Accession Number : ADD005556

Title :   In-Line Actuator Monitoring and Control Apparatus.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Westermeier,Theodore F

Report Date : 17 Oct 1978

Pagination or Media Count : 4

Abstract : An in-line actuator monitoring apparatus utilized in a redundant actuator system for determining which of the two redundant secondary actuators in a flight control system has failed and providing a disable signal to the failed actuator unit. (Author)

Descriptors :   *Patents, *Flight control systems, *Hydraulic actuators, Backup systems, Monitoring, Redundant components, Failure(Mechanics), Logic circuits, Signals

Subject Categories : Aircraft
      Hydraulic and Pneumatic Equipment

Distribution Statement : APPROVED FOR PUBLIC RELEASE