Inventor · disambiguated record
Edward Vlasic
Also filed as: VLASIC EDWARD · VLASIC EDWARD PARKER
15 granted patents·4 pending applications·396 citations·filing 2006–2019
94Inventor score
Top patents by PatentIndex Score
19 records- 0194US9909434B2Integrated strut-vane nozzle (ISV) with uneven vane axial chordsPRATT & WHITNEY CANADA·Filed 2015·Granted Mar 6, 2018·11 cites·20 claims
- 0293US7611326B2HP turbine vane airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Nov 3, 2009·43 cites·16 claims
- 0393US7566200B2HP turbine vane airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Jul 28, 2009·41 cites·15 claims
- 0493US7559749B2LP turbine vane airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Jul 14, 2009·51 cites·15 claims
- 0593US7520728B2HP turbine vane airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Apr 21, 2009·50 cites·15 claims
- 0693US7520726B2HP turbine blade airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Apr 21, 2009·40 cites·15 claims
- 0793US7520727B2HP turbine blade airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Apr 21, 2009·42 cites·15 claims
- 0890US7632074B2HP turbine blade airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Dec 15, 2009·36 cites·15 claims
- 0989US11193380B2Integrated strut-vanePRATT & WHITNEY CANADA·Filed 2019·Granted Dec 7, 2021·4 cites·8 claims
- 1089US8105044B2Compressor turbine blade airfoil profileMARINI REMO·Filed 2010·Granted Jan 31, 2012·26 cites·14 claims
- 1189US7559748B2LP turbine blade airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Jul 14, 2009·36 cites·15 claims
- 1273US10221707B2Integrated strut-vanePRATT & WHITNEY CANADA·Filed 2013·Granted Mar 5, 2019·4 cites·8 claims
- 1367US7857594B2Turbine exhaust strut airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Dec 28, 2010·10 cites·13 claims
- 1450US9163510B2Strut for a gas turbine enginePRATT & WHITNEY CANADA·Filed 2014·Granted Oct 20, 2015·0 cites·5 claims
- 1545US8784051B2Strut for a gas turbine engineMARINI REMO·Filed 2008·Granted Jul 22, 2014·2 cites·13 claims
- 1644US2014241899A1Blade leading edge tip ribPRATT & WHITNEY CANADA·Filed 2013·Application pending·0 cites
- 1743US2015075169A1Integrated turbine exhaust struts and mixer of turbofan enginePRATT & WHITNEY CANADA·Filed 2014·Application pending·0 cites
- 1840US2010135822A1Turbine blade for a gas turbine engineMARINI REMO·Filed 2008·Application pending·0 cites
- 1935US2017030213A1Turbine section with tip flow vanesPRATT & WHITNEY CANADA·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →