loadpatents
Patent applications and USPTO patent grants for Fowler; Donald W..The latest application filed is for "harmonic data transfer in rotary wing aircraft".
Patent | Date |
---|---|
Harmonic data transfer in rotary wing aircraft Grant 9,203,459 - Sane , et al. December 1, 2 | 2015-12-01 |
Harmonic Data Transfer In Rotary Wing Aircraft App 20140314130 - Sane; Harshad S. ;   et al. | 2014-10-23 |
Module for integrated approach to an offshore facility Grant 8,442,706 - Doeppner , et al. May 14, 2 | 2013-05-14 |
Flight control system for rotary wing aircraft Grant 8,271,151 - Hasan , et al. September 18, 2 | 2012-09-18 |
Flight Control System For Rotary Wing Aircraft App 20120072056 - Hasan; Muhammad Emadul ;   et al. | 2012-03-22 |
Module For Integrated Approach To An Offshore Facility App 20100168939 - Doeppner; Ronald S. ;   et al. | 2010-07-01 |
Helicopter integrated fire and flight control having a pre-launch and post-launch maneuver director Grant 5,465,212 - Fowler , et al. November 7, 1 | 1995-11-07 |
Helicopter integrated fire and flight control having azimuth and pitch control Grant 5,431,084 - Fowler , et al. July 11, 1 | 1995-07-11 |
Helicopter integrated fire and flight control having azimuth and pitch control Grant 5,331,881 - Fowler , et al. July 26, 1 | 1994-07-26 |
Helicopter integrated fire and flight control having constraint limiting control Grant 5,310,136 - Fowler , et al. May 10, 1 | 1994-05-10 |
Helicopter integrated fire and flight control having coordinated area bombing control Grant 5,310,135 - Fowler , et al. May 10, 1 | 1994-05-10 |
Safety coupling arrangement Grant 4,527,816 - Bresie , et al. July 9, 1 | 1985-07-09 |
Natural gas loading station Grant 4,483,376 - Bresie , et al. November 20, 1 | 1984-11-20 |
Method and apparatus for producing natural gas from tight formations Grant 4,479,546 - Bresie , et al. October 30, 1 | 1984-10-30 |
Helicopter force feel actuator automatic static null compensation Grant 4,382,281 - Fowler , et al. May 3, 1 | 1983-05-03 |
Updated lock-positioning of foldable helicopter blades Grant 4,376,979 - Fowler , et al. March 15, 1 | 1983-03-15 |
Adaptive aircraft actuator fault detection Grant 4,355,358 - Clelford , et al. October 19, 1 | 1982-10-19 |
Force feel actuator with limited proportional/integral error feedback Grant 4,313,165 - Clelford , et al. January 26, 1 | 1982-01-26 |
Force feel actuator fault detection with directional threshold Grant 4,294,162 - Fowler , et al. October 13, 1 | 1981-10-13 |
Method and system for producing and transporting natural gas Grant 4,213,476 - Bresie , et al. July 22, 1 | 1980-07-22 |
Aerodynamic surface control feel augmentation system Grant 3,960,348 - Fowler , et al. June 1, 1 | 1976-06-01 |
Load Stability System Grant 3,833,189 - Fowler , et al. September 3, 1 | 1974-09-03 |
Load Stability System Grant 3,756,543 - Fowler , et al. September 4, 1 | 1973-09-04 |
Fault Detector For Helicopter Feel Augmentation System Grant 3,719,336 - Fowler , et al. March 6, 1 | 1973-03-06 |
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