Inventor · disambiguated record
Michael F. Blair
Also filed as: BLAIR MICHAEL · BLAIR MICHAEL F
17 granted patents·1 pending application·292 citations·filing 1990–2018
94Inventor score
Files withUNITED TECHNOLOGIES CORP12SHARMA OM P3ABDEL-MESSEH WILLIAM1BLAIR MICHAEL F1UNITED TECHNLOGIES CORP1
Top patents by PatentIndex Score
18 records- 0194US8105030B2Cooled airfoils and gas turbine engine systems involving such airfoilsABDEL-MESSEH WILLIAM·Filed 2008·Granted Jan 31, 2012·49 cites·20 claims
- 0293US7837441B2Impingement skin core cooling for gas turbine engine bladeUNITED TECHNOLOGIES CORP·Filed 2007·Granted Nov 23, 2010·21 cites·16 claims
- 0393US7686068B2Blade outer air seal cores and manufacture methodsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Mar 30, 2010·25 cites·20 claims
- 0489US8066052B2Cooled wall thickness controlBLAIR MICHAEL F·Filed 2007·Granted Nov 29, 2011·23 cites·20 claims
- 0585US7984607B2Gas turbine engine systems and related methods involving vane-blade count ratios greater than unityUNITED TECHNOLOGIES CORP·Filed 2007·Granted Jul 26, 2011·21 cites·8 claims
- 0683US5370831AMethod of molding polymeric skins for trim productsUNITED TECHNOLOGIES CORP·Filed 1992·Granted Dec 6, 1994·44 cites·4 claims
- 0781US11085325B2Turbine engine cooling system with an open loop circuitUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 10, 2021·1 cites·19 claims
- 0881US8973374B2Blades in a turbine section of a gas turbine engineSHARMA OM P·Filed 2011·Granted Mar 10, 2015·7 cites·11 claims
- 0977US10480326B2Vane for variable area turbineUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 19, 2019·2 cites·16 claims
- 1076US10156359B2Gas turbine engine component having vascular engineered lattice structureUNITED TECHNOLOGIES CORP·Filed 2013·Granted Dec 18, 2018·3 cites·17 claims
- 1175US7137776B2Film cooling for microcircuitsUNITED TECHNOLOGIES CORP·Filed 2002·Granted Nov 21, 2006·41 cites·16 claims
- 1274US9739171B2Turbine engine cooling system with an open loop circuitUNITED TECHNOLOGIES CORP·Filed 2012·Granted Aug 22, 2017·3 cites·9 claims
- 1373US7766615B2Local indented trailing edge heat transfer devicesUNITED TECHNLOGIES CORP·Filed 2007·Granted Aug 3, 2010·14 cites·18 claims
- 1471US8468797B2Gas turbine engine systems and related methods involving vane-blade count ratios greater than unitySHARMA OM P·Filed 2011·Granted Jun 25, 2013·4 cites·11 claims
- 1567US5090866AHigh temperature leading edge vane insertUNITED TECHNOLOGIES CORP·Filed 1990·Granted Feb 25, 1992·34 cites·6 claims
- 1660US10047631B2Turbine engine cooling system with an open loop circuitUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 14, 2018·0 cites·12 claims
- 1748US8516793B2Gas turbine engine systems and related methods involving vane-blade count ratios greater than unitySHARMA OM P·Filed 2011·Granted Aug 27, 2013·0 cites·7 claims
- 1844US2015227677A1Gas Turbine Engine With First Turbine Vane ClockingUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
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