For the Inventor, By the Inventor

Enter assignee name

Societe Nationale D'etude Et De Construction De Moteurs D'aviation-snecma

USPTO Granted Patents = 33

EPO Patents = 1

Trademarks = 3

Forward Citations = 476

Loading Chart...

Loading Chart...

115 inventors (with patents filed for the assignee):

Jean-Pierre Maumus (3 out of 20 patents)

Dominique Coupe (2 out of 52 patents)

Daniel Cornu (2 out of 5 patents)

4. Jean-Michel De Monicault (2 out of 4 patents)

5. Jacques Thebault (2 out of 31 patents)

6. Pierre Camy (2 out of 8 patents)

7. Christian Coddet (2 out of 9 patents)

8. Christian Robin-Brosse (2 out of 8 patents)

9. Pierre Olry (2 out of 26 patents)

10. Christophe Verdy (2 out of 2 patents)

11. Stéphane Goujard (2 out of 2 patents)

12. René Pailler (2 out of 2 patents)

13. Eric Klinger (2 out of 2 patents)

14. Dominique Valentian (2 out of 15 patents)

15. Gilles Alain Marie Charier (1 out of 38 patents)

33 patents: Sort by Forward Citations

1. 6919118 - Method and machine for producing multiaxial fibrous webs (2005-07-19),

2. 6619668 - Static metal gasket and method of manufacturing it (2003-09-16),

3. 6543717 - Compact optimal and modulatable thrust device for controlling aerospace vehicles (2003-04-08),

4. 6516872 - High heat flux regenerative circuit, in particular for the combustion chamber of a rocket engine (2003-02-11),

5. 6482485 - Structural part including a portion made of thermostructural composite material cooled by fluid circulation (2002-11-19),

6. 6418710 - Deployable diverging part for a thruster (2002-07-16),

7. 6413585 - Thermochemical treatment, in halogenated atmosphere, of a carbon-containing material (2002-07-02),

8. 6410088 - CVI (chemical vapor infiltration) densification of porous structures (2002-06-25),

9. 6401941 - Rack for loading parts for heat treatment (2002-06-11),

10. 6378294 - System for activating an adjustable tube by means of an elastic ring for a thrust nozzle (2002-04-30),

11. 6375095 - Swiveling, converging-diverging, axisymmetric exhaust nozzle (2002-04-23),

12. 6319348 - Method for producing ring-shaped fibrous structures, in particular for making parts in composite material (2001-11-20),

13. 6318571 - Loader device for supporting parts for heat treatment in a furnace (2001-11-20),

14. 6314815 - Pressure sensor with compensation for null shift non-linearity at very low temperatures (2001-11-13),

15. 6291058 - Composite material with ceramic matrix and SiC fiber reinforcement, method for making same (2001-09-18),

Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) is a French aircraft engine manufacturer. It designs, develops, produces and supports a wide range of military and civil aircraft, including commercial airlines, combat jets, helicopters and satellites. Snecma is a subsidiary of Safran, a leading international high-technology group in aerospace and defense.

This text is generated by artificial intelligence and may not be accurate.

Company Badge

USPTO Data Jan 1 1976 - Dec 9 2025

33 Patents

#153 in Paris

#651 in France

#19,529 in the World

Societe Nationale D'etude Et De Construction De Moteurs D'aviation-snecma

Forward Citations = 476

115 inventors:

Jean-Pierre Maumus (3 out of 20 patents)

Dominique Coupe (2 out of 52 patents)

Daniel Cornu (2 out of 5 patents)

4. Jean-Michel De Monicault (2 out of 4 patents)

5. Jacques Thebault (2 out of 31 patents)

Please report any incorrect information to support@idiyas.com

Loading…