Jacques Roche — 14 Patents at Snecma

Jacques Roche has been granted 14 US patents while listed as an inventor at Snecma. The first was granted in 1994 and the most recent in March 2011. Jacques Roche ranks #332,869 of 4,157,543 US inventors in our database (top 8.0%). Patent records list Jacques Roche in Lisses, FR.

Issued Patents All Time

Showing 1–14 of 14 patents

Patent #	Title	Co-Inventors	Date
7908868	Device for mounting an air-flow dividing wall in a turbojet engine afterburner	Jacques Marcel Arthur Bunel, Alain Pierre Page, Yann Vuillemenot	2011-03-22
7614236	Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop	Emmanuel Mandet, Laurent Claude Patrick Salperwyck	2009-11-10
7600383	Turbojet with protection means for a fuel injection device, an injection device and a protective plate for the turbojet	Jacques Marcel Arthur Bunel, Alain Pierre Page	2009-10-13
7584615	Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performance	Sebastien Baboeuf, Sabine Charpenel, Eric Maingre, Alain Pierre Page	2009-09-08
7574866	Turbo-jet engine with a protective screen of the fuel manifold of a burner ring, the burner ring and the protective screen	Alain Pierre Page, Stephane Henri Guy Touchaud, Nicolas Pommier	2009-08-18
7506513	Device for feeding air and fuel to a burner ring in an after-burner chamber	Jacques Marcel Arthur Bunel	2009-03-24
7370477	Device for fastening a fluid duct to a turbojet casing	Jacques Marcel Arthur Bunel, Frederic Ruellan, Philippe Henry	2008-05-13
7367191	Device for fixing a burner ring in an afterburner combustion chamber of a turbojet engine	Jacques Marcel Arthur Bunel	2008-05-06
7287383	Afterburner arrangement	Jacques Marcel Arthur Bunel, Bien-Aime Rakotondrainibe, Stephane Henri Guy Touchaud	2007-10-30
6976361	Ventilation channels in an afterburner chamber confluence sheet	Thierry Cortes, Alain Pierre Page, Sebastien Baboeuf	2005-12-20
6966189	System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber	Guy Lapergue, Guillaume Sevi	2005-11-22
6792748	Cooling system for a gas turbine engine post-combustion jet nozzle	Léopold Jean-Marie de Verduzan, Maurice Floreani	2004-09-21
5400589	Afterburner for a turbofan engine	Olivier M. M. Mahias, Xavier J. Pasquali, Mireille S. N. Romero, Elisabeth Vilfeu	1995-03-28
5297391	Fuel injector for a turbojet engine afterburner	—	1994-03-29

Jacques Roche — 14 Patents

Issued Patents All Time

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