Inventor · disambiguated record
Philippe Gerard Chanez
Also filed as: CHANEZ PHILIPPE · CHANEZ PHILIPPE GERARD · CHANEZ PHILIPPE GÉRARD
18 granted patents·75 citations·filing 2007–2021
91Inventor score
Files withSAFRAN AIRCRAFT ENGINES11SNECMA3CHANEZ PHILIPPE GERARD2CHANEZ PHILIPPE GÉRARD1INST SUPERIEUR DE L AERONAUTIQUE ET DE L ESPACE1
Top patents by PatentIndex Score
18 records- 0185US9091207B2Gas turbine engine air intake in a nacelleCHANEZ PHILIPPE GERARD·Filed 2010·Granted Jul 28, 2015·14 cites·13 claims
- 0281US9494077B2Gas turbine engine comprising three rotary bodiesCHANEZ PHILIPPE GÉRARD·Filed 2012·Granted Nov 15, 2016·18 cites·9 claims
- 0380US10814989B2Propulsion assembly for an aircraft, comprising a gas generator, two offset fans and an air inlet sleeveSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 27, 2020·3 cites·15 claims
- 0478US11199108B2Outlet of a hot-gas pipe of an aircraft engine passing through an engine wallSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 14, 2021·2 cites·7 claims
- 0577US11913378B2Assembly for a turbomachineINST SUPERIEUR DE L AERONAUTIQUE ET DE L ESPACE·Filed 2020·Granted Feb 27, 2024·3 cites·13 claims
- 0674US10518890B2Propulsion assembly for an aircraft, comprising a gas generator and two offset fansSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 31, 2019·2 cites·12 claims
- 0773US8684302B2Airplane having engines partially encased in the fuselageCHANEZ PHILIPPE GERARD·Filed 2009·Granted Apr 1, 2014·13 cites·11 claims
- 0871US7600384B2Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowlSNECMA·Filed 2007·Granted Oct 13, 2009·11 cites·4 claims
- 0959US7845156B2Turbofan exhaust systemSNECMA·Filed 2007·Granted Dec 7, 2010·6 cites·9 claims
- 1049US7735776B2Air inlet for a turbofan engineSNECMA·Filed 2007·Granted Jun 15, 2010·3 cites·6 claims
- 1147US10408165B2Device with gratings for ejecting microjets in order to reduce the jet noise of a turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Sep 10, 2019·0 cites·21 claims
- 1243US12344376B2Nacelle air intake for an aircraft propulsion assembly to promote a thrust reversal phaseSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jul 1, 2025·0 cites·16 claims
- 1343US11772779B2Propulsion unit with improved boundary layer ingestionSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Oct 3, 2023·0 cites·11 claims
- 1442US12480452B2Aircraft dual-flow turbine engine assembly, the assembly being equipped with incidence-controlled air discharge finsSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Nov 25, 2025·0 cites·9 claims
- 1542US11913404B2Nacelle air outlet for aircraft turbojet engine comprising a straightening device for facilitating a reverse thrust phaseSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Feb 27, 2024·0 cites·19 claims
- 1641US10539155B2Propulsive assembly for aircraft comprising a turbojet fitted with a fan with removable bladesSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 21, 2020·0 cites·6 claims
- 1739US11059597B2Aircraft with multiple fan propulsion assembly fixed under the wingSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jul 13, 2021·0 cites·11 claims
- 1839US10859037B2Low fan noise turbojetSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Dec 8, 2020·0 cites·12 claims
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