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Patent applications and USPTO patent grants for Wakeman; Thomas G..The latest application filed is for "turbo machine shroud-to-rotor blade dynamic clearance control".
Patent | Date |
---|---|
Turbo machine shroud-to-rotor blade dynamic clearance control Grant 5,601,402 - Wakeman , et al. February 11, 1 | 1997-02-11 |
Expansion joint for fluid piping with rotation prevention member Grant 5,370,427 - Hoelle , et al. December 6, 1 | 1994-12-06 |
Tube coupling assembly Grant 5,350,200 - Peterson , et al. September 27, 1 | 1994-09-27 |
Aircraft engine thrust mount Grant 5,320,307 - Spofford , et al. June 14, 1 | 1994-06-14 |
Fan blade protection system Grant 5,224,831 - Hermans , et al. July 6, 1 | 1993-07-06 |
Apparatus for removably attaching a core frame to a vane frame with a stable mid ring Grant 5,222,360 - Antuna , et al. June 29, 1 | 1993-06-29 |
Gas turbine engine multi-hole film cooled combustor liner and method of manufacture Grant 5,181,379 - Wakeman , et al. January 26, 1 | 1993-01-26 |
Gas turbine engine structural frame with multi-yoke attachment of struts to outer casing Grant 5,180,282 - Lenhart , et al. January 19, 1 | 1993-01-19 |
Compressor discharge flowpath Grant 5,165,850 - Humke , et al. November 24, 1 | 1992-11-24 |
Torque multiplier for aircraft propeller Grant 5,154,372 - Hora , et al. October 13, 1 | 1992-10-13 |
Turbine shroud clearance control assembly Grant 5,127,793 - Walker , et al. July 7, 1 | 1992-07-07 |
Flexible connector for use in aircraft Grant 5,108,259 - Wakeman , et al. * April 28, 1 | 1992-04-28 |
Blade carrying means Grant 4,863,352 - Hauser , et al. September 5, 1 | 1989-09-05 |
Non-contacting flowpath seal Grant 4,752,185 - Butler , et al. June 21, 1 | 1988-06-21 |
Fabricated liner article and method Grant 4,688,310 - Kelm , et al. August 25, 1 | 1987-08-25 |
Blade pitch varying means Grant 4,657,484 - Wakeman , et al. April 14, 1 | 1987-04-14 |
Fabricated liner article and method Grant 4,628,694 - Kelm , et al. December 16, 1 | 1986-12-16 |
Combustion chamber construction Grant 4,614,082 - Sterman , et al. * September 30, 1 | 1986-09-30 |
Combustion chamber construction Grant 4,555,901 - Wakeman , et al. * December 3, 1 | 1985-12-03 |
Thermally responsive labyrinth seal Grant 4,513,975 - Hauser , et al. April 30, 1 | 1985-04-30 |
Compact air-to-air heat exchanger for jet engine application Grant 4,187,675 - Wakeman February 12, 1 | 1980-02-12 |
Compact fuel-to-air heat exchanger for jet engine application Grant 4,120,150 - Wakeman October 17, 1 | 1978-10-17 |
Cooling system for a thrust vectoring gas turbine engine exhaust system Grant 4,000,612 - Wakeman , et al. January 4, 1 | 1977-01-04 |
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