Inventor · disambiguated record
Philippe Jacques Pierre Fessou
Also filed as: FESSOU PHILIPPE · FESSOU PHILIPPE JACQUES · FESSOU PHILIPPE JACQUES PIERRE
9 granted patents·170 citations·filing 1996–2016
87Inventor score
Top patents by PatentIndex Score
9 records- 0188US10385708B2Guide assembly with optimised aerodynamic performanceSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 20, 2019·9 cites·5 claims
- 0284US7785066B2Bleed system for a low-pressure compressor of a turbomachineSNECMA·Filed 2007·Granted Aug 31, 2010·24 cites·5 claims
- 0380US5740674AArrangement of gas turbine engine comprising aerodynamic vanes and struts located in the same plane and an intermediate casingSNECMA·Filed 1996·Granted Apr 21, 1998·72 cites·21 claims
- 0476US7108486B2Backswept turbojet bladeSNECMA MOTEURS·Filed 2004·Granted Sep 19, 2006·28 cites·7 claims
- 0572US9945260B2Hub of an intermediate casing for an aircraft turbojet engine comprising doors with contoured geometrySNECMA·Filed 2014·Granted Apr 17, 2018·5 cites·10 claims
- 0668US7121792B1Nozzle vane with two slopesSNECMA MOTEURS·Filed 2004·Granted Oct 17, 2006·32 cites·20 claims
- 0734US10794218B2Discharge flow duct of a turbine engine comprising a VBV grating with variable settingSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 6, 2020·0 cites·14 claims
- 0833US11149565B2Turbine engine air guide assembly with improved aerodynamic performanceSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Oct 19, 2021·0 cites·7 claims
- 0933US10641289B2Airflow straightening assembly having improved aerodynamic performancesSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted May 5, 2020·0 cites·10 claims
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