# US 9,752,512 B2 · Actuator control device

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- Number: US 9,752,512 B2
- Document ID: US9752512B2
- Status: Granted
- Kind: B2
- Application number: 14/849,126
- Filed: 2015-09-09
- Published: 2015-12-31
- Granted: 2017-09-05
- Earliest claimed: 2013-03-14
- Assignees: IHI Corporation
- Applicants: IHI Corporation
- Inventors: Hiroyuki Furukawa; Takafumi Imazu
- Web page: https://patentgrep.com/patent/US9752512B2

## CPC

- F02C 9/20: by throttling; by adjusting vanes
- F15B 11/16: with two or more servomotors
- F15B 2211/6336: representing a state of the output member, e.g. position, speed or acceleration
- F15B 2211/7107: the output members being mechanically linked
- F15B 2211/76: Control of force or torque of the output member
- F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00)
- F15B: SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR

## Abstract

An actuator control device detects a displacement of a piston in a first actuator, controls the first actuator by feedback control, measures both of forces generated in first and second actuators, corrects a target position command value for a piston in the second actuator in accordance with an amount of imbalance between the forces, and controls the second actuator in accordance with the difference between the corrected command value and a feedback value of a displacement position of the second piston.

## Claims

### Claim 1

An actuator control device for controlling first and second actuators comprising first and second pistons respectively connected to points of application of forces on a coaxial synchronous link, the points of application being located on opposite sides of a center of rotation of the coaxial synchronous link, the actuator control device comprising:
a first servo valve for driving ejection and retraction of the first piston;
a second servo valve for driving ejection and retraction of the second piston independently of the first servo valve;
displacement sensors for detecting displacement positions of the first and second pistons, respectively;
force sensors for measuring forces generated in the first and second actuators, respectively; and
a control unit for controlling the first and second servo valves, the control unit configured to:
detect the displacement position of the first piston,
control the first servo valve by feedback control so that a position of the first piston matches a target position command value,
measure both of forces generated in the first and second actuators,
correct a target position command value for the second piston in accordance with an amount of imbalance between the forces, and
control the second servo valve in accordance with a difference between the corrected command value and a feedback value of the displacement position of the second piston so that a position of the second piston matches the corrected command value.

### Claim 2 (depends on 1)

The actuator control device according to claim 1, wherein the control unit is configured to:
measure both of forces generated in the first and second actuators by use of a feedback value of the displacement position of the first piston instead of the target position command value for the second actuator as a target position command value,
correct the target position command value for the piston of the second actuator in accordance with an amount of imbalance between the forces, and
control the second servo valve in accordance with a difference between the corrected command value and a feedback value of the displacement position of the piston of the second actuator so that the position of the piston of the second actuator matches the corrected command value.

### Claim 3 (depends on 2)

The actuator control device according to claim 2, wherein the control unit is further configured to:
control each of the first actuator and the second actuator by employing an active-standby configuration, and
alternately activate systems every time any one of start-up and a malfunction in one of the systems occurs.

### Claim 4 (depends on 2)

The actuator control device according to claim 2, wherein the control unit is further configured to:
control each of the first actuator and the second actuator by employing an active-active configuration, and
alternately activate systems every time any one of start-up and a malfunction in one of the systems occurs.

### Claim 5 (depends on 1)

The actuator control device according to claim 1, wherein the control unit is further configured to:
control each of the first actuator and the second actuator by employing an active-standby configuration, and
alternately activate systems every time any one of start-up and a malfunction in one of the systems occurs.

### Claim 6 (depends on 1)

The actuator control device according to claim 1, wherein the control unit is further configured to:
control each of the first actuator and the second actuator by employing an active-active configuration, and
alternately activate systems every time any one of start-up and a malfunction in one of the systems occurs.