Denis Roger Henri Ansart

Person

Bois le Ros, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Control of cooling flows for high-temperature combustion chambers h...
- Patent number 6,105,371
- Issue date Aug 22, 2000
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Denis Roger Henri Ansart
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbomachine combustion chamber with inner and outer injector rows
- Patent number 6,070,412
- Issue date Jun 6, 2000
- Societe National d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
- Denis Roger Henri Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel injection system with improved air/fuel homogenization
- Patent number 5,941,075
- Issue date Aug 24, 1999
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (SNECMA)
- Denis Roger Henri Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine combustion chamber for optimizing the mixture of...
- Patent number 5,934,067
- Issue date Aug 10, 1999
- Societe National d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M.A.)
- Denis Roger Henri Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Combustion chamber having a multi-hole cooling system with variably...
- Patent number 5,775,108
- Issue date Jul 7, 1998
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Denis Roger Henri Ansart
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Annular combustion chamber with a perforated wall
- Patent number 5,713,207
- Issue date Feb 3, 1998
- Societe National d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
- Denis Roger Henri Ansart
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Fuel injection assembly for a gas turbine engine
- Patent number 5,651,252
- Issue date Jul 29, 1997
- Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
- Denis Roger Henri Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Dual head combustion chamber
- Patent number 5,642,621
- Issue date Jul 1, 1997
- Socoiete Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
- Jean-Paul Daniel Alary
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Method of supplying fuel to a dual head combustion chamber
- Patent number 5,634,328
- Issue date Jun 3, 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
Double wall construction for a gas turbine combustion chamber
- Patent number 5,598,697
- Issue date Feb 4, 1997
- Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
- Christine J. M. Ambrogi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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
Fixing arrangement for a thermal protection tile in a combustion ch...
- Patent number 5,560,197
- Issue date Oct 1, 1996
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Denis R. H. Ansart
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Fixing arrangement for a thermal protection tile in a combustion ch...
- Patent number 5,501,071
- Issue date Mar 26, 1996
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Denis R. H. Ansart
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Cladded combustion chamber construction
- Patent number 5,499,499
- Issue date Mar 19, 1996
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation
- Christine J. M. Ambrogi
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Fuel injection system for a gas turbine combustor including radial...
- Patent number 5,437,159
- Issue date Aug 1, 1995
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation (S.N.E.C.M...
- Denis R. H. Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Aerodynamic fuel injection system for a gas turbine combustion chamber
- Patent number 5,351,475
- Issue date Oct 4, 1994
- Societe Nationale d'Etude et de Construction de Motors d'Aviation
- Denis R. H. Ansart
- 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 separator for a combustion chamber
- Patent number 5,311,743
- Issue date May 17, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Denis R. H. Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
System for reducing nitrogen-oxide emissions from a gas turbine engine
- Patent number 5,285,630
- Issue date Feb 15, 1994
- Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
- Denis R. H. Ansart
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Denis Roger Henri Ansart

Person

Patents Grantslast 30 patents

Control of cooling flows for high-temperature combustion chambers h...

Turbomachine combustion chamber with inner and outer injector rows

Fuel injection system with improved air/fuel homogenization

Gas turbine engine combustion chamber for optimizing the mixture of...

Combustion chamber having a multi-hole cooling system with variably...

Annular combustion chamber with a perforated wall

Fuel injection assembly for a gas turbine engine

Dual head combustion chamber

Method of supplying fuel to a dual head combustion chamber

Double wall construction for a gas turbine combustion chamber

Pre-mixing injection system for a turbojet engine

Fixing arrangement for a thermal protection tile in a combustion ch...

Fixing arrangement for a thermal protection tile in a combustion ch...

Cladded combustion chamber construction

Fuel injection system for a gas turbine combustor including radial...

Aerodynamic fuel injection system for a gas turbine combustion chamber

Fuel/oxidizer premixing combustion chamber

Gas separator for a combustion chamber

System for reducing nitrogen-oxide emissions from a gas turbine engine