Multiple loop control system

• US 4,542,679 A
• Filed: 12/15/1983
• Issued: 09/24/1985
• Est. Priority Date: 02/17/1981
• Status: Expired due to Term

• Current Assignee: Bell Helicopter Michigan Inc (Textron Inc)
• Original Assignee: Textron Inc
• Inventors: Murphy, Milford R., Haskins, Delbert E.
• Primary Examiner(s): Maslousky, Paul E.
• Application Number:
  US06/562,068
• Time in Patent Office: 649 Days
• Field of Search: 91/363 A, 91/509, 91/513, 91/522, 318/564, 318/565, 244/178, 244/194
• US Class Current: 91/363.00A
• CPC Class Codes: F15B 18/00 Parallel arrangements of independent servomotor systems
• CPC Class Codes: G05B 9/03 with multiple-channel loop, i.e. redundant control systems
• CPC Class Codes: G05D 1/0077 using redundant signals or controls

Abstract

A redundant, dual-fail/operate fly-by-wire control system actuates a redundant tandem piston actuator (10) to provide a single composite output evidenced by movement of a piston rod (12). The basic fault-tolerate actuation system consists of dual hydraulic primary actuators, quadruplex electrical control loops (14-17), and control servo valves (22-25). A failure management system connects to the actuation system by means of lines (18-21) to control the servo valves (22-25). The four control loops (14-17) connect to a pilot controller that provides a pilot individual input signals to amplifiers (26-29) for each of the control loops. A tracking loop (450) includes switches (480, 482, 484) for connecting the four control loops (14-17) and providing isolation therebetween.

Claims

1. A multiple loop control system providing a single composite output, comprising:

a plurality of actuators, each actuator receiving at least two separate control signals and generating an output interconnected with the output of all other actuators in the plurality to provide a single composite output;

a plurality of control loops, at least one connected to each of said actuators, each control loop responsive to an individual input signal and generating one of said control signals to one of the actuators;

failure monitoring means connected to each of said actuators and the control loops to monitor the operation thereof, said failure monitoring means including means responsive to a monitor signal from each actuator, and means responsive to the monitor signal from one actuator having a difference from the monitor signals for the other actuators above a first threshold level to generate a disengage signal to one of the actuators for a failure condition, said failure monitoring means further including means for detecting a hard-type failure and inert-type failure and means for generating the disengage signal at a lower threshold level for an inert-type failure than for a hard-type failure; and

said failure monitoring means further including means connected to each of said plurality of control loops for isolating each of said plurality of control loops from each other.

2. The multiple loop control system of claim 1 wherein said isolating means includes:

switch means for interconnecting the output of one of said plurality of control loops to each of the other ones of said plurality of control loops.

3. The multiple loop control system of claim 1 wherein each actuator includes a servo valve with the output of each servo valve interconnected to provide the single composite output.

4. The multiple loop control system of claim 3 wherein each servo valve is of the electrohydraulic type including a valve coil and the output of each control loop provides a control signal to one of the valve coils.

5. The multiple loop control system of claim 4 wherein each electrohydraulic servo valve includes a position transducer generating a monitor signal to the failure monitoring means.

6. An actuation system to control a hydraulic actuator, comprising:

a plurality of electrohydraulic actuators, each actuator including at least two servo valves each having a valve coil receiving an independent control signal, the sum of the outputs of each actuator combine to provide an output varying with the combination of the individual control signals;

a plurality of control loops, one for each valve coil, and responsive to individual input signals and generating the control signal to one of the valve coils;

a position transducer in each servo valve and responsive to the servo valve position and generating a feedback signal;

failure monitoring means connected to each of the control loops and responsive to the individual feedback signals to monitor the operation of each actuator and disengage a control loop upon detection of a failure; and

said failure monitoring means further including means connected to each of said plurality of control loops for isolating each of said plurality of control loops from each other.

7. The actuation system to control a hydraulic actuator of claim 6 wherein the failure monitoring means includes means responsive to a preset differential between one of the feedback signals and the remaining feedback signals to generate a disengage signal to one of the servo valves.

8. The actuation system to control a hydraulic actuator of claim 7 wherein said failure monitoring means includes means responsive to a preset differential between one of the feedback signals and the remaining feedback signals to generate a differential signal, and means responsive to a preset differential signal above a threshold level to generate the disengage-signal to the one servo valve.

9. The actuation system to control a hydraulic actuator of claim 6 wherein said failure monitoring means includes a time delay connected to said means responsive to the preset differential signal above a threshold level to delay the generation of the disengage signal for a predetermined time interval.

10. A four loop actuation system to control a hydrualic actuator, comprising:

four electrohydraulic servo valves, one for each loop of the actuation system, each servo valve providing a drive signal to the hydraulic actuator;

each servo valve including a valve coil receiving an independent control signal to actuate the interconnected servo valve;

four control loops, one for each valve coil and responsive to individual input signals and generating the control signal to the interconnected valve coil;

a position transducer connected to each electrohydraulic servo valve and responsive to valve position to generate a feedback signal;

failure monitoring means connected to each of the control loops and responsive to the individual feedback signals to monitor the operation of each loop and disengage a control loop upon detection of a failure; and

said failure monitoring means further including switch means connected to each of said control loops for isolating one of said four control loops from the other three of said four control loops.

11. The four loop actuation system of claim 10 wherein said failure monitoring means includes means responsive to a preset differential between one of the feedback signals and the remaining three feedback signals to generate a disengage signal to one of the control loops.

12. The four loop actuation system of claim 11 wherein said failure monitoring means further includes means responsive to a preset differential above a threshold level to generate the disengage signal to the one loop only when the differential exceeds the threshold.

13. The four loop actuation system of claim 11 wherein said failure monitoring means includes time delay means responsive to the disengage signal to delay the connection of the disengage signal to the one loop for a predetermined time interval.

14. The four loop actuation system of claim 13 wherein said failure monitoring means includes means for detecting a hard-type failure and an inert-type failure, and wherein said means responsive to the preset differential above a threshold level generates the disengage signal for an inert-type failure at a lower threshold level than for a hard-type failure.

15. A multiple control loop system providing a single composite output, comprising:

a plurality of actuators, each actuator receiving at least two separate control signals and generating an output interconnected with the outputs of all other actuators of the plurality to provide a single composite output;

a plurality of control loops, at least one connected to each of said actuators, each control loop responsive to an individual input signal and generating one of said control signals to one of the actuators;

failure monitoring means connected to each of said actuators and the control loops to monitor the operation thereof and provide a disengage signal to one of the control loops for a failure condition, said failure monitoring means further including means for generating an alignment signal for each control loop to align the actuators; and

said failure monitoring means further including means connected to each of said plurality of control loops for isolating each of said plurality of control loops from each other.

16. The multiple control loop system of claim 15 wherein said isolating means includes:

switch means for interconnecting the output of one of said plurality of control loops to each of the other ones of said plurality of control loops.