Inventor · disambiguated record
Alain Cayre
Also filed as: CAYRE ALAIN · CAYRE ALAIN RENE
9 granted patents·1 pending application·54 citations·filing 2005–2016
85Inventor score
Top patents by PatentIndex Score
10 records- 0173US8291709B2Combustion chamber of a turbomachine including cooling groovesCAYRE ALAIN·Filed 2008·Granted Oct 23, 2012·14 cites·14 claims
- 0273US7707834B2Diffuser for an annular combustion chamber, in particular for an airplane turbine engineSNECMA·Filed 2005·Granted May 4, 2010·8 cites·17 claims
- 0370US7721545B2Device for injecting a mixture of air and fuel, combustion chamber and turbomachine both equipped with such a deviceSNECMA·Filed 2007·Granted May 25, 2010·8 cites·11 claims
- 0464US8276388B2Optimizing an anti-coke film in an injector system for a gas turbine engineCAYRE ALAIN·Filed 2008·Granted Oct 2, 2012·9 cites·13 claims
- 0564US7805943B2Shroud for a turbomachine combustion chamberSNECMA·Filed 2006·Granted Oct 5, 2010·9 cites·11 claims
- 0659US7908865B2Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine provided with such a deviceSNECMA·Filed 2007·Granted Mar 22, 2011·6 cites·13 claims
- 0741US8091368B2Turbomachine combustion chamberCAYRE ALAIN·Filed 2008·Granted Jan 10, 2012·0 cites·8 claims
- 0840US10677463B2Air intake ring for a turbomachine combustion chamber injection system and method of atomizing fuel in an injection system comprising said air intake ringSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jun 9, 2020·0 cites·7 claims
- 0937US11125435B2Bent combustion chamber from a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Sep 21, 2021·0 cites·8 claims
- 1030US2016153662A1Annular deflection wall for a turbomachine combustion chamber injection system providing a wide fuel atomization zoneSNECMA·Filed 2015·Application pending·0 cites
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