P

Inventor

HERNANDEZ DIDIER HIPPOLYTE

FR41 patents
⚠️ This page may combine multiple inventors who share the name “HERNANDEZ DIDIER HIPPOLYTE”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

SNECMA

22 patents
US7827798B2Nov 9, 2010

System for ventilating a combustion chamber wall in a turbomachine

SNECMA21 citations92
US7775051B2Aug 17, 2010

Arrangement for a jet engine combustion chamber

SNECMA21 citations92
US7770398B2Aug 10, 2010

Annular combustion chamber of a turbomachine

SNECMA23 citations92
US7849696B2Dec 14, 2010

Assembling an annular combustion chamber of a turbomachine

SNECMA34 citations91
US7478534B2Jan 20, 2009

Arrangement with a twist-lock coupling for a turbomachine combustion chamber

SNECMA44 citations88
US8683806B2Apr 1, 2014

Chamber-bottom baffle, combustion chamber comprising same and gas turbine engine fitted therewith

SNECMA17 citations84
US8033114B2Oct 11, 2011

Multimode fuel injector for combustion chambers, in particular of a jet engine

SNECMA10 citations84
US7891193B2Feb 22, 2011

Cooling of a multimode fuel injector for combustion chambers, in particular of a jet engine

SNECMA14 citations84
US7788928B2Sep 7, 2010

Annular combustion chamber of a turbomachine

SNECMA12 citations84
US7661273B2Feb 16, 2010

Turbomachine with annular combustion chamber

SNECMA11 citations84
US8037691B2Oct 18, 2011

Deflector for a combustion chamber endwall, combustion chamber equipped therewith and turbine engine comprising them

SNECMA8 citations83
US7942005B2May 17, 2011

Combustion chamber in a turbomachine

SNECMA13 citations83
US7926281B2Apr 19, 2011

Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine provided with such a device

SNECMA20 citations81
US7673460B2Mar 9, 2010

System of attaching an injection system to a turbojet combustion chamber base

SNECMA14 citations81
US7549294B2Jun 23, 2009

Turbomachine with angular air delivery

SNECMA11 citations78
US5996333ADec 7, 1999

Oxidizer control device for a gas turbine engine

SNECMA15 citations74
US7971439B2Jul 5, 2011

Annular turbomachine combustion chamber

SNECMA2 citations62
US7937944B2May 10, 2011

System for ventilating a combustion chamber wall

SNECMA3 citations62
US7854126B2Dec 21, 2010

Annular combustion chamber with a removable end wall

SNECMA2 citations62
US7617688B2Nov 17, 2009

Combustion chamber of a gas turbine engine with an upstream fairing for separating the gas stream, annular wall forming a cap of the upstream fairing of the chamber, and gas turbine engine with the chamber

SNECMA5 citations60
US8028530B2Oct 4, 2011

Device for attaching a combustion chamber

SNECMA4 citations59
US8015707B2Sep 13, 2011

Method of fabricating a combustion chamber

SNECMA0 citations48

HERNANDEZ DIDIER HIPPOLYTE

10 patents

COMMARET PATRICE ANDRE

3 patents

DUVAL SYLVAIN

2 patents

SANDELIS DENIS JEAN MAURICE

2 patents

BOURGOIS SEBASTIEN ALAIN CHRISTOPHE

1 patent

BOURGOIS SÉBASTIEN ALAIN CHRISTOPHE

1 patent