Inventor · disambiguated record
Michel A. A. Desaulty
Also filed as: DESAULTY MICHEL · DESAULTY MICHEL A A · DESAULTY MICHEL ANDRE · DESAULTY MICHEL ANDRE ALBERT
35 granted patents·1,414 citations·filing 1985–2008
98Inventor score
Top patents by PatentIndex Score
35 records- 0197US7942003B2Dual-injector fuel injector systemSNECMA·Filed 2008·Granted May 17, 2011·105 cites·13 claims
- 0295US4901522ATurbojet engine combustion chamber with a double wall converging zoneSNECMA·Filed 1988·Granted Feb 20, 1990·117 cites·8 claims
- 0389US5797266ADevice for actively controlling combustion instabilities and for decoking a fuel injectorSNECMA·Filed 1995·Granted Aug 25, 1998·74 cites·12 claims
- 0489US5592819APre-mixing injection system for a turbojet engineSNECMA·Filed 1995·Granted Jan 14, 1997·80 cites·11 claims
- 0588US5775108ACombustion chamber having a multi-hole cooling system with variably oriented holesSNECMA·Filed 1996·Granted Jul 7, 1998·64 cites·7 claims
- 0688US5235805AGas turbine engine combustion chamber with oxidizer intake flow controlSNECMA·Filed 1992·Granted Aug 17, 1993·62 cites·15 claims
- 0787US4754600AAxial-centripetal swirler injection apparatusSNECMA·Filed 1987·Granted Jul 5, 1988·57 cites·15 claims
- 0885US4805397ACombustion chamber structure for a turbojet engineSNECMA·Filed 1987·Granted Feb 21, 1989·57 cites·10 claims
- 0984US6035645AAerodynamic fuel injection system for a gas turbine engineSNECMA·Filed 1997·Granted Mar 14, 2000·97 cites·9 claims
- 1084US5590531APerforated wall for a gas turbine engineNAT D ETDUE ET DE CONSTRUCTION·Filed 1994·Granted Jan 7, 1997·49 cites·8 claims
- 1183US5592820AGas turbine diffuserNAT D ETDUE ET DE CONSTRUCTION·Filed 1994·Granted Jan 14, 1997·71 cites·13 claims
- 1280US5937653AReduced pollution combustion chamber having an annular fuel injectorSNECMA·Filed 1997·Granted Aug 17, 1999·50 cites·7 claims
- 1379US4726182AVariable flow air-fuel mixing device for a turbojet engineSNECMA·Filed 1985·Granted Feb 23, 1988·44 cites·8 claims
- 1477US6112516AOptimally cooled, carbureted flameholderSNECMA·Filed 1998·Granted Sep 5, 2000·42 cites·4 claims
- 1577US4766722AEnlarged bowl member for a turbojet engine combustion chamberSNECMA·Filed 1986·Granted Aug 30, 1988·34 cites·10 claims
- 1674US5341645AFuel/oxidizer premixing combustion chamberSNECMA·Filed 1993·Granted Aug 30, 1994·33 cites·11 claims
- 1773US6070412ATurbomachine combustion chamber with inner and outer injector rowsSNECMA·Filed 1998·Granted Jun 6, 2000·54 cites·7 claims
- 1870US7721545B2Device for injecting a mixture of air and fuel, combustion chamber and turbomachine both equipped with such a deviceSNECMA·Filed 2007·Granted May 25, 2010·8 cites·11 claims
- 1970US5209067AGas turbine combustion chamber wall structure for minimizing cooling film disturbancesSNECMA·Filed 1991·Granted May 11, 1993·44 cites·12 claims
- 2068US5568721ASystem for supplying fuel to and cooling a fuel injector of a dual head combustion chamberSNECMA·Filed 1995·Granted Oct 29, 1996·27 cites·9 claims
- 2167US5211675AVariable volume combustion chamber for a gas turbine engineSNECMA·Filed 1992·Granted May 18, 1993·27 cites·9 claims
- 2266US7823387B2Gas turbine engine diffuser and combustion chamber and gas turbine engine comprising sameSNECMA·Filed 2008·Granted Nov 2, 2010·8 cites·17 claims
- 2364US7805943B2Shroud for a turbomachine combustion chamberSNECMA·Filed 2006·Granted Oct 5, 2010·9 cites·11 claims
- 2463US8047777B2Turbomachine diffuserSNECMA·Filed 2008·Granted Nov 1, 2011·8 cites·2 claims
- 2563US4696157AFuel and air injection system for a turbojet engineSNECMA·Filed 1986·Granted Sep 29, 1987·22 cites·9 claims
- 2661US5295354ALow pollution combustion chamber for a turbojet engineSNECMA·Filed 1992·Granted Mar 22, 1994·22 cites·13 claims
- 2759US7908865B2Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine provided with such a deviceSNECMA·Filed 2007·Granted Mar 22, 2011·6 cites·13 claims
- 2859US5339622AGas turbine engine with improved water ingestion preventionSNECMA·Filed 1993·Granted Aug 23, 1994·30 cites·6 claims
- 2958US5417069ASeparator for an annular gas turbine combustion chamberSNECMA·Filed 1994·Granted May 23, 1995·24 cites·11 claims
- 3056US5209066ACounter flow combustion chamber for a gas turbine engineSNECMA·Filed 1991·Granted May 11, 1993·24 cites·5 claims
- 3155US5335491ACombustion chamber with axially displaced fuel injectorsSNECMA·Filed 1993·Granted Aug 9, 1994·17 cites·8 claims
- 3254US7155913B2Turbomachine annular combustion chamberSNECMA MOTEURS·Filed 2004·Granted Jan 2, 2007·17 cites·20 claims
- 3352US5261239ALean premixture combustion-chamber comprising a counterflow enclosure to stabilize the premixture flameCONST DE MOTORS D AVIAT SOC NA·Filed 1992·Granted Nov 16, 1993·16 cites·11 claims
- 3441US5528896AGas-flow separator for a double dome gas turbine engine combustion chamberSNECMA·Filed 1994·Granted Jun 25, 1996·11 cites·8 claims
- 3528US5699663AMethod of preventing instabilities produced by combustion in a turbojet engineSNECMA·Filed 1996·Granted Dec 23, 1997·4 cites·7 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →