Inventor · disambiguated record
Richard H. Page
Also filed as: PAGE RICHARD · PAGE RICHARD H
10 granted patents·2 pending applications·150 citations·filing 2004–2014
90Inventor score
Top patents by PatentIndex Score
12 records- 0193US7686068B2Blade outer air seal cores and manufacture methodsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Mar 30, 2010·25 cites·20 claims
- 0287US8100165B2Investment casting cores and methodsPIGGUSH JUSTIN D·Filed 2008·Granted Jan 24, 2012·16 cites·21 claims
- 0383US9038700B2Process and refractory metal core for creating varying thickness microcircuits for turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2012·Granted May 26, 2015·7 cites·10 claims
- 0482US7713027B2Turbine blade with split impingement ribUNITED TECHNOLOGIES CORP·Filed 2006·Granted May 11, 2010·21 cites·20 claims
- 0581US7273353B2Shroud honeycomb cutterUNITED TECHNOLOGIES CORP·Filed 2006·Granted Sep 25, 2007·15 cites·11 claims
- 0671US8347947B2Process and refractory metal core for creating varying thickness microcircuits for turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2009·Granted Jan 8, 2013·11 cites·10 claims
- 0771US7094023B2Shroud honeycomb cutterUNITED TECHNOLOGIES CORP·Filed 2004·Granted Aug 22, 2006·13 cites·20 claims
- 0868US6997675B2Turbulated hole configurations for turbine bladesUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 14, 2006·24 cites·18 claims
- 0955US7114916B2Tailored turbulation for turbine bladesUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 3, 2006·15 cites·22 claims
- 1051US7726944B2Turbine blade with improved durability tip capUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jun 1, 2010·3 cites·12 claims
- 1140US2016001354A1Gas turbine engine component manufacturing method and core for making sameUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1238US2009208339A1Blade root stress reliefUNITED TECHNOLOGIES CORP·Filed 2008·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →