Inventor · disambiguated record
Neil L. Tatman
Also filed as: TATMAN NEIL L
17 granted patents·39 citations·filing 2011–2019
90Inventor score
Top patents by PatentIndex Score
17 records- 0189US9822668B2Blade outer air seal spring clipsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Nov 21, 2017·6 cites·13 claims
- 0282US10801342B2Stator assembly for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 13, 2020·4 cites·23 claims
- 0380US10329934B2Reversible flow blade outer air sealUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 25, 2019·3 cites·20 claims
- 0480US10100670B2Heatshield assembly with double lap joint for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 16, 2018·6 cites·15 claims
- 0577US8919134B2Intershaft seal with support linkageTATMAN NEIL L·Filed 2011·Granted Dec 30, 2014·7 cites·8 claims
- 0675US11021962B2Turbulent air reducer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 1, 2021·2 cites·8 claims
- 0773US10815827B2Variable thickness core for gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 27, 2020·2 cites·26 claims
- 0873US9896955B2Static axial brush seal with dual bristle packsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 20, 2018·2 cites·20 claims
- 0970US10132187B2Clearance control assemblyUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 20, 2018·3 cites·18 claims
- 1066US10138748B2Gas turbine engine components with optimized leading edge geometryUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 27, 2018·1 cites·20 claims
- 1163US9366149B2Multi-stage high pressure compressor caseUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jun 14, 2016·2 cites·19 claims
- 1256US10184354B2Windback heat shieldUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 22, 2019·0 cites·18 claims
- 1355US11384841B2Brush seal with crossing bristlesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 12, 2022·0 cites·20 claims
- 1455US10240467B2Anti-rotation lug for a gas turbine engine stator assemblyTATMAN NEIL L·Filed 2012·Granted Mar 26, 2019·1 cites·11 claims
- 1550US10100667B2Axial flowing cooling passages for gas turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 16, 2018·0 cites·20 claims
- 1648US10408080B2Tailored thermal control system for gas turbine engine blade outer air seal arrayUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 10, 2019·0 cites·7 claims
- 1734US11035470B2Multi-plane brush sealUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 15, 2021·0 cites·19 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →