Inventor · disambiguated record
Kevin N. Mccusker
Also filed as: MCCUSKER KEVIN · MCCUSKER KEVIN N
8 granted patents·1 pending application·209 citations·filing 1994–2022
88Inventor score
Top patents by PatentIndex Score
9 records- 0184US11555416B2Rotor stack bushing with adaptive temperature metering for a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Jan 17, 2023·1 cites·9 claims
- 0284US8992177B2High solidity and low entrance angle impellers on turbine rotor diskWU CHARLES C·Filed 2011·Granted Mar 31, 2015·10 cites·11 claims
- 0381US8167547B2Gas turbine engine with canted pocket and canted knife edge sealWU CHARLES C·Filed 2007·Granted May 1, 2012·28 cites·7 claims
- 0478US5439348ATurbine shroud segment including a coating layer having varying thicknessUNITED TECHNOLOGIES CORP·Filed 1994·Granted Aug 8, 1995·63 cites·5 claims
- 0570US7690896B2Gas turbine disk slots and gas turbine engine using sameUNITED TECHNOLOGIES CORP·Filed 2005·Granted Apr 6, 2010·15 cites·14 claims
- 0668US6852280B2Condensed perfusion circuit for cardiopulmonary bypass and cardioplegiaFiled 2003·Granted Feb 8, 2005·49 cites·31 claims
- 0767US6946099B2Methods of using condensed perfusion circuit for cardiopulmonary bypass and cardioplegiaVIJAY VENKATARAMANA·Filed 2003·Granted Sep 20, 2005·43 cites·9 claims
- 0861US11352903B2Rotor stack bushing with adaptive temperature metering for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2020·Granted Jun 7, 2022·0 cites·10 claims
- 0935US2013017059A1Hole for rotating component cooling systemUNITED TECHNOLOGIES CORP·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →