Inventor · disambiguated record
Laurent Pierre Tarnowski
Also filed as: TARNOWSKI LAURENT · TARNOWSKI LAURENT PIERRE
10 granted patents·3 pending applications·22 citations·filing 2009–2021
82Inventor score
Files withSAFRAN HELICOPTER ENGINES6PORODO JEROME2BRILLET CHRISTOPHE MICHEL GEORGES MARCEL1HERRAN MATHIEU1PORODO JÉRÔME YVES FÉLIX GILBERT1
Top patents by PatentIndex Score
13 records- 0180US9611862B2Air bleed having an inertial filter in the tandem rotor of a compressorBRILLET CHRISTOPHE MICHEL GEORGES MARCEL·Filed 2010·Granted Apr 4, 2017·11 cites·11 claims
- 0268US9890792B2Radial or mixed-flow compressor diffuser having vanesTURBOMECA·Filed 2014·Granted Feb 13, 2018·3 cites·11 claims
- 0365US9683576B2Centrifugal compressor impellerHERRAN MATHIEU·Filed 2012·Granted Jun 20, 2017·4 cites·9 claims
- 0458US8641373B2Diffuser having blades with aperturesPORODO JEROME·Filed 2009·Granted Feb 4, 2014·4 cites·14 claims
- 0549US11988112B2Recovered-cycle aircraft turbomachineSAFRAN HELICOPTER ENGINES·Filed 2021·Granted May 21, 2024·0 cites·10 claims
- 0648US11852033B2Rotor blade for a turbomachineSAFRAN HELICOPTER ENGINES·Filed 2021·Granted Dec 26, 2023·0 cites·14 claims
- 0745US12435729B2Method for manufacturing a compressor impeller for a turbomachineSAFRAN HELICOPTER ENGINES·Filed 2020·Granted Oct 7, 2025·0 cites·5 claims
- 0845US12286926B2Recovered-cycle aircraft turbomachineSAFRAN HELICOPTER ENGINES·Filed 2021·Granted Apr 29, 2025·0 cites·21 claims
- 0942US11187234B2Wheel blade for turbomachine, comprising a winglet at its tip and at the leading edgeSAFRAN HELICOPTER ENGINES·Filed 2018·Granted Nov 30, 2021·0 cites·14 claims
- 1035US2014133957A1Method of diffusing a gas turbine compression stage, and diffusion stage for implementing sameTARNOWSKI LAURENT PIERRE·Filed 2012·Application pending·0 cites
- 1134US9618008B2Gas turbine diffuser blowing method and corresponding diffuserPORODO JÉRÔME YVES FÉLIX GILBERT·Filed 2012·Granted Apr 11, 2017·0 cites·13 claims
- 1232US2012087800A1Centrifugal impeller for a compressorPORODO JEROME·Filed 2010·Application pending·0 cites
- 1330US2023175527A1Turbomachine compressor having a stationary wall provided with a shape treatmentSAFRAN HELICOPTER ENGINES·Filed 2021·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →