Inventor · disambiguated record
Xavier M. H. Bardey
Also filed as: BARDEY XAVIER · BARDEY XAVIER M H
8 granted patents·1 pending application·202 citations·filing 1991–2021
89Inventor score
Top patents by PatentIndex Score
9 records- 0188US5235805AGas turbine engine combustion chamber with oxidizer intake flow controlSNECMA·Filed 1992·Granted Aug 17, 1993·62 cites·15 claims
- 0279US12054271B2Method for assembling an aircraft pylon and aircraft pylon obtained by this methodAIRBUS SAS·Filed 2021·Granted Aug 6, 2024·1 cites·12 claims
- 0367US5211675AVariable volume combustion chamber for a gas turbine engineSNECMA·Filed 1992·Granted May 18, 1993·27 cites·9 claims
- 0465US5242117AFuel injector for a gas turbine engineSNECMA·Filed 1992·Granted Sep 7, 1993·25 cites·9 claims
- 0559US5339622AGas turbine engine with improved water ingestion preventionSNECMA·Filed 1993·Granted Aug 23, 1994·30 cites·6 claims
- 0656US5209066ACounter flow combustion chamber for a gas turbine engineSNECMA·Filed 1991·Granted May 11, 1993·24 cites·5 claims
- 0755US5335491ACombustion chamber with axially displaced fuel injectorsSNECMA·Filed 1993·Granted Aug 9, 1994·17 cites·8 claims
- 0852US5261239ALean premixture combustion-chamber comprising a counterflow enclosure to stabilize the premixture flameCONST DE MOTORS D AVIAT SOC NA·Filed 1992·Granted Nov 16, 1993·16 cites·11 claims
- 0936US2019257269A1Turbojet engine comprising a nacelle equipped with a thrust-reversing system comprising outer and inner doorsAIRBUS OPERATIONS SAS·Filed 2019·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →