Aircraft trim actuator shutdown monitor system and method

Details Aircraft trim actuator shutdown monitor system and method Aircraft trim actuator shutdown monitor system and method

1983-05-02

1986-07-08

Gruber, Felix D.

Boots, shoes, and leggings

364433, 364434, 318565, 244194, G05D 100, G05D 2302, G06F 1520

Patent

active

045996989

ABSTRACT:
The directions of travel of an inner and an outer loop actuator are monitored for movement in opposite directions within selected ranges and the outer loop actuator is disabled under selected conditions. These conditions may include movement of both the inner and outer loop actuators in opposite directions, any one of which has been detected moving at a rate greater than a selected rate or to a position outside a selected range. The invention is particularly suited for an aircraft trim actuator shutdown monitor system.

REFERENCES:
patent: 3969664 (1976-07-01), Camillieri et al.
patent: 4043526 (1977-08-01), Donley et al.
patent: 4337516 (1982-06-01), Murphy et al.
patent: 4374423 (1983-02-01), Kundler et al.
patent: 4472806 (1984-09-01), Blair
Stern: Preliminary Design of an Integrated Redundant Digital Flight Control System for the Maritime Patrol Aircraft.
Conference Fort Worth, TX, USA. Challenge of the 80's, 3rd. Digital Avionics Systems, Nov. 1979, pp 101-116.

Affiliated with

Also associated with

Rating

Aircraft trim actuator shutdown monitor system and method does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft trim actuator shutdown monitor system and method, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft trim actuator shutdown monitor system and method will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1455317