Strohl; J. Page
Patent Applications and Registrations
Patent applications and USPTO patent grants for Strohl; J. Page.The latest application filed is for "nickel-base alloy for gas turbine applications".
- Strohl; J. Page - Stuart FL US
- Strohl; J. Page - Tequesta FL
| Patent | Date |
|---|---|
| Nickel-base alloy for gas turbine applications Grant 9,322,089 - Biondo , et al. April 26, 2 | 2016-04-26 |
| Compressor airfoil Grant 8,057,188 - Parker , et al. November 15, 2 | 2011-11-15 |
| Turbine static structure for reduced leakage air Grant 7,958,735 - Ellis , et al. June 14, 2 | 2011-06-14 |
| Nickel-base alloy for gas turbine applications App 20100080729 - Biondo; Charles ; et al. | 2010-04-01 |
| Compressor Airfoil App 20090290987 - PARKER; DAVID ; et al. | 2009-11-26 |
| Hook ring segment for a compressor vane Grant 7,618,234 - Brackett , et al. November 17, 2 | 2009-11-17 |
| Blade Disk Seal App 20090148298 - Strohl; J. Page ; et al. | 2009-06-11 |
| Hook Ring Segment For A Compressor Vane App 20080193290 - Brackett; James G. ; et al. | 2008-08-14 |
| Turbine Static Structure for Reduced Leakage Air App 20080148737 - Ellis; Charlie ; et al. | 2008-06-26 |
| Vane platform rail configuration for reduced airfoil stress Grant 7,293,957 - Ellis , et al. November 13, 2 | 2007-11-13 |
| Vane Platform Rail Configuration For Reduced Airfoil Stress App 20070166154 - ELLIS; CHARLIE ; et al. | 2007-07-19 |
| Vane platform rail configuration for reduced airfoil stress Grant 7,229,245 - Ellis , et al. June 12, 2 | 2007-06-12 |
| Fastened vane assembly Grant 7,101,150 - Bash , et al. September 5, 2 | 2006-09-05 |
| Vane platform rail configuration for reduced airfoil stress App 20060013685 - Ellis; Charles A. ; et al. | 2006-01-19 |
| Fastened vane assembly App 20050254944 - Bash, Gary ; et al. | 2005-11-17 |
| Turbine blade airfoil having improved creep capability Grant 6,932,577 - Strohl , et al. August 23, 2 | 2005-08-23 |
| Turbine Blade Airfoil Having Improved Creep Capability App 20050111978 - Strohl, J. Page ; et al. | 2005-05-26 |
| Turbine blade airfoil Grant 6,769,878 - Parker , et al. August 3, 2 | 2004-08-03 |
| Turbine blade platform trailing edge undercut Grant 6,761,536 - Bash , et al. July 13, 2 | 2004-07-13 |
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