Jean-Claude Christian Taillant

Person

Vauz le Penil, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Low pressure turbine for an aircraft turbomachine, comprising a seg...
- Patent number 8,979,489
- Issue date Mar 17, 2015
- SNECMA
- Jean-Claude Christian Taillant
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Ventilation for a turbine wheel in a turbine engine
- Patent number 8,336,317
- Issue date Dec 25, 2012
- SNECMA
- Stéphane Pierre Guillaume Blanchard
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Turbomachine with contrarotating fans
- Patent number 7,458,773
- Issue date Dec 2, 2008
- SNECMA
- Michel Brault
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turboshaft engine comprising two elements connected to each other w...
- Patent number 7,140,840
- Issue date Nov 28, 2006
- SNECMA Moteurs
- Jean-Claude Taillant
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Gas turbine with stator shroud in the cavity beneath the chamber
- Patent number 7,036,320
- Issue date May 2, 2006
- SNECMA Moteurs
- Sylvie Coulon
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbomachine with cooled ring segments
- Patent number 7,011,493
- Issue date Mar 14, 2006
- SNECMA Moteurs
- Marc Marchi
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Ventilation device for a high pressure turbine rotor of a turbomachine
- Patent number 6,916,151
- Issue date Jul 12, 2005
- SNECMA Moteurs
- Maurice Judet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Cooling the upstream end plate of a high pressure turbine by means...
- Patent number 6,787,947
- Issue date Sep 7, 2004
- SNECMA Moteurs
- Sylvie Coulon
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbomachine including a device for supplying pressurized gas
- Patent number 6,334,755
- Issue date Jan 1, 2002
- SNECMA Moteurs
- Xavier Gérard André Coudray
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbine vane cooling system
- Patent number 5,993,156
- Issue date Nov 30, 1999
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Yves Maurice Bailly
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Device for blowing gases for regulating clearances in a gas turbine...
- Patent number 5,980,201
- Issue date Nov 9, 1999
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation
- Josette Benoist
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Layout and process for adjusting the diameter of a stator ring
- Patent number 5,915,919
- Issue date Jun 29, 1999
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Claude Taillant
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Labyrinth disk with built-in stiffener for turbomachine rotor
- Patent number 5,816,776
- Issue date Oct 6, 1998
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Frederic Chambon
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Cooled turbine guide vane
- Patent number 5,772,398
- Issue date Jun 30, 1998
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Isabelle Marie-Agnes Noiret
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Sectored, one-piece nozzle of a turbine engine turbine stator
- Patent number 5,752,804
- Issue date May 19, 1998
- Societe Nationale d'etude et de Construction de Monteurs d'Aviation "Snecma"
- Josette Benoist
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Unsectored, one piece distributor of a turbojet turbine stator
- Patent number 5,645,398
- Issue date Jul 8, 1997
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Josette Benoist
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Seal for gas turbine rotor blades
- Patent number 5,599,170
- Issue date Feb 4, 1997
- Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
- Marc R. Marchi
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
System for removably mounting a pre-vaporizing bowl to a combustion...
- Patent number 5,222,358
- Issue date Jun 29, 1993
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M...
- Guillaume H. Chaput
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fixing arrangement for mounting an annular member on a disk of a tu...
- Patent number 5,173,024
- Issue date Dec 22, 1992
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation
- Jacques H. Mouchel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
AIRCRAFT TURBOMACHINE COMPRISING AN ELECTRIC MACHINE
- Publication number 20250052203
- Publication date Feb 13, 2025
- SAFRAN AIRCRAFT ENGINES
- Jean-Claude Christian TAILLANT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM FOR CONTROLLING THE PITCH SETTING OF A PROPELLER VANE FOR AN...
- Publication number 20250035009
- Publication date Jan 30, 2025
- SAFRAN AIRCRAFT ENGINES
- Régis Eugène Henri SERVANT
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
SLEEVE MOUNTED ONTO A LOW-PRESSURE SHAFT IN A TURBOMACHINE
- Publication number 20240337201
- Publication date Oct 10, 2024
- SAFRAN AIRCRAFT ENGINES
- Vianney SIMON
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
FAN MODULE EQUIPPED WITH AN OIL TRANSFER DEVICE
- Publication number 20240151149
- Publication date May 9, 2024
- SAFRAN AIRCRAFT ENGINES
- Paul Ghislain Albert LEVISSE
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
LOW PRESSURE TURBINE FOR AN AIRCRAFT TURBOMACHINE, COMPRISING A SEG...
- Publication number 20120134788
- Publication date May 31, 2012
- SNECMA
- Jean-Claude Christian TAILLANT
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
VENTILATION FOR A TURBINE WHEEL IN A TURBINE ENGINE
- Publication number 20110072832
- Publication date Mar 31, 2011
- SNECMA
- Stephane Pierre Guillaume BLANCHARD
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbomachine with contrarotating fans
- Publication number 20070006569
- Publication date Jan 11, 2007
- SNECMA
- Michel Brault
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Gas turbine ventilation circuitry
- Publication number 20050201859
- Publication date Sep 15, 2005
- Sylvie Coulon
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Gas turbine with stator shround in the cavity beneath the chamber
- Publication number 20050172642
- Publication date Aug 11, 2005
- SNECMA MOTEURS
- Sylvie Coulon
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turboshaft engine comprising two elements connected to each other w...
- Publication number 20050095123
- Publication date May 5, 2005
- SNECMA MOTEURS
- Jean-Claude Taillant
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Ventilation device for a high pressure turbine rotor of a turbomachine
- Publication number 20040219008
- Publication date Nov 4, 2004
- SNECMA MOTEURS
- Maurice Judet
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turbomachine with cooled ring segments
- Publication number 20040219009
- Publication date Nov 4, 2004
- SNECMA MOTEURS
- Marc Marchi
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Cooling the upstream end plate of a high pressure turbine by means...
- Publication number 20030223893
- Publication date Dec 4, 2003
- SNECMA MOTEURS
- Sylvie Coulon
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Jean-Claude Christian Taillant

Person

Patents Grantslast 30 patents

Low pressure turbine for an aircraft turbomachine, comprising a seg...

Ventilation for a turbine wheel in a turbine engine

Turbomachine with contrarotating fans

Turboshaft engine comprising two elements connected to each other w...

Gas turbine with stator shroud in the cavity beneath the chamber

Turbomachine with cooled ring segments

Ventilation device for a high pressure turbine rotor of a turbomachine

Cooling the upstream end plate of a high pressure turbine by means...

Turbomachine including a device for supplying pressurized gas

Turbine vane cooling system

Device for blowing gases for regulating clearances in a gas turbine...

Layout and process for adjusting the diameter of a stator ring

Labyrinth disk with built-in stiffener for turbomachine rotor

Cooled turbine guide vane

Sectored, one-piece nozzle of a turbine engine turbine stator

Unsectored, one piece distributor of a turbojet turbine stator

Seal for gas turbine rotor blades

System for removably mounting a pre-vaporizing bowl to a combustion...

Fixing arrangement for mounting an annular member on a disk of a tu...

Patents Applicationslast 30 patents

AIRCRAFT TURBOMACHINE COMPRISING AN ELECTRIC MACHINE

SYSTEM FOR CONTROLLING THE PITCH SETTING OF A PROPELLER VANE FOR AN...

SLEEVE MOUNTED ONTO A LOW-PRESSURE SHAFT IN A TURBOMACHINE

FAN MODULE EQUIPPED WITH AN OIL TRANSFER DEVICE

LOW PRESSURE TURBINE FOR AN AIRCRAFT TURBOMACHINE, COMPRISING A SEG...

VENTILATION FOR A TURBINE WHEEL IN A TURBINE ENGINE

Turbomachine with contrarotating fans

Gas turbine ventilation circuitry

Gas turbine with stator shround in the cavity beneath the chamber

Turboshaft engine comprising two elements connected to each other w...

Ventilation device for a high pressure turbine rotor of a turbomachine

Turbomachine with cooled ring segments

Cooling the upstream end plate of a high pressure turbine by means...