Inventor · disambiguated record
Hubert Pascal Verdier
Also filed as: VERDIER HUBERT · VERDIER HUBERT PASCAL
5 granted patents·3 pending applications·15 citations·filing 2002–2020
69Inventor score
Files withTURBOMECA3COURTIE PHILIPPE ROGER1SAFRAN AIRCRAFT ENGINES1SAFRAN HELICOPTER ENGINES1SAVARY NICOLAS1
Top patents by PatentIndex Score
8 records- 0164US10551064B2Annular wall of a combustion chamber with improved cooling at the level of primary and/or dilution holesSAFRAN AIRCRAFT ENGINES·Filed 2012·Granted Feb 4, 2020·3 cites·11 claims
- 0246US11867401B2Pre-vaporizing pipe, combustion assembly provided therewith and turbomachine provided therewithSAFRAN HELICOPTER ENGINES·Filed 2020·Granted Jan 9, 2024·0 cites·16 claims
- 0345US7249721B2Device and method for injecting a liquid fuel into an air flow for a combustion chamberTURBOMECA·Filed 2002·Granted Jul 31, 2007·12 cites·6 claims
- 0442US2015369489A1Turbo machine combustion assembly comprising an improved fuel supply circuitTURBOMECA·Filed 2014·Application pending·0 cites
- 0539US10156358B2Combustion chamber wallSAVARY NICOLAS·Filed 2012·Granted Dec 18, 2018·0 cites·13 claims
- 0633US2008209910A1Method of starting a gas turbine helicopter engine, a fuel feed circuit for such an engine, and an engine having such a circuitTURBOMECA·Filed 2008·Application pending·0 cites
- 0732US2012210725A1Non-flame-out test for the combustion chamber of a turbine engineCOURTIE PHILIPPE ROGER·Filed 2010·Application pending·0 cites
- 0822US9518512B2Method for starting a turbomachineVERDIER HUBERT PASCAL·Filed 2012·Granted Dec 13, 2016·0 cites·10 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →