Issued Patents All Time
Showing 26–50 of 90 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 11143038 | Gas turbine engine high lift airfoil cooling in stagnation zone | Matthew A. Devore | 2021-10-12 |
| 11098595 | Airfoil for gas turbine engine | Tracy A. Propheter-Hinckley | 2021-08-24 |
| 11098612 | Blade outer air seal including cooling trench | Winston Gregory Smiddy, Matthew D. Parekh, Jeffrey T. Morton | 2021-08-24 |
| 11085305 | Lost core structural frame | Steven Taffet, Brandon S. Donnell, Daniel C. Nadeau, Russell Deibel | 2021-08-10 |
| 11073285 | Combustor panel configuration with skewed side walls | Jeremy Styborski, Caroline Karanian | 2021-07-27 |
| 11002153 | Balance bracket | Alberto A. Mateo, Tracy A. Propheter-Hinckley | 2021-05-11 |
| 10982552 | Gas turbine engine component with film cooling hole | Sasha M. Moore, Clifford J. Musto, Timothy J. Jennings, Thomas N. Slavens, Nicholas M. LoRicco +3 more | 2021-04-20 |
| 10947854 | Internal cooling cavity with trip strips | Atul Kohli, Matthew A. Devore, Steven Bruce Gautschi | 2021-03-16 |
| 10830434 | Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor | Jeffrey T. Morton, Matthew D. Parekh | 2020-11-10 |
| 10823415 | Deflector for combustor of gas turbine engine | Kristy Rose Riley, John R. Battye, Joanne V. Rampersad | 2020-11-03 |
| 10821500 | Lost core molding cores for forming cooling passages | Lane Thornton, Steven Bruce Gautschi | 2020-11-03 |
| 10823411 | Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor | Jeffrey T. Morton, Matthew D. Parekh | 2020-11-03 |
| 10823412 | Panel surface pockets for coating retention | Andreas Sadil, Donald W. Peters | 2020-11-03 |
| 10808551 | Airfoil cooling circuits | Eric A. Hudson, Tracy A. Propheter-Hinckley, Matthew A. Devore | 2020-10-20 |
| 10801407 | Core assembly for gas turbine engine | Tracy A. Propheter-Hinckley | 2020-10-13 |
| 10731477 | Woven skin cores for turbine airfoils | Jeffrey T. Morton | 2020-08-04 |
| 10718521 | Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor | Jeffrey T. Morton, Matthew D. Parekh | 2020-07-21 |
| 10689988 | Disk lug impingement for gas turbine engine airfoil | Steven Bruce Gautschi, Tracy A. Propheter-Hinckley | 2020-06-23 |
| 10684014 | Combustor panel for gas turbine engine | Brian T. Hazel, Kaitlin M. Tomeo, Robert Selinsky, Jr., Aaron S. Butler, John S. Tu +2 more | 2020-06-16 |
| 10677462 | Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor | Jeffrey T. Morton, Matthew D. Parekh | 2020-06-09 |
| 10655473 | Gas turbine engine turbine blade leading edge tip trench cooling | Lane Thornton | 2020-05-19 |
| 10633978 | Directional cooling arrangement for airfoils | Alberto A. Mateo, Jeffrey T. Morton, Jason Shenny, Gregory Anselmi | 2020-04-28 |
| 10633981 | Airfoil tip pocket with augmentation features | Tracy A. Propheter-Hinckley, Steven Bruce Gautschi | 2020-04-28 |
| 10605094 | Internal cooling cavity with trip strips | Atul Kohli, Matthew A. Devore, Steven Bruce Gautschi | 2020-03-31 |
| 10570748 | Impingement cooling arrangement for airfoils | Jason Shenny, Jeffrey T. Morton, Alberto A. Mateo, Gregory Anselmi | 2020-02-25 |