Examples of 'control actuator' in a sentence
Meaning of "control actuator"
A control actuator is a device used to control or manipulate a system. In the context of engineering or automation, it is typically used to regulate or adjust the movement, position, or flow of a mechanism or process
How to use "control actuator" in a sentence
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control actuator
Flow control actuator with an adjustable frequency.
That thing is the electric control actuator.
Control actuator or effector responding to the status transition computer.
This invention relates to a speed control actuator.
Electromechanical valve control actuator for internal combustion engines.
Sensing load relief by a secondary path of a flight control actuator.
Monitoring of a flight control actuator of an aircraft.
Control actuator housing.
Externally driven flow control actuator.
A currently used flow control actuator may take the form of a fluidic oscillator.
The present invention relates to detection of a fault in a flight control actuator.
A currently used type of flow control actuator may take the form of a fluidic oscillator.
A similar coupling is advantageously provided for the flow control actuator.
Figure 4 is an illustration of a flow control actuator in accordance with an illustrative embodiment ;.
The said adjustment means may be operable by a depth control actuator.
See also
Figure 5 is an exploded view of a flow control actuator in accordance with an illustrative embodiment ;.
This invention relates to a device for testing the detection of load on a flight control actuator.
Monitoring system for monitoring a flight control actuator of an aircraft, comprising,.
In a first embodiment, the associated drive elements include a linear control actuator.
Preferably, said control actuator has a first end hinged to the support group.
Access method of the present invention does not intend to control actuator head rigorously.
Preferably, said control actuator has a second end hinged to the guiding frame.
An electrical control system for driving said control actuator electrically ;.
A third control actuator 113 may be configured to selectively activate a massage mode.
Consequently, the forces generated by the control actuator can be smaller.
The control actuator 3 comprises a cylinder 4 and a piston 5 connected to the drive rod 2.
Switch 9 is closed by actuating an external control actuator that is not illustrated.
Control device with servocontrol loop, particularly an electro-hydraulic flight control actuator.
In this illustrative example, flow control actuator is an externally driven flow control actuator.
This makes it possible to limit the electrical power consumption of the control actuator 4.
Control ring driven by said direction control actuator using said frangible transmission part ;.
Preferably, said first sensor continuously measures the position of said control actuator.
As explained in the above paragraph, the upper control actuator rod poses various production problems.
The present invention relates to a highly versatile fluid-actuated valve control actuator.
FIGS . 1 to 4 are schematic representations of a flight control actuator 1 with a primary path and a secondary path.
The present invention relates to servo-control devices, in particular for an aircraft flight control actuator.
FIG . 1 diagrammatically shows a flight control actuator 1 with a primary path and a secondary path.
FIG . 2 is a graph showing the measured position of the stopper rod control actuator versus time.
In an embodiment, the flow control actuator 1165 can include multiple actuators.
In Figure 9, an illustration of fluid flow out of a flow control actuator is shown.
As stated earlier, the flight control actuator 12 includes a primary load path 1 and a secondary load path 10.
The alignment may also be maintained by locking the control actuator 22 hydraulically.
The flow control actuator 28 may also be a pulse-width-modulation type rather than a degree-of-pinch type.
The present invention concerns a system for monitoring a flight control actuator of an aircraft, including,.
Controller 112 can control actuator 128 such that a particular repetition rate and duty cycle are achieved.
Servo-control devices, in particular for an aircraft flight control actuator.
In FIGS . 2 to 4, the control actuator 4 shown comprises a primary path 5 and an independent secondary path 6.
Apparatus according to claim 15, wherein the adjustment means is operable by a depth control actuator.
The roller control actuator 330 receives opposed hydraulic fluid pressures through lines S1, S2.
This voltage is rectified by the rectifying circuit 4 and drive the control actuator 41.
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Examples of using Actuator
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Rotate actuator lever to depress switch plunger
Care and adjustment of the actuator cables
Actuator latch engages automatically during coupling
