Inventor · disambiguated record
Matthieu Jean Luc Vollebregt
Also filed as: VOLLEBREGT MATTHIEU JEAN LUC
16 granted patents·7 citations·filing 2014–2020
86Inventor score
Top patents by PatentIndex Score
16 records- 0179US10486226B2Core for manufacturing a turbomachine bladeSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 26, 2019·1 cites·10 claims
- 0274US9981308B2Method for manufacturing a core for moulding a bladeSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted May 29, 2018·1 cites·9 claims
- 0363US10618106B2Core for casting a blade of a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Apr 14, 2020·1 cites·7 claims
- 0460US10519980B2Turbomachine component or collection of components and associated turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Dec 31, 2019·2 cites·14 claims
- 0559US9869187B2Turbomachine turbine blade comprising a cooling circuit with improved homogeneitySAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jan 16, 2018·1 cites·10 claims
- 0656US10926444B2Assembly for manufacturing a turbine engine bladeSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Feb 23, 2021·0 cites·9 claims
- 0754US10344771B2Turbomachine component with non-axisymmetric surfaceSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Jul 9, 2019·1 cites·20 claims
- 0851US11135686B2Method of positioning a hollow workpieceSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Oct 5, 2021·0 cites·15 claims
- 0950US10913105B2Method for producing a pattern for lost pattern castingSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Feb 9, 2021·0 cites·8 claims
- 1046US10216867B2Method for modeling a non-axisymmetric surfaceSNECMA·Filed 2014·Granted Feb 26, 2019·0 cites·12 claims
- 1144US11925986B2Method for manufacturing a blade comprising a bathtub tip integrating a small wallSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Mar 12, 2024·0 cites·17 claims
- 1244US10682687B2Turbomachine blade cooling circuitSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jun 16, 2020·0 cites·11 claims
- 1339US11434769B2Impact-cooling tubular insert for a turbomachine distributorSAFRAN AIRCRAFT EGINES·Filed 2020·Granted Sep 6, 2022·0 cites·10 claims
- 1439US10864660B2Core for the moulding of a blade having superimposed cavities and including a de-dusting hole traversing a cavity from end to endSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 15, 2020·0 cites·4 claims
- 1538US10689985B2Turbine blade with optimised coolingSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jun 23, 2020·0 cites·13 claims
- 1638US10493520B2Unit for moulding a turbomachine blade, comprising a raised portion with a large cross-sectionSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 3, 2019·0 cites·9 claims
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