Issued Patents All Time
Showing 351–375 of 379 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 6981846 | Vortex cooling of turbine blades | — | 2006-01-03 |
| 6971851 | Multi-metered film cooled blade tip | — | 2005-12-06 |
| 6955525 | Cooling system for an outer wall of a turbine blade | — | 2005-10-18 |
| 6939102 | Flow guide component with enhanced cooling | — | 2005-09-06 |
| 6932573 | Turbine blade having a vortex forming cooling system for a trailing edge | — | 2005-08-23 |
| 6918742 | Combustion turbine with airfoil having multi-section diffusion cooling holes and methods of making same | — | 2005-07-19 |
| 6916150 | Cooling system for a tip of a turbine blade | — | 2005-07-12 |
| 6902372 | Cooling system for a turbine blade | — | 2005-06-07 |
| 6869268 | Combustion turbine with airfoil having enhanced leading edge diffusion holes and related methods | — | 2005-03-22 |
| 6808367 | Cooling system for a turbine blade having a double outer wall | — | 2004-10-26 |
| 6616406 | Airfoil trailing edge cooling construction | — | 2003-09-09 |
| 6602052 | Airfoil tip squealer cooling construction | — | 2003-08-05 |
| 6471480 | Thin walled cooled hollow tip shroud | J. Tyson Balkcum, Timothy J. Remley, Christopher Williams, Hans R. Przirembel | 2002-10-29 |
| 6301877 | Ejector extension cooling for exhaust nozzle | William J. Yeager, John F. Soileau | 2001-10-16 |
| 6210111 | Turbine blade with platform cooling | — | 2001-04-03 |
| 6164059 | Multi-expansion ejector nozzle with diverging walls | John F. Soileau | 2000-12-26 |
| 6139269 | Turbine blade with multi-pass cooling and cooling air addition | — | 2000-10-31 |
| 5975851 | Turbine blade with trailing edge root section cooling | — | 1999-11-02 |
| 5605046 | Cooled liner apparatus | — | 1997-02-25 |
| 5407133 | Cooled thin metal liner | — | 1995-04-18 |
| 5157917 | Gas turbine engine cooling air flow | George W. Beal, Gary J. Dillard | 1992-10-27 |
| 5077969 | Cooled liner for hot gas conduit | Curtis C. Cowan | 1992-01-07 |
| 5056307 | Exhaust nozzle cooling utilizing total engine flow | — | 1991-10-15 |
| 5039562 | Method and apparatus for cooling high temperature ceramic turbine blade portions | — | 1991-08-13 |
| 5030060 | Method and apparatus for cooling high temperature ceramic turbine blade portions | — | 1991-07-09 |