P

Inventor

DESAULTY MICHEL A A

FR20 patents
⚠️ This page may combine multiple inventors who share the name “DESAULTY MICHEL A A”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

SNECMA

18 patents
US5235805AAug 17, 1993

Gas turbine engine combustion chamber with oxidizer intake flow control

SNECMA62 citations95
US4754600AJul 5, 1988

Axial-centripetal swirler injection apparatus

SNECMA57 citations94
US5341645AAug 30, 1994

Fuel/oxidizer premixing combustion chamber

SNECMA33 citations92
US5295354AMar 22, 1994

Low pollution combustion chamber for a turbojet engine

SNECMA22 citations92
US5211675AMay 18, 1993

Variable volume combustion chamber for a gas turbine engine

SNECMA27 citations92
US5209066AMay 11, 1993

Counter flow combustion chamber for a gas turbine engine

SNECMA24 citations92
US5592819AJan 14, 1997

Pre-mixing injection system for a turbojet engine

SNECMA80 citations91
US5568721AOct 29, 1996

System for supplying fuel to and cooling a fuel injector of a dual head combustion chamber

SNECMA27 citations91
US5417069AMay 23, 1995

Separator for an annular gas turbine combustion chamber

SNECMA24 citations91
US4901522AFeb 20, 1990

Turbojet engine combustion chamber with a double wall converging zone

SNECMA117 citations91
US4766722AAug 30, 1988

Enlarged bowl member for a turbojet engine combustion chamber

SNECMA34 citations91
US4805397AFeb 21, 1989

Combustion chamber structure for a turbojet engine

SNECMA57 citations90
US4726182AFeb 23, 1988

Variable flow air-fuel mixing device for a turbojet engine

SNECMA44 citations90
US5339622AAug 23, 1994

Gas turbine engine with improved water ingestion prevention

SNECMA30 citations87
US5209067AMay 11, 1993

Gas turbine combustion chamber wall structure for minimizing cooling film disturbances

SNECMA44 citations87
US4696157ASep 29, 1987

Fuel and air injection system for a turbojet engine

SNECMA22 citations78
US5335491AAug 9, 1994

Combustion chamber with axially displaced fuel injectors

SNECMA17 citations73
US5528896AJun 25, 1996

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

SNECMA11 citations67

NAT D ETDUE ET DE CONSTRUCTION

1 patent

CONST DE MOTORS D AVIAT SOC NA

1 patent