Issued Patents All Time
Showing 51–75 of 219 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 11125087 | Needled ceramic matrix composite cooling passages | Raymond Surace | 2021-09-21 |
| 11118474 | Vane cooling structures | Raymond Surace | 2021-09-14 |
| 11111802 | Seal for a gas turbine engine | Egon Salimusaj | 2021-09-07 |
| 11098595 | Airfoil for gas turbine engine | San Quach | 2021-08-24 |
| 11092017 | Mini core passage with protrusion | Allan N. Arisi | 2021-08-17 |
| 11092016 | Airfoil with dual profile leading end | — | 2021-08-17 |
| 11085325 | Turbine engine cooling system with an open loop circuit | Michael F. Blair, Mark F. Zelesky | 2021-08-10 |
| 11077494 | Method and casting core for forming a landing for welding a baffle inserted in an airfoil | — | 2021-08-03 |
| 11041395 | Airfoils and core assemblies for gas turbine engines and methods of manufacture | Emma J. Place, Timothy J. Jennings, Jeremy B. Fredette | 2021-06-22 |
| 11028702 | Airfoil with cooling passage network having flow guides | Allan N. Arisi | 2021-06-08 |
| 11028700 | Airfoil with cooling passage circuit through platforms and airfoil section | Allan N. Arisi | 2021-06-08 |
| 11014145 | Core assembly including studded spacer | James T. Auxier, Eric A. Hudson | 2021-05-25 |
| 11008979 | Passive centrifugal bleed valve system for a gas turbine engine | Michael G. McCaffrey | 2021-05-18 |
| 11002153 | Balance bracket | Alberto A. Mateo, San Quach | 2021-05-11 |
| 10987727 | Investment casting core system | — | 2021-04-27 |
| 10968777 | Chordal seal | Kyle J. Brevick | 2021-04-06 |
| 10968753 | Airfoil having impingement leading edge | Carey Clum, Timothy J. Jennings | 2021-04-06 |
| 10968752 | Turbine airfoil with minicore passage having sloped diffuser orifice | James Tilsley Auxier, Allan N. Arisi | 2021-04-06 |
| 10941663 | Airfoil having improved leading edge cooling scheme and damage resistance | Timothy J. Jennings, Kyle C. Lana | 2021-03-09 |
| 10914320 | Additive manufacturing process grown integrated torsional damper mechanism in gas turbine engine blade | Wendell V. Twelves, Pauline Cabrila | 2021-02-09 |
| 10907479 | Airfoil having improved leading edge cooling scheme and damage resistance | Timothy J. Jennings, Kyle C. Lana | 2021-02-02 |
| 10890079 | Gas turbine engine arc segments with arced walls | Justin M. Aniello, Kyle J. Brevick | 2021-01-12 |
| 10830438 | Modulated combustor bypass | Anton G. Banks | 2020-11-10 |
| 10815818 | Variable-pitch vane assembly | Raymond Surace, Robert L. Hazzard, Mark Borja | 2020-10-27 |
| 10808551 | Airfoil cooling circuits | Eric A. Hudson, San Quach, Matthew A. Devore | 2020-10-20 |