Issued Patents All Time
Showing 25 most recent of 31 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 12421863 | Turbine engine tip clearance control system with thrust bearing | Andrew E. Breault | 2025-09-23 |
| 12404812 | Open rotor aircraft propulsion system with bypass flowpath | Andrew E. Breault, Jon E. Sobanski | 2025-09-02 |
| 12397924 | Open rotor aircraft propulsion system with bypass flowpath | Andrew E. Breault, Jon E. Sobanski | 2025-08-26 |
| 12352185 | Open rotor variable pitch blade with retracting inboard trailing edge | Andrew E. Breault, Jon E. Sobanski | 2025-07-08 |
| 12352287 | Variable guide vane for aircraft propulsion system | Stephen G. Pixton | 2025-07-08 |
| 12203385 | Telescoping guide vane for aircraft propulsion system | Stephen G. Pixton | 2025-01-21 |
| 12018587 | Turbine airfoil having cooling hole arrangement | Johan K. Westin, Jason B. Moran | 2024-06-25 |
| 11661852 | Turbine blade trailing edge cooling feed | Nicholas M. LoRicco, Parth Jariwala, Alex J. Schneider, Bret M. Teller, Matthew S. Gleiner | 2023-05-30 |
| 11384654 | Mateface for blade outer air seals in a gas turbine engine | Winston Gregory Smiddy, San Quach, Matthew D. Parekh | 2022-07-12 |
| 11346230 | Turbine blade cooling hole arrangement | Alex J. Schneider, Parth Jariwala, Nicholas M. LoRicco, Ryan Lundgreen, David A. Niezelski | 2022-05-31 |
| 11255197 | Impingement cooling arrangement for airfoils | Jason Shenny, Alberto A. Mateo, San Quach, Gregory Anselmi | 2022-02-22 |
| 11156359 | Combustor liner panel end rail with diffused interface passage for a gas turbine engine combustor | Donald W. Peters, San Quach, Matthew D. Parekh | 2021-10-26 |
| 11143037 | Turbine blade cooling hole arrangement | Alex J. Schneider, Timothy J. Jennings, David A. Niezelski, Nicholas M. LoRicco, Bret M. Teller | 2021-10-12 |
| 11098591 | Turbine blade with contoured fillet | David A. Niezelski | 2021-08-24 |
| 11098612 | Blade outer air seal including cooling trench | Winston Gregory Smiddy, San Quach, Matthew D. Parekh | 2021-08-24 |
| 10914178 | Airfoils having tapered tip flag cavity and cores for forming the same | Nicholas M. LoRicco | 2021-02-09 |
| 10830434 | Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor | San Quach, Matthew D. Parekh | 2020-11-10 |
| 10823411 | Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor | San Quach, Matthew D. Parekh | 2020-11-03 |
| 10815792 | Gas turbine engine component with a cooling circuit having a flared base | James Tilsley Auxier, Matthew S. Gleiner, Parth Jariwala, Charles Thistle, Megan J. Kwolek | 2020-10-27 |
| 10801325 | Turbine blade with tip vortex control and tip shelf | Dominic J. Mongillo, Scott D. Lewis | 2020-10-13 |
| 10731477 | Woven skin cores for turbine airfoils | San Quach | 2020-08-04 |
| 10718521 | Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor | San Quach, Matthew D. Parekh | 2020-07-21 |
| 10677462 | Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor | San Quach, Matthew D. Parekh | 2020-06-09 |
| 10633978 | Directional cooling arrangement for airfoils | San Quach, Alberto A. Mateo, Jason Shenny, Gregory Anselmi | 2020-04-28 |
| 10570748 | Impingement cooling arrangement for airfoils | Jason Shenny, Alberto A. Mateo, San Quach, Gregory Anselmi | 2020-02-25 |