Inventor · disambiguated record
Lane Thornton
Also filed as: THORNTON LANE · THORNTON LANE M · THORNTON LANE MIKAL
22 granted patents·14 pending applications·35 citations·filing 2012–2025
92Inventor score
Top patents by PatentIndex Score
36 records- 0193US10208602B2Asymmetric diffuser opening for film cooling holesUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 19, 2019·11 cites·20 claims
- 0290US9845694B2Flow directing cover for engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 19, 2017·5 cites·12 claims
- 0386US10458264B2Seal arrangement for turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 29, 2019·4 cites·13 claims
- 0479US11008873B2Turbine blade tip wall coolingUNITED TECHNOLOGIES CORP·Filed 2019·Granted May 18, 2021·2 cites·15 claims
- 0578US10259039B2Gas turbine engine component cooling passage and space casting coreUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 16, 2019·1 cites·5 claims
- 0677US10273809B2Centrifugal airfoil cooling modulationUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 30, 2019·4 cites·22 claims
- 0777US10113441B2Thermally driven spring valve for turbine gas path partsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 30, 2018·2 cites·14 claims
- 0876US10821500B2Lost core molding cores for forming cooling passagesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 3, 2020·0 cites·10 claims
- 0975US10844730B2Centrifugal airfoil cooling modulationUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 24, 2020·1 cites·25 claims
- 1071US10005123B2Lost core molding cores for forming cooling passagesUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 26, 2018·0 cites·16 claims
- 1169US12503759B2Chemical vapor infiltration tooling hole modification for optimizing infiltration in ceramic matrix compositesRAYTHEON TECH CORP·Filed 2023·Granted Dec 23, 2025·0 cites·17 claims
- 1269US2025389193A1Variable thickness coating controlRTX CORP·Filed 2025·Application pending·0 cites
- 1368US12479775B2Chemical vapor infiltration tooling for optimizing infiltration in ceramic matrix compositesRAYTHEON TECH CORP·Filed 2023·Granted Nov 25, 2025·0 cites·20 claims
- 1466US10196915B2Trailing edge platform sealsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 5, 2019·1 cites·16 claims
- 1563US11781439B2Seal arrangement for turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 10, 2023·0 cites·22 claims
- 1663US2024300141A1Chemical vapor infiltration tooling for optimizing infiltration in ceramic matrix compositesRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 1762US10655473B2Gas turbine engine turbine blade leading edge tip trench coolingUNITED TECHNOLOGIES CORP·Filed 2012·Granted May 19, 2020·2 cites·10 claims
- 1860US10465543B2Flow directing cover for engine componentUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 5, 2019·0 cites·14 claims
- 1959US10738619B2Fan cooling hole arrayUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 11, 2020·1 cites·6 claims
- 2059US2019176228A1Gas turbine engine component cooling passage and space eating coreUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2158US2019003333A1Thermally driven spring valve for turbine gas path partsUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 2254US10370979B2Baffle for a component of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·0 cites·20 claims
- 2350US9228441B2Passive thermostatic valveTHORNTON LANE·Filed 2012·Granted Jan 5, 2016·1 cites·17 claims
- 2449US10400607B2Large-footprint turbine cooling holeUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 3, 2019·0 cites·26 claims
- 2548US10711640B2Cooled cooling air to blade outer air seal passing through a static vaneUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 14, 2020·0 cites·13 claims
- 2644US2019309685A1Fluid injection coolingUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 2743US2016298465A1Gas turbine engine component cooling passage with asymmetrical pedestalsUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2843US2018291760A1Cooling air chamber for blade outer air sealUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 2943US2016169001A1Diffused platform cooling holesUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3042US2016208620A1Gas turbine engine airfoil turbulator for airfoil creep resistanceUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 3142US2019345833A1Vane including internal radiant heat shieldUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 3240US11215061B2Blade with wearable tip-rub-portions above squealer pocketUNITED TECHNOLOGIES CORP·Filed 2020·Granted Jan 4, 2022·0 cites·14 claims
- 3340US2014075947A1Gas turbine engine component cooling circuitUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 3437US2016298462A1Cooling passages for a gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 3535US2016326909A1Gas turbine engine component with separation rib for cooling passagesUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 3632US2015322797A1Blade element cross-tiesSNYDER DANIEL A·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →