Inventor · disambiguated record
Mark A. Boeke
Also filed as: BOEKE MARK A
15 granted patents·3 pending applications·70 citations·filing 2012–2016
91Inventor score
Top patents by PatentIndex Score
18 records- 0191US10072517B2Gas turbine engine component having variable width feather seal slotUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 11, 2018·22 cites·20 claims
- 0289US10024172B2Gas turbine engine airfoilUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 17, 2018·6 cites·18 claims
- 0389US9863259B2Chordal sealUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jan 9, 2018·8 cites·20 claims
- 0488US10648353B2Low loss airfoil platform rim seal assemblyUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 12, 2020·5 cites·10 claims
- 0588US10557360B2Vane intersegment gap sealing arrangementUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 11, 2020·5 cites·17 claims
- 0684US10329937B2Flowpath component for a gas turbine engine including a chordal sealUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jun 25, 2019·4 cites·15 claims
- 0784US9752446B2Support buttressUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 5, 2017·4 cites·18 claims
- 0878US10273820B2Turbine vane cooling arrangementUNITED TECHNOLOGIES CORP·Filed 2016·Granted Apr 30, 2019·2 cites·10 claims
- 0978US9334755B2Airfoil with variable trip strip heightUNITED TECHNOLOGIES CORP·Filed 2012·Granted May 10, 2016·6 cites·13 claims
- 1077US9982560B2Cooling feed orificesUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 29, 2018·3 cites·17 claims
- 1175US10196913B1Featherseal having tapered radial portionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 5, 2019·2 cites·9 claims
- 1262US10294806B2Multiple coating configurationUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 21, 2019·0 cites·16 claims
- 1356US9080452B2Gas turbine engine airfoil with vane platform cooling passageUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jul 14, 2015·1 cites·14 claims
- 1454US10107107B2Gas turbine engine component with discharge slot having oval geometryBOEKE MARK A·Filed 2012·Granted Oct 23, 2018·2 cites·22 claims
- 1547US2016003152A1Gas turbine engine multi-vaned stator cooling configurationUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1646US10443401B2Cooled turbine vane with alternately orientated film cooling hole rowsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 15, 2019·0 cites·20 claims
- 1738US2017198601A1Internally cooled ni-base superalloy component with spallation-resistant tbc systemUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 1836US2016326894A1Airfoil cooling passageUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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