Inventor · disambiguated record
Martin Schnieder
Also filed as: SCHNIEDER MARTIN
12 granted patents·1 pending application·110 citations·filing 2001–2017
89Inventor score
Files withALSTOM TECHNOLOGY LTD3KRUECKELS JOERG2SCHNIEDER MARTIN2ALSTOM SWITZERLAND LTD1ANSALDO ENERGIA IP UK LTD1
Top patents by PatentIndex Score
13 records- 0192US8770920B2Gas turbine airfoil with shaped trailing edge coolant ejection holesALSTOM TECHNOLOGY LTD·Filed 2012·Granted Jul 8, 2014·18 cites·17 claims
- 0290US8353663B2Shroud seal segments arrangement in a gas turbineALSTOM TECHNOLOGY LTD·Filed 2011·Granted Jan 15, 2013·24 cites·13 claims
- 0383US6595750B2Component of a flow machineALSTOM SWITZERLAND LTD·Filed 2001·Granted Jul 22, 2003·47 cites·11 claims
- 0475US8801366B2Stator blade for a gas turbine and gas turbine having sameDUECKERSHOFF ROLAND·Filed 2010·Granted Aug 12, 2014·7 cites·15 claims
- 0573US9932836B2Turbine bladeANSALDO ENERGIA IP UK LTD·Filed 2014·Granted Apr 3, 2018·5 cites·19 claims
- 0668US9062555B2Gas turbine blade and method for producing a bladeSCHNIEDER MARTIN·Filed 2012·Granted Jun 23, 2015·4 cites·14 claims
- 0755US9382804B2Cooled blade for a gas turbineALSTOM TECHNOLOGY LTD·Filed 2013·Granted Jul 5, 2016·2 cites·10 claims
- 0849US8182225B2Blade for a gas turbineKRUECKELS JOERG·Filed 2010·Granted May 22, 2012·1 cites·8 claims
- 0948US9097118B2Transitional region for a combustion chamber of a gas turbineSCHNIEDER MARTIN·Filed 2011·Granted Aug 4, 2015·1 cites·18 claims
- 1039US8718989B2Method to determine the internal structure of a heat conducting bodyCLIFTON ANDREW·Filed 2006·Granted May 6, 2014·1 cites·8 claims
- 1138US11255212B2Blade to stator heat shield interface in a gas turbineAnsaldo Energia Switzerland AG·Filed 2017·Granted Feb 22, 2022·0 cites·12 claims
- 1232US2012063891A1Cooled component for a gas turbineKRUECKELS JOERG·Filed 2011·Application pending·0 cites
- 1328US8057164B2Continuous-flow machine, turbine, or compressorEPPLER VOLKER·Filed 2009·Granted Nov 15, 2011·0 cites·14 claims
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