| Patent Number |
Title Of Patent |
Date Issued |
| 6852171 |
Method and apparatus for deicing mirrors or windows |
February 8, 2005 |
| Deicing of an external mirror (10) on a vehicle is effected by applying a sudden deformation force to the mirror. Sandwiched between the mirror (10) and a mounting surface (12) is a structure that includes a ribbon conductor (14), portions of which overlap each other in such a way that |
| 6839031 |
Wireless loop antenna battery saver |
January 4, 2005 |
| A wireless telephone antenna system including at least one loop antenna (12) providing a directional antenna field pattern with superior gain performance in comparison to an omnidirectional antenna. The antenna system effectively rotates the loop antenna and selects the best gain in a |
| 6774860 |
UAV (unmanned air vehicle) servoing dipole |
August 10, 2004 |
| Apparatus for controlling the rotational position of a dipole antenna (10) to compensate for roll and pitch movements of an unmanned air vehicle (UAV). The antenna (10) is connected to a dual-axis roll and pitch antenna mount (26), the rotational position is controlled by a pair of motor |
| 6148251 |
Touchtone electronic steering wheel |
November 14, 2000 |
| A steering wheel control system (10) that employs a method for passing push-button commands from a steering wheel to a vehicle system where the method is not dependant upon the contact resistance of a sliding contact (32) located in the steering wheel column. The control system (10) uses |
| 6054778 |
Electronic steering wheel technique for passing information with a programmable current source a |
April 25, 2000 |
| A steering wheel control system (10) that employs a method for passing push-button commands from a steering wheel to a vehicle system, wherein the method is not dependant upon the contact resistance of a sliding contact (32) located in the steering wheel column. The control system (10) |
| 5864221 |
Dedicated avionics standby power supply |
January 26, 1999 |
| A standby power supply dedicated to a peripheral electronics apparatus on aircraft provides an isolated ungrounded self-contained source of DC operating voltage. That source is applied to the electronics apparatus upon indication of turbine generator shut-down or failure before the v |
