Issued Patents All Time
Showing 1–11 of 11 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 11168571 | Airfoil having dead-end tip flag cavity | David A. Niezelski, Timothy J. Jennings, Bret M. Teller, Thomas N. Slavens | 2021-11-09 |
| 10982552 | Gas turbine engine component with film cooling hole | Sasha M. Moore, Clifford J. Musto, Timothy J. Jennings, Thomas N. Slavens, San Quach +3 more | 2021-04-20 |
| 10196902 | Cooling for gas turbine engine components | Sasha M. Moore, Timothy J. Jennings, Thomas N. Slavens, Clifford J. Musto, Nicholas M. LoRicco +3 more | 2019-02-05 |
| 10006371 | Film hole with in-wall accumulator | Thomas N. Slavens, Clifford J. Musto, Timothy J. Jennings, Nicholas M. LoRicco, Sasha M. Moore | 2018-06-26 |
| 9957810 | Film hole with protruding flow accumulator | Clifford J. Musto, Nicholas M. LoRicco, Thomas N. Slavens, Timothy J. Jennings, Carey Clum +3 more | 2018-05-01 |
| 9957814 | Gas turbine engine component with film cooling hole with accumulator | Clifford J. Musto, Sasha M. Moore, Thomas N. Slavens, San Quach, Nicholas M. LoRicco +1 more | 2018-05-01 |
| 9482103 | Intermediate additively manufactured component | Lea Kennard Castle, Brandon W. Spangler, JinQuan Xu | 2016-11-01 |
| 9415438 | Method for forming single crystal parts using additive manufacturing and remelt | Lea Kennard Castle, Brandon W. Spangler | 2016-08-16 |
| 9375782 | Regenerating an additively manufactured component | Lea Kennard Castle, Brandon W. Spangler, JinQuan Xu | 2016-06-28 |
| 9376920 | Gas turbine engine cooling hole with circular exit geometry | Brandon W. Spangler, Matthew A. Devore | 2016-06-28 |
| 9364888 | Regenerating an additively manufactured component to cure defects and alter microstructure | Lea Kennard Castle, Brandon W. Spangler, JinQuan Xu | 2016-06-14 |