Michel Desaulty

Person

Vert Saint Denis, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Turbomachine annular combustion chamber
- Patent number 7,155,913
- Issue date Jan 2, 2007
- SNECMA Moteurs
- Frederic Beule
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Optimally cooled, carbureted flameholder
- Patent number 6,112,516
- Issue date Sep 5, 2000
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M...
- Frederic Bruno Beule
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Reduced pollution combustion chamber having an annular fuel injector
- Patent number 5,937,653
- Issue date Aug 17, 1999
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Jean-Paul Daniel Alary
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Device for actively controlling combustion instabilities and for de...
- Patent number 5,797,266
- Issue date Aug 25, 1998
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Marie Brocard
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Method of preventing instabilities produced by combustion in a turb...
- Patent number 5,699,663
- Issue date Dec 23, 1997
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Jean-Yves Capelle
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine diffuser
- Patent number 5,592,820
- Issue date Jan 14, 1997
- Societe National D'Etdue et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
- Jean-Paul D. Alary
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Pre-mixing injection system for a turbojet engine
- Patent number 5,592,819
- Issue date Jan 14, 1997
- Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
- Denis R. H. Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Perforated wall for a gas turbine engine
- Patent number 5,590,531
- Issue date Jan 7, 1997
- Societe National D'Etdue et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
- Michel A. A. Desaulty
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
System for supplying fuel to and cooling a fuel injector of a dual...
- Patent number 5,568,721
- Issue date Oct 29, 1996
- Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
- Jean-Paul D. Alary
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas-flow separator for a double dome gas turbine engine combustion...
- Patent number 5,528,896
- Issue date Jun 25, 1996
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Jean-Paul D. Alary
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Separator for an annular gas turbine combustion chamber
- Patent number 5,417,069
- Issue date May 23, 1995
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Jean-Paul D. Alary
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel/oxidizer premixing combustion chamber
- Patent number 5,341,645
- Issue date Aug 30, 1994
- Societe National d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M.A.)
- Denis R. H. Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine with improved water ingestion prevention
- Patent number 5,339,622
- Issue date Aug 23, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Xavier M. H. Bardey
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Combustion chamber with axially displaced fuel injectors
- Patent number 5,335,491
- Issue date Aug 9, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Gerard Y. G. Barbier
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Low pollution combustion chamber for a turbojet engine
- Patent number 5,295,354
- Issue date Mar 22, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M...
- Gerard Y. G. Barbier
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Lean premixture combustion-chamber comprising a counterflow enclosu...
- Patent number 5,261,239
- Issue date Nov 16, 1993
- Societe Nationale d'Etude et de Construction de Motors d'Aviation
- Gerard Y. G. Barbier
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine combustion chamber with oxidizer intake flow con...
- Patent number 5,235,805
- Issue date Aug 17, 1993
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M...
- Gerard Y. G. Barbier
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Variable volume combustion chamber for a gas turbine engine
- Patent number 5,211,675
- Issue date May 18, 1993
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation
- Xavier M. H. Bardey
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Counter flow combustion chamber for a gas turbine engine
- Patent number 5,209,066
- Issue date May 11, 1993
- Societe Nationale d'Etude et de Construction de Moteurs
- Gerard Y. G. Barbier
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine combustion chamber wall structure for minimizing coolin...
- Patent number 5,209,067
- Issue date May 11, 1993
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Gerard Y. G. Barbier
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Combustion chamber structure for a turbojet engine
- Patent number 4,805,397
- Issue date Feb 21, 1989
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Gerard Y. G. Barbier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Enlarged bowl member for a turbojet engine combustion chamber
- Patent number 4,766,722
- Issue date Aug 30, 1988
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Gerard J. P. Bayle-Laboure
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Axial-centripetal swirler injection apparatus
- Patent number 4,754,600
- Issue date Jul 5, 1988
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Gerard Y. G. Barbier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable flow air-fuel mixing device for a turbojet engine
- Patent number 4,726,182
- Issue date Feb 23, 1988
- 501 Societe Nationale d'Etude et de Construction de Meteur d'Aviation-S.N.E.C...
- Gerard Y. G. Barbier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
Turbomachine annular combustion chamber
- Publication number 20050042076
- Publication date Feb 24, 2005
- SNECMA MOTEURS
- Frederic Beule
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Michel Desaulty

Person

Patents Grantslast 30 patents

Turbomachine annular combustion chamber

Optimally cooled, carbureted flameholder

Reduced pollution combustion chamber having an annular fuel injector

Device for actively controlling combustion instabilities and for de...

Method of preventing instabilities produced by combustion in a turb...

Gas turbine diffuser

Pre-mixing injection system for a turbojet engine

Perforated wall for a gas turbine engine

System for supplying fuel to and cooling a fuel injector of a dual...

Gas-flow separator for a double dome gas turbine engine combustion...

Separator for an annular gas turbine combustion chamber

Fuel/oxidizer premixing combustion chamber

Gas turbine engine with improved water ingestion prevention

Combustion chamber with axially displaced fuel injectors

Low pollution combustion chamber for a turbojet engine

Lean premixture combustion-chamber comprising a counterflow enclosu...

Gas turbine engine combustion chamber with oxidizer intake flow con...

Variable volume combustion chamber for a gas turbine engine

Counter flow combustion chamber for a gas turbine engine

Gas turbine combustion chamber wall structure for minimizing coolin...

Combustion chamber structure for a turbojet engine

Enlarged bowl member for a turbojet engine combustion chamber

Axial-centripetal swirler injection apparatus

Variable flow air-fuel mixing device for a turbojet engine

Patents Applicationslast 30 patents

Turbomachine annular combustion chamber