Inventor · disambiguated record
Patrick James Mccomb
Also filed as: MCCOMB PATRICK J · MCCOMB PATRICK JAMES
9 granted patents·3 pending applications·22 citations·filing 2012–2017
80Inventor score
Top patents by PatentIndex Score
12 records- 0186US9828864B2Fan blade tall dovetail for individually bladed rotorsUNITED TECHNOLOGIES CORP·Filed 2013·Granted Nov 28, 2017·10 cites·12 claims
- 0284US9995152B2Hollow fan blade with extended wing sheathUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jun 12, 2018·10 cites·14 claims
- 0360US10323521B2Hybrid fan blade biscuit constructionUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jun 18, 2019·1 cites·17 claims
- 0456US10954804B2Rotary machines including a hybrid rotor with hollow and solid rotor blade setsUNITED TECHNOLOGIES CORP·Filed 2017·Granted Mar 23, 2021·0 cites·20 claims
- 0551US10408068B2Fan blade dovetail and spacerUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 10, 2019·1 cites·14 claims
- 0650US9896936B2Spinner for electrically grounding fan bladesUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 20, 2018·0 cites·19 claims
- 0744US9810078B2Rotary machines including a hybrid rotor with an integrally bladed rotor portionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Nov 7, 2017·0 cites·16 claims
- 0841US11118463B2Electrically grounding fan platformsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 14, 2021·0 cites·18 claims
- 0940US2014219808A1Sheath with extended wingsUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 1034US2016177732A1Hollow fan blade for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 1134US2017058916A1Gas turbine fan fairing platform and method of fairing a root leading edge of a fan blade of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 1232US10036261B2Blade dovetail bottomWHITEHURST SEAN A·Filed 2012·Granted Jul 31, 2018·0 cites·3 claims
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