Inventor · disambiguated record
J. Page Strohl
Also filed as: STROHL J PAGE
10 granted patents·1 pending application·309 citations·filing 2003–2008
91Inventor score
Files withPOWER SYSTEMS MFG LLC7ALSTOM TECHNOLOGIES LTD LLC1BIONDO CHARLES1PARKER DAVID1POWER SYSTEM MFG LLC1
Top patents by PatentIndex Score
11 records- 0188US6932577B2Turbine blade airfoil having improved creep capabilityPOWER SYSTEMS MFG LLC·Filed 2003·Granted Aug 23, 2005·53 cites·10 claims
- 0287US6769878B1Turbine blade airfoilPOWER SYSTEMS MFG LLC·Filed 2003·Granted Aug 3, 2004·78 cites·12 claims
- 0387US6761536B1Turbine blade platform trailing edge undercutPOWER SYSTEMS MFG LLC·Filed 2003·Granted Jul 13, 2004·56 cites·4 claims
- 0482US7293957B2Vane platform rail configuration for reduced airfoil stressPOWER SYSTEMS MFG LLC·Filed 2007·Granted Nov 13, 2007·24 cites·20 claims
- 0580US8057188B2Compressor airfoilPARKER DAVID·Filed 2008·Granted Nov 15, 2011·20 cites·18 claims
- 0679US9322089B2Nickel-base alloy for gas turbine applicationsBIONDO CHARLES·Filed 2006·Granted Apr 26, 2016·7 cites·7 claims
- 0771US7618234B2Hook ring segment for a compressor vanePOWER SYSTEM MFG LLC·Filed 2007·Granted Nov 17, 2009·16 cites·20 claims
- 0868US7101150B2Fastened vane assemblyPOWER SYSTEMS MFG LLC·Filed 2004·Granted Sep 5, 2006·28 cites·17 claims
- 0960US7958735B2Turbine static structure for reduced leakage airPOWER SYSTEMS MFG LLC·Filed 2006·Granted Jun 14, 2011·7 cites·17 claims
- 1060US7229245B2Vane platform rail configuration for reduced airfoil stressPOWER SYSTEMS MFG LLC·Filed 2004·Granted Jun 12, 2007·20 cites·2 claims
- 1139US2009148298A1Blade disk sealALSTOM TECHNOLOGIES LTD LLC·Filed 2008·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →