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 patentsUS5235805AAug 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