Issued Patents 2019
Showing 1–16 of 16 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 10519778 | Gas turbine engine component with converging/diverging cooling passage | Glenn Levasseur | 2019-12-31 |
| 10487666 | Cooling hole with enhanced flow attachment | Glenn Levasseur | 2019-11-26 |
| 10464135 | Additive manufacturing method for the addition of features within cooling holes | — | 2019-11-05 |
| 10458331 | Fuel injector with heat pipe cooling | — | 2019-10-29 |
| 10443428 | Gas turbine engine having minimum cooling airflow | — | 2019-10-15 |
| 10400674 | Cooled fuel injector system for a gas turbine engine and method for operating the same | — | 2019-09-03 |
| 10371052 | Integrated thermal management with nacelle laminar flow control for geared architecture gas turbine engine | — | 2019-08-06 |
| 10371381 | Combustor wall for a gas turbine engine and method of acoustic dampening | — | 2019-08-06 |
| 10329920 | Multi-lobed cooling hole | — | 2019-06-25 |
| 10323522 | Gas turbine engine component with diffusive cooling hole | — | 2019-06-18 |
| 10307817 | Additively manufactured casting articles for manufacturing gas turbine engine parts | Thomas N. Slavens, Mark F. Zelesky, Joel H. Wagner | 2019-06-04 |
| 10302100 | Gas turbine engine having a mistuned stage | Frederic Tisdall Tenney | 2019-05-28 |
| 10294801 | Rotor blade having anti-wear surface | Glenn Levasseur, Gregory M. Dolansky | 2019-05-21 |
| 10280764 | Multiple diffusing cooling hole | — | 2019-05-07 |
| 10215030 | Cooling hole for a gas turbine engine component | — | 2019-02-26 |
| 10208603 | Staggered crossovers for airfoils | Scott D. Lewis | 2019-02-19 |