Inventor · disambiguated record
Brooks E. Snyder
Also filed as: SNYDER BROOKS E
27 granted patents·8 pending applications·81 citations·filing 2014–2019
94Inventor score
Files withUNITED TECHNOLOGIES CORP35
Top patents by PatentIndex Score
35 records- 0196US9713843B2Method for additively constructing internal channelsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 25, 2017·14 cites·15 claims
- 0295US9988923B2Seal for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 5, 2018·24 cites·15 claims
- 0395US9932841B2Workpiece manufactured from an additive manufacturing system having a particle separator and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 3, 2018·8 cites·14 claims
- 0493US10012088B2Additive manufacturing system utilizing an epitaxy process and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 3, 2018·5 cites·20 claims
- 0582US10370981B2Gas turbine engine component cooling circuit with respirating pedestalUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·3 cites·12 claims
- 0682US9932835B2Airfoil cooling device and method of manufactureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 3, 2018·3 cites·18 claims
- 0779US10066549B2Variable vane segmentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 4, 2018·2 cites·14 claims
- 0878US9845524B2Fixture for application of coatings and method of using sameUNITED TECHNOLOGIES CORP·Filed 2014·Granted Dec 19, 2017·1 cites·19 claims
- 0977US10612392B2Gas turbine engine component with conformal fillet cooling pathUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 7, 2020·2 cites·13 claims
- 1077US10094229B2Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 9, 2018·2 cites·14 claims
- 1175US10012090B2Airfoil cooling apparatusUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 3, 2018·2 cites·19 claims
- 1274US10240464B2Gas turbine engine airfoil with leading edge trench and impingement coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 26, 2019·4 cites·16 claims
- 1373US10960460B2Additive manufactured mold, a method of manufacturing the mold, and a workpiece casted from the moldUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 30, 2021·1 cites·7 claims
- 1472US10683768B2Circumferential axial segmented trough sealUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 16, 2020·4 cites·9 claims
- 1569US11591914B2Cupped contour for gas turbine engine blade assemblyUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 28, 2023·0 cites·16 claims
- 1666US2019085719A1Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal partsUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 1764US10935240B2Additive manufactured combustor heat shieldUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 2, 2021·1 cites·15 claims
- 1864US10364683B2Gas turbine engine component cooling passage turbulatorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jul 30, 2019·2 cites·11 claims
- 1963US10487667B2Airfoil, and method for manufacturing the sameUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 26, 2019·2 cites·25 claims
- 2061US10465530B2Gas turbine engine component cooling cavity with vortex promoting featuresUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 5, 2019·1 cites·9 claims
- 2161US2020011187A1Gas turbine engine component cooling cavity with vortex promoting featuresUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2260US10094240B2Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal partsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 9, 2018·0 cites·13 claims
- 2358US10344597B2Cupped contour for gas turbine engine blade assemblyUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 9, 2019·0 cites·19 claims
- 2458US2018298820A1Variable vane segmentUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 2554US10434545B2Particle separator for an additive manufacturing system and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 8, 2019·0 cites·19 claims
- 2654US10436039B2Gas turbine engine turbine blade tip coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 8, 2019·0 cites·16 claims
- 2749US10494929B2Cooled airfoil structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 3, 2019·0 cites·17 claims
- 2848US10208604B2Cooling features with three dimensional chevron geometryUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 19, 2019·0 cites·15 claims
- 2948US2016222793A1Cooling configuration for engine componentUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3045US10179948B2Method and system for controlling coating in non-line-of-sight locationsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 15, 2019·0 cites·4 claims
- 3144US10563583B2Bore-cooled film dispensing pedestalsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 18, 2020·0 cites·23 claims
- 3243US2016313005A1Additive manufactured combustor heat shield with cooled attachment studUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 3341US2016332371A1Additive manufacturing system and method of operationUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 3439US2017211404A1Blade outer air seal having surface layer with pocketsUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 3538US2017051625A1Blade outer air seal component with varying thermal expansion coefficientUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →