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Patent applications and USPTO patent grants for Blake; Mosheshe Camara-Khary.The latest application filed is for "enhanced adhesion thermal barrier coating".
Patent | Date |
---|---|
Enhanced adhesion thermal barrier coating Grant 11,306,600 - Blake , et al. April 19, 2 | 2022-04-19 |
Enhanced Adhesion Thermal Barrier Coating App 20210079797 - Blake; Mosheshe Camara-Khary ;   et al. | 2021-03-18 |
Enhanced adhesion thermal barrier coating Grant 10,731,482 - Blake , et al. | 2020-08-04 |
Gas turbine engine blade with ceramic tip and cooling arrangement Grant 10,415,394 - Slavens , et al. Sept | 2019-09-17 |
Article with sections having different microstructures and method therefor Grant 10,408,061 - Slavens , et al. Sept | 2019-09-10 |
Gas turbine engine component having curved turbulator Grant 10,316,668 - Blake , et al. | 2019-06-11 |
Heat temperature gradient heat exchanger Grant 10,260,422 - Slavens , et al. | 2019-04-16 |
Seal for gas turbine engine Grant 9,988,923 - Snyder , et al. June 5, 2 | 2018-06-05 |
Chordal seal Grant 9,863,259 - Boeke , et al. January 9, 2 | 2018-01-09 |
Heat Temperature Gradient Heat Exchanger App 20170321605 - Slavens; Thomas N. ;   et al. | 2017-11-09 |
Enhanced Adhesion Thermal Barrier Coating App 20170159460 - Blake; Mosheshe Camara-Khary ;   et al. | 2017-06-08 |
Chordal Seal App 20160333712 - Boeke; Mark A. ;   et al. | 2016-11-17 |
Gas Turbine Engine Blade With Ceramic Tip And Cooling Arrangement App 20160312617 - Slavens; Thomas N. ;   et al. | 2016-10-27 |
Seal For Gas Turbine Engine App 20160215644 - Snyder; Brooks E. ;   et al. | 2016-07-28 |
Article With Sections Having Different Microstructures And Method Therefor App 20160003051 - Slavens; Thomas N. ;   et al. | 2016-01-07 |
Gas Turbine Engine Component Having Curved Turbulator App 20150377029 - BLAKE; Mosheshe Camara-Khary ;   et al. | 2015-12-31 |
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