Inventor · disambiguated record
Romain Jean-Claude Ferrier
Also filed as: FERRIER ROMAIN · FERRIER ROMAIN JEAN CLAUDE
8 granted patents·1 pending application·9 citations·filing 2014–2019
77Inventor score
Top patents by PatentIndex Score
9 records- 0178US11199108B2Outlet 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
- 0269US10562638B2Cradle for a turbopropeller engine with integrated air inlet ductSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Feb 18, 2020·2 cites·10 claims
- 0364US10167814B2Turbine engine nozzle having confluent streams and including a core cowl with overlapping flapsSNECMA·Filed 2014·Granted Jan 1, 2019·3 cites·12 claims
- 0463US10640222B2Turbine engine having horizontally offset axesSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted May 5, 2020·1 cites·11 claims
- 0557US10946975B2Turbomachine comprising a trap for foreign objects circulating in an air flowSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Mar 16, 2021·1 cites·15 claims
- 0650US10837706B2Heat exchanger fitted with upstream cover to reduce disturbance to fluid flow in a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 17, 2020·0 cites·7 claims
- 0744US10415470B2Air inlet duct for an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Sep 17, 2019·0 cites·9 claims
- 0843US10054049B2Air guidance device for a turbomachine with grooves to maintain boundary layerSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Aug 21, 2018·0 cites·8 claims
- 0937US2016123228A1Air intake sleeve for an aircraft turboprop engineSNECMA·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →