Inventor · disambiguated record
Jacky Naudet
Also filed as: NAUDET JACKY · NAUDET JACKY S · NAUDET JACKY SERGE
39 granted patents·2 pending applications·1,255 citations·filing 1984–2004
98Inventor score
Top patents by PatentIndex Score
41 records- 0194US4604030ACompressor with variable incidence stator vanesSNECMA·Filed 1984·Granted Aug 5, 1986·81 cites·8 claims
- 0291US5328327AStator for directing the inlet of air inside a turbo-engine and method for mounting a vane of said statorSNECMA·Filed 1992·Granted Jul 12, 1994·68 cites·12 claims
- 0389US7500644B2Device for maintaining and positioning harnesses on a turbo-jet engineSNECMA·Filed 2004·Granted Mar 10, 2009·98 cites·19 claims
- 0488US4706354AMethod of manufacturing a root pivot assembly of a variable incidence turbo-machine bladeSNECMA·Filed 1986·Granted Nov 17, 1987·53 cites·5 claims
- 0587US4844694AFastening spindle and method of assembly for attaching rotor elements of a gas-turbine engineSNECMA·Filed 1987·Granted Jul 4, 1989·72 cites·2 claims
- 0684US6629463B2Acoustic inspection of one-piece bladed wheelsSNECMA MOTEURS·Filed 2001·Granted Oct 7, 2003·32 cites·7 claims
- 0783US4730983ASystem for attaching a rotor blade to a rotor diskSNECMA·Filed 1987·Granted Mar 15, 1988·64 cites·13 claims
- 0882US5161949ARotor fitted with spacer blocks between the bladesSNECMA·Filed 1991·Granted Nov 10, 1992·64 cites·4 claims
- 0981US6390771B1High-pressure compressor statorSNECMA MOTEURS·Filed 2000·Granted May 21, 2002·30 cites·8 claims
- 1079US5288206ATurbo aero engine equipped with means facilitating adjustment of plays of the stator and between the stator and rotorSNECMA·Filed 1992·Granted Feb 22, 1994·41 cites·11 claims
- 1177US4750746ADevice for attaching a seal member to a shaftSNECMA·Filed 1987·Granted Jun 14, 1988·36 cites·19 claims
- 1276US5039277AVariable stator vane with separate guide diskSNECMA·Filed 1990·Granted Aug 13, 1991·61 cites·11 claims
- 1370US5330324AAnnular gasket disposed at one axial extremity of a rotor and covering blade feetSNECMA·Filed 1993·Granted Jul 19, 1994·41 cites·5 claims
- 1468US5277544ABlade control rod and system of such rodsSNECMA·Filed 1992·Granted Jan 11, 1994·29 cites·5 claims
- 1566US6688846B2Device for controlling variable-pitch bladesSNECMA MOTEURS·Filed 2001·Granted Feb 10, 2004·28 cites·10 claims
- 1666US6464463B2Blade locking device with hammer fastener on a diskSNECMA MOTEURS·Filed 2001·Granted Oct 15, 2002·29 cites·4 claims
- 1766US5324165ASealing structure for a pivoting blade of a gas turbineSNECMA·Filed 1993·Granted Jun 28, 1994·28 cites·5 claims
- 1865US4595339ACentripetal accelerator for air exhaustion in a cooling device of a gas turbine combined with the compressor discSNECMA·Filed 1984·Granted Jun 17, 1986·30 cites·3 claims
- 1964US5314303ADevice for checking the clearances of a gas turbine compressor casingSNECMA·Filed 1993·Granted May 24, 1994·38 cites·9 claims
- 2063US7438492B2Link between two mechanical membersSNECMA·Filed 2004·Granted Oct 21, 2008·13 cites·18 claims
- 2163US5328328ASealing device between blade stages and a rotary drum, particularly for preventing leaks around the stages of straightener bladesSNECMA·Filed 1993·Granted Jul 12, 1994·33 cites·9 claims
- 2261US6011617ASystem for inspecting internal zones of a machine by optical fibre endoscopySNECMA·Filed 1998·Granted Jan 4, 2000·23 cites·14 claims
- 2359US5473883ACompressor turbojet engine whose rotor has a movable upstream stageSNECMA·Filed 1994·Granted Dec 12, 1995·32 cites·8 claims
- 2453US6332617B1Leaktight seal of a circular vane stageSNECMA·Filed 1999·Granted Dec 25, 2001·33 cites·9 claims
- 2551US5407322AVariable phase vaneSNECMA·Filed 1993·Granted Apr 18, 1995·19 cites·5 claims
- 2649US5702217ABraking nuts or screws and mountings obtained with same devicesSNECMA·Filed 1995·Granted Dec 30, 1997·17 cites·1 claims
- 2749US5236304AStemmed blade for a flow-straightening stage of a gas turbine engine and method of fixing said bladeSNECMA·Filed 1991·Granted Aug 17, 1993·10 cites·5 claims
- 2848US5224820AOperating mechanism for variably settable blades of a turbomachineSNECMA·Filed 1992·Granted Jul 6, 1993·20 cites·9 claims
- 2947US5466122ATurbine engine stator with pivoting blades and control ringSNECMA·Filed 1994·Granted Nov 14, 1995·27 cites·6 claims
- 3041US5096377ATurboshaft engine casing joint with reinforced axial restraintSNECMA·Filed 1990·Granted Mar 17, 1992·13 cites·6 claims
- 3141US4787820ATurbine plant compressor disc with centripetal accelerator for the induction of turbine cooling airSNECMA·Filed 1988·Granted Nov 29, 1988·13 cites·5 claims
- 3241US4732536ATurbo-machine compressor with variable incidence stator vanesSNECMA·Filed 1986·Granted Mar 22, 1988·14 cites·12 claims
- 3338US7018173B2Device for stopping in rotation a fixed blade bearing sector in a gas turbine casingSNECMA MOTEURS·Filed 2002·Granted Mar 28, 2006·7 cites·13 claims
- 3437US5320484ATurbomachine stator having a double skin casing including means for preventing gas flow longitudinally therethroughGEN ELECTRIC·Filed 1993·Granted Jun 14, 1994·16 cites·3 claims
- 3536US6349539B1Axisymmetric, converging-diverging, jet-deflecting turbojet-engine exhaust-nozzleSNECMA MOTEURS·Filed 2000·Granted Feb 26, 2002·3 cites·3 claims
- 3636US5319850AMethod of fixing stemmed blade for a flow-straightening stage of a gas turbine engineSNECMA·Filed 1993·Granted Jun 14, 1994·9 cites·1 claims
- 3736US5000659ATemporary locking system for variably settable stator bladesSNECMA·Filed 1990·Granted Mar 19, 1991·10 cites·9 claims
- 3836US2005129521A1Rotor blade for a turbo-machineSNECMA MOTEURS·Filed 2004·Application pending·0 cites
- 3934US5919032ABladed disk with three-root bladesSNECMA·Filed 1998·Granted Jul 6, 1999·15 cites·4 claims
- 4033US2004244195A1Method for making a blade ringFiled 2002·Application pending·0 cites
- 4132US5579644ATurbo-jet equipped with inclined balancing disks within the rotor of the high pressure compressor and process for producing such disksSNECMA·Filed 1994·Granted Dec 3, 1996·5 cites·3 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →