Inventor · disambiguated record
Christophe Pieussergues
Also filed as: PIEUSSERGUES CHRISTOPHE
28 granted patents·1 pending application·324 citations·filing 1993–2022
96Inventor score
Files withSNECMA9PIEUSSERGUES CHRISTOPHE7SAFRAN AIRCRAFT ENGINES6SNECMA MOTEURS2BUNEL JACQUES MARCEL ARTHUR1
Top patents by PatentIndex Score
29 records- 0195US5524430AGas-turbine engine with detachable combustion chamberSNECMA·Filed 1993·Granted Jun 11, 1996·100 cites·17 claims
- 0288US8661828B2Sealing between a combustion chamber and a turbine nozzle in a turbomachinePIEUSSERGUES CHRISTOPHE·Filed 2009·Granted Mar 4, 2014·29 cites·18 claims
- 0388US6988369B2Combustion chamber sealing ring, and a combustion chamber including such a ringSNECMA MOTEURS·Filed 2003·Granted Jan 24, 2006·43 cites·20 claims
- 0485US11441779B2Configuring and positioning air passage holes in a combustion chamber wallSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Sep 13, 2022·2 cites·9 claims
- 0583US8763406B2Turbomachine combustion chamberPIEUSSERGUES CHRISTOPHE·Filed 2009·Granted Jul 1, 2014·16 cites·12 claims
- 0682US9091445B2Guiding a sparkplug in a turbine engine combustion chamberBUNEL JACQUES MARCEL ARTHUR·Filed 2010·Granted Jul 28, 2015·4 cites·12 claims
- 0776US8099963B2Device for mounting an igniter plug in a combustion chamber of a gas turbine enginePIEUSSERGUES CHRISTOPHE·Filed 2009·Granted Jan 24, 2012·14 cites·10 claims
- 0873US7707834B2Diffuser for an annular combustion chamber, in particular for an airplane turbine engineSNECMA·Filed 2005·Granted May 4, 2010·8 cites·17 claims
- 0973US7673460B2System of attaching an injection system to a turbojet combustion chamber baseSNECMA·Filed 2006·Granted Mar 9, 2010·14 cites·13 claims
- 1073US7197882B2Turbojet diffuserSNECMA MOTEURS·Filed 2005·Granted Apr 3, 2007·15 cites·20 claims
- 1167US7954327B2Chamber endwall, method of producing it, combustion chamber comprising it, and turbine engine equipped therewithSNECMA·Filed 2007·Granted Jun 7, 2011·9 cites·18 claims
- 1265US10883718B2Air intake swirler for a turbomachine injection system comprising an aerodynamic deflector at its inletSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jan 5, 2021·1 cites·12 claims
- 1365US9651260B2Annular combustion chamber for a turbine engineSNECMA·Filed 2012·Granted May 16, 2017·2 cites·10 claims
- 1464US8806872B2Procedure for igniting a turbine engine combustion chamberPIEUSSERGUES CHRISTOPHE·Filed 2011·Granted Aug 19, 2014·1 cites·14 claims
- 1564US8276388B2Optimizing an anti-coke film in an injector system for a gas turbine engineCAYRE ALAIN·Filed 2008·Granted Oct 2, 2012·9 cites·13 claims
- 1662US8312723B2System for injecting a mixture of air and fuel into a turbomachine combustion chamberPIEUSSERGUES CHRISTOPHE·Filed 2008·Granted Nov 20, 2012·7 cites·9 claims
- 1761US8453459B2Fuel injection system for a combustion chamber of a turbomachineCAMERIANO LAURENT BERNARD·Filed 2011·Granted Jun 4, 2013·3 cites·13 claims
- 1859US8875484B2Guide for an ignition plug in a turbomachine combustion chamberLAINS DOMINIQUE MAURICE JACQUES·Filed 2010·Granted Nov 4, 2014·2 cites·6 claims
- 1958US5417069ASeparator for an annular gas turbine combustion chamberSNECMA·Filed 1994·Granted May 23, 1995·24 cites·11 claims
- 2057US8215118B2Optimizing the angular positioning of a turbine nozzle at the outlet from a turbomachine combustion chamberPIEUSSERGUES CHRISTOPHE·Filed 2009·Granted Jul 10, 2012·3 cites·4 claims
- 2156US8069669B2Separator for feeding cooling air to a turbinePIEUSSERGUES CHRISTOPHE·Filed 2008·Granted Dec 6, 2011·5 cites·12 claims
- 2253US10233836B2Turbomachine combustion chamber provided with air deflection means for reducing the wake created by an ignition plugSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Mar 19, 2019·1 cites·12 claims
- 2351US8047002B2Annular combustion chamber of a gas turbine engineSNECMA·Filed 2008·Granted Nov 1, 2011·2 cites·9 claims
- 2451US7637111B2Easily demountable combustion chamber with improved aerodynamic performanceSNECMA·Filed 2006·Granted Dec 29, 2009·4 cites·14 claims
- 2546US12366358B2Flame-holder device for a turbojet afterburner, comprising three-branched armsSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Jul 22, 2025·0 cites·11 claims
- 2645US11846420B2Combustion chamber comprising means for cooling an annular casing zone downstream of a chimneySAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Dec 19, 2023·0 cites·13 claims
- 2742US11725822B2Combustion module for a gas turbo engine with chamber bottom stopSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Aug 15, 2023·0 cites·17 claims
- 2841US8505311B2Turbomachine with separate fuel injection systems, using identical sealing jointsDESCHAMPS FRANCOISE·Filed 2009·Granted Aug 13, 2013·6 cites·15 claims
- 2940US2011113748A1Guiding an ignition spark plug in a turbomachine combustion chamberSNECMA·Filed 2010·Application pending·0 cites
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