JN

Jacky Naudet

SM Snecma Moteurs: 6 patents #12 of 501Top 3%
SN Snecma: 2 patents #478 of 1,717Top 30%
GE: 1 patents #19,878 of 36,430Top 55%
📍 Bondoufle, FR: #1 of 33 inventorsTop 4%
Overall (All Time): #83,487 of 4,157,543Top 3%
39
Patents All Time

Issued Patents All Time

Showing 1–25 of 39 patents

Patent #TitleCo-InventorsDate
7500644 Device for maintaining and positioning harnesses on a turbo-jet engine Aude Rivory, Gael Gaignon 2009-03-10
7438492 Link between two mechanical members Gerard Etoile, Frederic Babec 2008-10-21
7018173 Device for stopping in rotation a fixed blade bearing sector in a gas turbine casing Serge Bongrand, Alain Bouron, Sebastien Goux, Fabrice Marois, Gabriel Radeljak +1 more 2006-03-28
6688846 Device for controlling variable-pitch blades Jean-Pierre Caubet, Antoine Jean, Gabrijel Radeljak, Sébastien Riccioz 2004-02-10
6629463 Acoustic inspection of one-piece bladed wheels Jean-Luc Mary, Andre Collot, Marc Berthillier 2003-10-07
6464463 Blade locking device with hammer fastener on a disk Jean-Luc Christian Yvon Goga 2002-10-15
6390771 High-pressure compressor stator Pascal Gérard Gervais, Pascal Lejeune, Carmen Miraucourt, Patrice Suet, Monique Thore 2002-05-21
6349539 Axisymmetric, converging-diverging, jet-deflecting turbojet-engine exhaust-nozzle Didier Feder, Daniel Kettler, Guy Lapergue, Bertrand Pierre Renaud Monville, Laurent Claude Patrick Salperwyck 2002-02-26
6332617 Leaktight seal of a circular vane stage Jacques Leveaux 2001-12-25
6011617 System for inspecting internal zones of a machine by optical fibre endoscopy 2000-01-04
5919032 Bladed disk with three-root blades Christophe Poy 1999-07-06
5702217 Braking nuts or screws and mountings obtained with same devices Jean-Louis Charbonnel, Michel Franchet 1997-12-30
5579644 Turbo-jet equipped with inclined balancing disks within the rotor of the high pressure compressor and process for producing such disks 1996-12-03
5473883 Compressor turbojet engine whose rotor has a movable upstream stage 1995-12-12
5466122 Turbine engine stator with pivoting blades and control ring Jean-Louis Charbonnel, Philippe Guerout, Jacques L. Happey, Frederic G. J. Mainfroy, Jean-Claude Porcher 1995-11-14
5407322 Variable phase vane Jean-Louis Charbonnel, Jean-Luc Christian Yvon Goga, Gerard G. Miraucourt, Denis B. Pottier 1995-04-18
5330324 Annular gasket disposed at one axial extremity of a rotor and covering blade feet Daniel Andre Agram, Jean-Louis Charbonnel, Philippe Gerard, Edmond Joly, Gerard G. Miraucourt, Jean-Claude Prato 1994-07-19
5328328 Sealing device between blade stages and a rotary drum, particularly for preventing leaks around the stages of straightener blades Jean-Louis Charbonnel, Jean-Christophe Marc Cordier, Corrine G. Delahaye, Jean-Claude L. Delonge, Guy Frank Paul Dusserre-Telmon +5 more 1994-07-12
5328327 Stator for directing the inlet of air inside a turbo-engine and method for mounting a vane of said stator 1994-07-12
5324165 Sealing structure for a pivoting blade of a gas turbine Jean-Louis Charbonnel 1994-06-28
5319850 Method of fixing stemmed blade for a flow-straightening stage of a gas turbine engine Jean-Louis Charbonnel, Gerard G. Miraucourt 1994-06-14
5320484 Turbomachine stator having a double skin casing including means for preventing gas flow longitudinally therethrough Jean-Louis Charbonnel, Pierre Debeneix, Christopher Charles Glynn, Daniel J. Marey, Jean-Pierre Mourlan +3 more 1994-06-14
5314303 Device for checking the clearances of a gas turbine compressor casing Jean-Louis Charbonnel, Gerard Jacques Stangalini 1994-05-24
5288206 Turbo aero engine equipped with means facilitating adjustment of plays of the stator and between the stator and rotor Alain Marc Lucien Bromann, Jean-Louis Charbonnel, Pierre Debeneix, Daniel J. Marey, Thierry Niclot +1 more 1994-02-22
5277544 Blade control rod and system of such rods 1994-01-11