Inventor · disambiguated record
Ken Lagueux
Also filed as: LAGUEUX KEN · LAGUEUX KEN R · Lagueux Ken Robert
9 granted patents·3 pending applications·319 citations·filing 1989–2015
90Inventor score
Top patents by PatentIndex Score
12 records- 0194US8944756B2Blade outer air seal assemblyLAGUEUX KEN·Filed 2011·Granted Feb 3, 2015·56 cites·20 claims
- 0294US6190124B1Columnar zirconium oxide abrasive coating for a gas turbine engine seal systemUNITED TECHNOLOGIES CORP·Filed 1997·Granted Feb 20, 2001·149 cites·20 claims
- 0378US8038388B2Abradable component for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2007·Granted Oct 18, 2011·10 cites·20 claims
- 0475US9797260B2Engine component with wear surface protectionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 24, 2017·2 cites·16 claims
- 0573US6180262B1Thermal coating compositionUNITED TECHNOLOGIES CORP·Filed 1997·Granted Jan 30, 2001·37 cites·3 claims
- 0664US10280783B2Turbomachinery blade outer air sealUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 7, 2019·2 cites·17 claims
- 0764US5090193AActive clearance control with cruise modeUNITED TECHNOLOGIES CORP·Filed 1989·Granted Feb 25, 1992·32 cites·2 claims
- 0851US5005352AClearance control method for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1989·Granted Apr 9, 1991·23 cites·5 claims
- 0938US2012099992A1Abrasive rotor coating for forming a seal in a gas turbine engineSTROCK CHRISTOPHER W·Filed 2010·Application pending·0 cites
- 1038US2013028705A1Gas turbine engine active clearance controlLAGUEUX KEN·Filed 2011·Application pending·0 cites
- 1135US2017074112A1Active clearance control for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 1234US5088885AMethod for protecting gas turbine engine sealsUNITED TECHNOLOGIES CORP·Filed 1989·Granted Feb 18, 1992·8 cites·4 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →