Inventor · disambiguated record
Daniele Coutandin
Also filed as: COUTANDIN DANIELE
11 granted patents·6 pending applications·64 citations·filing 2002–2024
87Inventor score
Top patents by PatentIndex Score
17 records- 0184US11566532B2Turbine clearance control systemGE AVIO SRL·Filed 2021·Granted Jan 31, 2023·1 cites·18 claims
- 0280US9181805B2Gas turbine bladed rotor for aeronautic engines and method for cooling said bladed rotorCOUTANDIN DANIELE·Filed 2011·Granted Nov 10, 2015·8 cites·17 claims
- 0379US9132372B2Filter, in particular for a rotary separatorGE AVIO S R I·Filed 2013·Granted Sep 15, 2015·7 cites·10 claims
- 0470US9188008B2Gas turbine for aeronautic enginesCOUTANDIN DANIELE·Filed 2011·Granted Nov 17, 2015·7 cites·14 claims
- 0569US9662603B2Filtering net, in particular for a rotary separatorGE AVIO SRL·Filed 2013·Granted May 30, 2017·2 cites·10 claims
- 0661US9790810B2Stator casing cooling systemGE AVIO SRL·Filed 2013·Granted Oct 17, 2017·2 cites·21 claims
- 0757US6913440B2Variable-geometry turbine stator blade, particularly for aircraft enginesAVIO SPA·Filed 2003·Granted Jul 5, 2005·20 cites·12 claims
- 0853US6810672B2Gas turbine combustor, particularly for an aircraft engineFIATAVIO SPA·Filed 2002·Granted Nov 2, 2004·17 cites·8 claims
- 0950US2025146442A1Aircraft system having a thermal management systemGE AVIO SRL·Filed 2024·Application pending·0 cites
- 1049US9623361B2Filter provided with structural elements, in particular for a rotary separatorGE AVIO SRL·Filed 2013·Granted Apr 18, 2017·0 cites·6 claims
- 1145US11905853B2Turbine engine component with a set of deflectorsGE AVIO SRL·Filed 2021·Granted Feb 20, 2024·0 cites·16 claims
- 1241US2021404348A1Turbine engine sealing and methodGE AVIO SRL·Filed 2021·Application pending·0 cites
- 1338US2017130601A1Gas turbine engine stage provided with a labyrinth sealGE AVIO SRL·Filed 2016·Application pending·0 cites
- 1434US11739643B2Method and apparatus for cooling a portion of a counter-rotating turbine engineGE AVIO SRL·Filed 2021·Granted Aug 29, 2023·0 cites·20 claims
- 1528US2004109763A1Method of producing and assembling a cooling device inside an axial-flow gas turbine blade, and axial-flow gas turbine blade produced using such a methodAVIO SPA·Filed 2003·Application pending·0 cites
- 1628US2004107538A1Hinge device for a rotary member of an aircraft engineAVIO SPA·Filed 2003·Application pending·0 cites
- 1724US2003017051A1Double-wall blade for a turbine, particularly for aeronautical applicationsFIATAVIO SPA·Filed 2002·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →