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):

Report Date:

1978-10-17

Pagination or Media Count:

4.0

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

Subject Categories:

  • Aircraft
  • Hydraulic and Pneumatic Equipment

Distribution Statement:

APPROVED FOR PUBLIC RELEASE