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Class Information
Number: 244/192
Name: Aeronautics > Aircraft control > Automatic > Electric course control > With "dead-zone" control
Description: System wherein the aircraft is governed by a command or control signal, and the aircraft temporarily flies in a condition in which it receives a null or minimal signal, and wherein the aircraft has no finite control signal applied thereto during the temporary period or minimal signal, in spite of which the aircraft continues to fly by its own mechanism.










Patents under this class:

Patent Number Title Of Patent Date Issued
6619592 Self-actuating firearm Sep. 16, 2003
6092703 Holster having a frontal reinforcement Jul. 25, 2000
5424950 Vehicle control surface position feedback compensator for reducing vehicle oscillation Jun. 13, 1995
5039037 Throttle control system having manual and automatic modes of operation Aug. 13, 1991
4471280 Anti-log power amplifier for reversible D.C. motor in automotive steering controls Sep. 11, 1984











 
 
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