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 patentsUS7827798B2Nov 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 patentsUS8186163B2May 29, 2012
Multipoint injector for turbomachine
HERNANDEZ DIDIER HIPPOLYTE12 citations84
US8142148B2Mar 27, 2012
Diffuser-nozzle assembly for a turbomachine
HERNANDEZ DIDIER HIPPOLYTE12 citations84
US9303876B2Apr 5, 2016
Injection system for a turbomachine combustion chamber, including air injection means improving the air-fuel mixture
HERNANDEZ DIDIER HIPPOLYTE13 citations82
US9097425B2Aug 4, 2015
Fuel mixing device for turbine engine combustion chamber comprising improved air feed means
HERNANDEZ DIDIER HIPPOLYTE5 citations73
US9003805B2Apr 14, 2015
Turbine engine with diffuser
HERNANDEZ DIDIER HIPPOLYTE4 citations73
US8959772B2Feb 24, 2015
Multipoint injector for turbomachine
HERNANDEZ DIDIER HIPPOLYTE4 citations73
US9003802B2Apr 14, 2015
Multipoint injection device for a combustion chamber of a turbine engine
HERNANDEZ DIDIER HIPPOLYTE5 citations70
US8156744B2Apr 17, 2012
Annular combustion chamber for a gas turbine engine
HERNANDEZ DIDIER HIPPOLYTE4 citations62
US8096134B2Jan 17, 2012
Combustion chamber comprising chamber end wall heat shielding deflectors and gas turbine engine equipped therewith
HERNANDEZ DIDIER HIPPOLYTE3 citations62
US9046271B2Jun 2, 2015
Multipoint injector for a turbine engine combustion chamber
HERNANDEZ DIDIER HIPPOLYTE0 citations52
COMMARET PATRICE ANDRE
3 patentsUS8490401B2Jul 23, 2013
Annular combustion chamber for a gas turbine engine
COMMARET PATRICE ANDRE5 citations71
US8875517B2Nov 4, 2014
Diffuser for turbine engine including indented annular webs
COMMARET PATRICE ANDRE0 citations51
US8387395B2Mar 5, 2013
Annular combustion chamber for a turbomachine
COMMARET PATRICE ANDRE1 citations45