Inventor · disambiguated record
John David Stampfli
Also filed as: STAMPFLI JOHN DAVID
14 granted patents·2 pending applications·613 citations·filing 1998–2016
94Inventor score
Top patents by PatentIndex Score
16 records- 0196US6438484B1Method and apparatus for detecting and compensating for compressor surge in a gas turbine using remote monitoring and diagnosticsGEN ELECTRIC·Filed 2001·Granted Aug 20, 2002·142 cites·26 claims
- 0295US7186090B2Air foil shape for a compressor bladeGEN ELECTRIC·Filed 2004·Granted Mar 6, 2007·123 cites·15 claims
- 0395US6364602B1Method of air-flow measurement and active operating limit line management for compressor surge avoidanceGEN ELECTRIC·Filed 2000·Granted Apr 2, 2002·130 cites·20 claims
- 0494US10047620B2Circumferentially varying axial compressor endwall treatment for controlling leakage flow thereinGEN ELECTRIC·Filed 2014·Granted Aug 14, 2018·23 cites·15 claims
- 0594US7467926B2Stator blade airfoil profile for a compressorGEN ELECTRIC·Filed 2006·Granted Dec 23, 2008·51 cites·12 claims
- 0684US6226974B1Method of operation of industrial gas turbine for optimal performanceGEN ELECTRIC·Filed 1999·Granted May 8, 2001·88 cites·10 claims
- 0781US10415464B2Airfoil shape for thirteenth stage compressor rotor bladeGEN ELECTRIC·Filed 2016·Granted Sep 17, 2019·3 cites·24 claims
- 0880US10415585B2Airfoil shape for fourth stage compressor rotor bladeGEN ELECTRIC·Filed 2016·Granted Sep 17, 2019·3 cites·24 claims
- 0979US10443611B2Airfoil shape for eighth stage compressor rotor bladeGEN ELECTRIC·Filed 2016·Granted Oct 15, 2019·3 cites·24 claims
- 1077US10823194B2Compressor end-wall treatment with multiple flow axesGEN ELECTRIC·Filed 2014·Granted Nov 3, 2020·6 cites·20 claims
- 1174US9790796B2Systems and methods for modifying a pressure side on an airfoil about a trailing edgeGEN ELECTRIC·Filed 2013·Granted Oct 17, 2017·5 cites·1 claims
- 1268US8322145B2Systems and methods for providing surge protection to a turbine componentSNIDER DAVID AUGUST·Filed 2009·Granted Dec 4, 2012·11 cites·17 claims
- 1354US6220086B1Method for ascertaining surge pressure ratio in compressors for turbinesGEN ELECTRIC·Filed 1998·Granted Apr 24, 2001·21 cites·12 claims
- 1449US2016153465A1Axial compressor endwall treatment for controlling leakage flow thereinGEN ELECTRIC·Filed 2014·Application pending·0 cites
- 1547US6574584B2Method for evaluating compressor stall/surge margin requirementsGEN ELECTRIC·Filed 2000·Granted Jun 3, 2003·4 cites·23 claims
- 1644US2014130513A1System and method for improving gas turbine performance at part-load operationGEN ELECTRIC·Filed 2012·Application pending·0 cites
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