS

AIR INTAKE STRUCTURE FOR AN AIRCRAFT NACELLE

TURBOFAN NACELLE INCLUDING A REVERSER FLAP

NACELLE OF A TURBOJET ENGINE COMPRISING AN INVERTER FLAP