loadpatents
Patent applications and USPTO patent grants for Hauser; Ambrose A..The latest application filed is for "booster recirculation passageway and methods for recirculating air".
Patent | Date |
---|---|
Booster recirculation passageway and methods for recirculating air Grant 6,220,012 - Hauser , et al. April 24, 2 | 2001-04-24 |
Bearing lubrication configuration in a turbine engine Grant 5,813,214 - Moniz , et al. September 29, 1 | 1998-09-29 |
Gas turbine engine rotor support system Grant 5,361,580 - Ciokajlo , et al. November 8, 1 | 1994-11-08 |
Arched combustor Grant 5,335,502 - Roberts, Jr. , et al. August 9, 1 | 1994-08-09 |
Counterrotating turbine support assembly Grant 5,307,622 - Ciokajlo , et al. May 3, 1 | 1994-05-03 |
Gas turbine engine lubrication system Grant 5,272,868 - Ciokajlo , et al. December 28, 1 | 1993-12-28 |
Fan blade protection system Grant 5,224,831 - Hermans , et al. July 6, 1 | 1993-07-06 |
Turbine support assembly including turbine heat shield and bolt retainer assembly Grant 5,211,541 - Fledderjohn , et al. May 18, 1 | 1993-05-18 |
Compressor stator Grant 5,197,856 - Koertge , et al. March 30, 1 | 1993-03-30 |
Clearance control assembly having a thermally-controlled one-piece cylindrical housing for radially positioning shroud segments Grant 5,167,488 - Ciokajlo , et al. December 1, 1 | 1992-12-01 |
Aft entry cooling system and method for an aircraft engine Grant 5,134,844 - Lee , et al. August 4, 1 | 1992-08-04 |
Flexible connector for use in aircraft Grant 5,108,259 - Wakeman , et al. * April 28, 1 | 1992-04-28 |
Blade tip clearance control apparatus using cam-actuated shroud segment positioning mechanism Grant 5,049,033 - Corsmeier , et al. September 17, 1 | 1991-09-17 |
Blade tip clearance control apparatus with shroud segment position adjustment by unison ring movement Grant 5,035,573 - Tseng , et al. July 30, 1 | 1991-07-30 |
Mechanical blade tip clearance control apparatus for a gas turbine engine Grant 5,018,942 - Ciokajlo , et al. May 28, 1 | 1991-05-28 |
Blade carrying means Grant 4,863,352 - Hauser , et al. September 5, 1 | 1989-09-05 |
Power frame Grant 4,758,129 - Strock , et al. July 19, 1 | 1988-07-19 |
Aircraft engine or similar article Grant D286,880 - Smith, Jr. , et al. November 25, 1 | 1986-11-25 |
Thermally responsive labyrinth seal Grant 4,513,975 - Hauser , et al. April 30, 1 | 1985-04-30 |
Clearance control Grant 4,363,599 - Cline , et al. December 14, 1 | 1982-12-14 |
Fluid-cooled element Grant 4,353,679 - Hauser October 12, 1 | 1982-10-12 |
Seal vibration-reducing apparatus Grant 4,251,986 - Thompson , et al. February 24, 1 | 1981-02-24 |
Ceramic turbine shroud assembly Grant 4,087,199 - Hemsworth , et al. May 2, 1 | 1978-05-02 |
Method for forming cooling slot in airfoil blades Grant 3,934,322 - Hauser , et al. January 27, 1 | 1976-01-27 |
Cooling Slot For Airfoil Blade Grant 3,819,295 - Hauser , et al. June 25, 1 | 1974-06-25 |
Pin-fin Cooling System Grant 3,800,864 - Hauser , et al. April 2, 1 | 1974-04-02 |
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