Inventor · disambiguated record
Alain Pierre Page
Also filed as: PAGE ALAIN · PAGE ALAIN PIERRE
10 granted patents·61 citations·filing 2004–2007
88Inventor score
Top patents by PatentIndex Score
10 records- 0179US7866162B2Exhaust cone for channeling a stream of gas downstream from a turbineSNECMA·Filed 2007·Granted Jan 11, 2011·14 cites·10 claims
- 0268US7784284B2Exhaust assembly forming a horizontal propulsion gas elbow in an aircraftSNECMA·Filed 2007·Granted Aug 31, 2010·9 cites·18 claims
- 0363US7581400B2Elbow-shaped propulsion gas exhaust assembly in an aircraftSNECMA·Filed 2007·Granted Sep 1, 2009·4 cites·20 claims
- 0462US7908868B2Device for mounting an air-flow dividing wall in a turbojet engine afterburnerSNECMA·Filed 2007·Granted Mar 22, 2011·9 cites·12 claims
- 0558US7574866B2Turbo-jet engine with a protective screen of the fuel manifold of a burner ring, the burner ring and the protective screenSNECMA·Filed 2005·Granted Aug 18, 2009·6 cites·4 claims
- 0655US7600383B2Turbojet with protection means for a fuel injection device, an injection device and a protective plate for the turbojetSNECMA·Filed 2005·Granted Oct 13, 2009·5 cites·21 claims
- 0755US7584615B2Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performanceSNECMA·Filed 2005·Granted Sep 8, 2009·6 cites·18 claims
- 0852US7870740B2Turbojet engine comprising an afterburner duct cooled by a variable-throughput ventilation streamSNECMA·Filed 2007·Granted Jan 18, 2011·4 cites·8 claims
- 0938US6976361B1Ventilation channels in an afterburner chamber confluence sheetSNECMA MOTEURS·Filed 2004·Granted Dec 20, 2005·4 cites·5 claims
- 1034US7631486B2Thrust orienting nozzleSNECMA·Filed 2006·Granted Dec 15, 2009·0 cites·14 claims
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