Inventor · disambiguated record
Alain M. J. Lardellier
Also filed as: LARDELLIER ALAIN · LARDELLIER ALAIN M J · LARDELLIER ALAIN MARIE JOSEPH
32 granted patents·1,096 citations·filing 1975–2007
98Inventor score
Top patents by PatentIndex Score
32 records- 0193US4646810AMethod for the manufacture of a ceramic turbine ring integral with a metallic annular carrierSNECMA·Filed 1985·Granted Mar 3, 1987·31 cites·9 claims
- 0289US5407326AHollow blade for a turbomachineSNECMA·Filed 1994·Granted Apr 18, 1995·50 cites·22 claims
- 0389US4623298ATurbine shroud sealing deviceSNECMA·Filed 1984·Granted Nov 18, 1986·74 cites·3 claims
- 0488US3964257ADevice for boosting and bleeding a gas turbine engineSNECMA·Filed 1975·Granted Jun 22, 1976·46 cites·14 claims
- 0587US4500143AMeans for controlling clearance in an intershaft bearing journal of a multi-spool gas turbineSNECMA·Filed 1982·Granted Feb 19, 1985·39 cites·9 claims
- 0684US7168913B2Twin-spool turbojet with means for driving ancillary machinesSNECMA MOTEURS·Filed 2004·Granted Jan 30, 2007·49 cites·15 claims
- 0784US4451110ATurbine bearingSNECMA·Filed 1982·Granted May 29, 1984·56 cites·3 claims
- 0883US4295785ARemovable sealing gasket for distributor segments of a jet engineSNECMA·Filed 1980·Granted Oct 20, 1981·53 cites·8 claims
- 0982US5058379AHigh by-pass ratio turbojet engine with counterrotating upstream and downstream fansSNECMA·Filed 1990·Granted Oct 22, 1991·43 cites·9 claims
- 1081US6148605AMethod and device for reversing the thrust of very high bypass ratio turbojet enginesSNECMA·Filed 1999·Granted Nov 21, 2000·71 cites·8 claims
- 1181US4648795AContainment structure for a turbojet engineSNECMA·Filed 1985·Granted Mar 10, 1987·62 cites·5 claims
- 1281US4295787ARemovable support for the sealing lining of the casing of jet engine blowersSNECMA·Filed 1980·Granted Oct 20, 1981·36 cites·7 claims
- 1380US4762462AHousing for an axial compressorSNECMA·Filed 1987·Granted Aug 9, 1988·56 cites·6 claims
- 1479US7237378B2Turbomachine with low noise emissions for aircraftSNECMA MOTEURS·Filed 2004·Granted Jul 3, 2007·28 cites·9 claims
- 1579US5343619AHollow blade for a turbomachine and method of manufacturing said bladeSNECMA·Filed 1993·Granted Sep 6, 1994·33 cites·2 claims
- 1676US7656054B2Turbine engine with an alternator and method for transmitting movement to an alternatorSNECMA·Filed 2007·Granted Feb 2, 2010·14 cites·7 claims
- 1775US4714404AApparatus for controlling radial clearance between a rotor and a stator of a tubrojet engine compressorSNECMA·Filed 1986·Granted Dec 22, 1987·46 cites·12 claims
- 1874US7581920B2Method for air circulation in a turbomachine compressor, compressor arrangement using this method, compression stage and compressor incorporating such a arrangement, and aircraft engine equipped with such a compressorSNECMA·Filed 2005·Granted Sep 1, 2009·14 cites·38 claims
- 1972US4548546AAdjustment system of centering a turbomachine wheel and mounted turbomachine by way of permitting the application of said systemSNECMA·Filed 1982·Granted Oct 22, 1985·37 cites·2 claims
- 2068US5105618ACounterrotating fan engineSNECMA·Filed 1990·Granted Apr 21, 1992·37 cites·9 claims
- 2163US5311736AVariable cycle propulsion engine for supersonic aircraftSNECMA·Filed 1992·Granted May 17, 1994·25 cites·7 claims
- 2262US5119626ACombined turborocket and ramjet propulsion unitSNECMA·Filed 1990·Granted Jun 9, 1992·30 cites·10 claims
- 2360US7469528B2Aircraft braking method and ducted fan jet engine for implementing the methodSNECMA·Filed 2005·Granted Dec 30, 2008·5 cites·15 claims
- 2459US5255510AThrust reverser for a high-bypass ratio turbofan engineSNECMA·Filed 1992·Granted Oct 26, 1993·23 cites·60 claims
- 2558US4940196AWing mounting nacelle for a very high by-pass ratio turbojet aero-engineSNECMA·Filed 1988·Granted Jul 10, 1990·23 cites·10 claims
- 2656US4279153AApparatus for measuring the temperature of a gas flow traversing a grid of bladesSNECMA·Filed 1979·Granted Jul 21, 1981·14 cites·14 claims
- 2756US4197052ASafety device for an axially rotating machineSNECMA·Filed 1978·Granted Apr 8, 1980·20 cites·9 claims
- 2854US6279852B1Drive system for a propeller driven transport aircraftSNECMA·Filed 1998·Granted Aug 28, 2001·30 cites·9 claims
- 2949US4696619AHousing for a turbojet engine compressorSNECMA·Filed 1986·Granted Sep 29, 1987·19 cites·10 claims
- 3045US5103635AContra-rotating fan engineSNECMA·Filed 1990·Granted Apr 14, 1992·18 cites·9 claims
- 3144US7134843B2Turbine wheel for turbomachine and the assembly method for such a wheelSNECMA MOTEURS·Filed 2004·Granted Nov 14, 2006·7 cites·23 claims
- 3228US4993638AThrust vectoring nozzle assemblyMATEURS D AVIAT S N E C M A SO·Filed 1990·Granted Feb 19, 1991·7 cites·10 claims
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