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 26–39 of 39 patents

Patent #TitleCo-InventorsDate
5236304 Stemmed blade for a flow-straightening stage of a gas turbine engine and method of fixing said blade Jean-Louis Charbonnel, Gerard G. Miraucourt 1993-08-17
5224820 Operating mechanism for variably settable blades of a turbomachine Christophe Brichet, Jean-Louis Charbonnel, Gerard G. Miraucourt, Jean-Francois Van De Voorde 1993-07-06
5161949 Rotor fitted with spacer blocks between the blades Michel Antoine Brioude, Philippe Chereau 1992-11-10
5096377 Turboshaft engine casing joint with reinforced axial restraint Philippe P. Catte 1992-03-17
5039277 Variable stator vane with separate guide disk 1991-08-13
5000659 Temporary locking system for variably settable stator blades Philippe P. Catte 1991-03-19
4844694 Fastening spindle and method of assembly for attaching rotor elements of a gas-turbine engine 1989-07-04
4787820 Turbine plant compressor disc with centripetal accelerator for the induction of turbine cooling air Jacques M. P. Stenneler 1988-11-29
4750746 Device for attaching a seal member to a shaft Jean-Claude Marcel Boudot 1988-06-14
4732536 Turbo-machine compressor with variable incidence stator vanes Claude Lejars, Jean-Max M. Silhouette, Jacques M. P. Stenneler 1988-03-22
4730983 System for attaching a rotor blade to a rotor disk Jean-Louis Bertrand 1988-03-15
4706354 Method of manufacturing a root pivot assembly of a variable incidence turbo-machine blade Jacques M. P. Stenneler 1987-11-17
4604030 Compressor with variable incidence stator vanes 1986-08-05
4595339 Centripetal accelerator for air exhaustion in a cooling device of a gas turbine combined with the compressor disc 1986-06-17