Inventor · disambiguated record
Russell B. Hanson
Also filed as: HANSON RUSSELL · HANSON RUSSELL B
25 granted patents·4 pending applications·168 citations·filing 1982–2019
95Inventor score
Files withUNITED TECHNOLOGIES CORP23HANSON JR WALLACE A2HANSON RUSSELL B2MAREMONT CORP1WINTER MICHAEL1
Top patents by PatentIndex Score
29 records- 0197US9791153B2Line replaceable fuel nozzle apparatus, system and methodUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 17, 2017·14 cites·20 claims
- 0296US10082039B2Segmented annular sealUNITED TECHNOLOGIES CORP·Filed 2016·Granted Sep 25, 2018·19 cites·20 claims
- 0390US7721551B2Fan variable area nozzle for a gas turbine engine fan nacelleUNITED TECHNOLOGIES CORP·Filed 2006·Granted May 25, 2010·24 cites·18 claims
- 0489US7637095B2Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelleUNITED TECHNOLOGIES CORP·Filed 2006·Granted Dec 29, 2009·19 cites·9 claims
- 0586US4463663AHydraulic cylinder assembly with a liquid recovery systemHANSON JR WALLACE A·Filed 1982·Granted Aug 7, 1984·39 cites·11 claims
- 0683US9470151B2Alignment system and methodology to account for variation in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2012·Granted Oct 18, 2016·8 cites·8 claims
- 0772US9920693B2Hollow-wall heat shield for fuel injector componentUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 20, 2018·7 cites·18 claims
- 0869US10941669B2Diffuser case support structureUNITED TECHNOLOGIES CORP·Filed 2018·Granted Mar 9, 2021·1 cites·20 claims
- 0969US10190773B2Attachment stud on a combustor floatwall panel with internal cooling holesUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 29, 2019·3 cites·19 claims
- 1063US10648670B2Swirler assembly for a turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 12, 2020·1 cites·19 claims
- 1156US10816205B2Thermally isolated combustor pre-diffuserUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 27, 2020·0 cites·20 claims
- 1256US8769925B2Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelleWINTER MICHAEL·Filed 2009·Granted Jul 8, 2014·3 cites·9 claims
- 1356US2018202365A1Hollow-wall heat shield for fuel injector componentUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 1455US10335905B2Iso-grid composite componentUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 2, 2019·0 cites·20 claims
- 1555US10197285B2Gas turbine engine wall assembly interfaceUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 5, 2019·0 cites·20 claims
- 1654US8733800B1Tube having an integral, spring-loaded, spherical jointUNITED TECHNOLOGIES CORP·Filed 2012·Granted May 27, 2014·1 cites·8 claims
- 1753US10655855B2Gas turbine engine wall assembly with support shell contour regionsUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 19, 2020·0 cites·20 claims
- 1852US10570944B2Alignment system and methodology to account for variation in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 25, 2020·0 cites·6 claims
- 1951US11015636B2Nut strip assembly with array of captured nutsUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 25, 2021·0 cites·16 claims
- 2051US9789570B2Iso-grid composite componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 17, 2017·0 cites·20 claims
- 2150US11236677B2Diffuser case support structureUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 1, 2022·0 cites·20 claims
- 2249US11022144B2Diffuser case assemblyUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 1, 2021·0 cites·18 claims
- 2349US9126374B2Iso-grid composite componentHANSON RUSSELL B·Filed 2010·Granted Sep 8, 2015·0 cites·18 claims
- 2448US4484831APipe or tube assembly utilizing a differential screwHANSON JR WALLACE A·Filed 1982·Granted Nov 27, 1984·17 cites·11 claims
- 2548US2016201908A1Vena contracta swirling dilution passages for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2645US10815822B2Borescope plug assemblyUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 27, 2020·0 cites·16 claims
- 2745US4641814AOn-vehicle spring compressor toolMAREMONT CORP·Filed 1984·Granted Feb 10, 1987·12 cites·2 claims
- 2845US2021003284A1Combustor mounting structures for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2934US2014216042A1Combustor component with cooling holes formed by additive manufacturingHANSON RUSSELL B·Filed 2012·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →