JPH0621841B2 - Wind tunnel wind speed controller - Google Patents

Description

TECHNICAL FIELD The present invention relates to a wind speed control device for a wind tunnel.

BACKGROUND ART Wind tunnels are widely used as a means for investigating the aerodynamic characteristics of structures such as bridges and high-rise buildings. Wind tunnels are also used to study the aerodynamic performance of vehicles and flying objects. Furthermore, wind tunnels are also used to simulate atmospheric and meteorological conditions. Generally, when the survey object is large, a scale model is used, and when the survey object is small, the real thing is used for the test.

The equipment of the wind tunnel is basically (a) an air flow source that is a blower that causes an air flow, (b) an air conditioner that adjusts the temperature and humidity of the air, and (c) an object to be investigated. A measuring unit for installing a test object, (d) a measuring device provided in the measuring unit for measuring the aerodynamic performance of the object of investigation, and (e) limiting the air flow spatially and making the flow uniform. And (f) a controller for adjusting the air source and the air conditioner to obtain a predetermined air flow condition. The present invention relates to a wind speed control device for adjusting the wind speed among the control devices in such a wind tunnel.

As prior arts of such a wind tunnel wind speed control device, JP-A-57-149943 and JP-A-59-69817 are known.

In such a prior art, when the capacity of the motor that drives the blower is relatively low, or when abrupt acceleration / deceleration is performed under a high load, the motor or an inverter that energizes the motor is overloaded and trips. .

When the motor or the inverter trips, the operation is temporarily stopped and then restarted for safety. Since the blower and the motor have large inertia, it takes a long time, for example, about 10 minutes until the blower and the motor stop. Also, when conducting a thermal experiment using a wind tunnel, the trip causes the thermal equilibrium state to collapse, so to establish the same thermal equilibrium state, for example, 2
It takes as long as ~ 3 hours.

If the motor and the inverter are operated within a range that does not cause overload, tripping will not be necessary, but doing so will limit the capacity of the equipment, and thus the motor and the inverter that are larger than the specified capacity. Result in higher costs.

Problems to be Solved by the Invention An object of the present invention is to prevent the operation from being stopped due to overload and to improve the efficiency of experiments. Another objective is to reduce the equipment capacity and cost. That is, an object of the present invention is to detect the occurrence of an overload and prevent the equipment or device from stopping in the overload area for a long time.

Means for Solving the Problems The present invention provides (a) a wind velocity control device for a wind tunnel that blows air from blowers 2 and 3 to an object to be tested through a wind pipe, and (b) sets the wind velocity of the blown air. And a blower 2, 3 in response to the output of the wind speed setting means 1.
Fan control means 7, 8 and 29 for generating a signal ε for controlling the rotation speed of the fan, and (d) means 89 and 90 for detecting overload of the fans 2 and 3.
(E) Subtractors 33, 107 for subtracting the input signal from the rotation speed control signal ε and giving the blowers 2, 3; (f) Overload limiting circuit 91, (f1) Subtracting the integrated output (F2) In response to the outputs of the overload detection means 89, 90 in response to the outputs of the overload detection means 89, 90, when the overload is detected, the rotation speed control means ε is applied to the integration circuit 95, A wind tunnel wind speed control device comprising: an overload limiting circuit 91 having means 75 and SW4 for giving a signal to the integrating circuit 95 to make the output of the integrating circuit 95 zero when no overload is detected. Is.

Further, in the present invention, the blower control means 7, 8 and 29 are means 7 for detecting the wind speed of the blown air, and the rotation speed control signal representing the deviation between the output of the wind speed setting means 1 and the output of the wind speed detecting means 7. Generates ε and blowers 2 and 3
The negative feed back control means 8 and 29 for controlling the rotational speeds of the blowers 2 and 3 so that the deviation becomes zero.
It is characterized by including and.

Further, the present invention relates to (a) a wind velocity control device for a wind tunnel that blows air from blowers 2 and 3 through a wind pipe onto an object to be tested, and (b) means 1 for setting the wind velocity of the blown air; c) In response to the output of the wind speed setting means 1, the blowers 2 and 3
Blower control means 7, 8, 29 for controlling the rotation speed of the fan, and (d) means 89, 90 for detecting overload of the blowers 2, 3.
(E) Subtractors 33, 10 that subtract the input signal from the output of the wind speed setting means 1 and give it to the air blowing control means 7, 8, 29.
7, (f) a rate-of-change calculator 104 for calculating the time rate of change of the output of the wind speed setting means 1, (g) an overload limiting circuit 91, and (g1) the integrated output of the subtracters 33, 107. (G2) In response to the outputs of the overload detection means 89 and 90 and an integrator circuit 95 given as an input signal, when an overload is detected, a signal representing the time change rate is given to the integrator circuit 95 to detect the overload. The wind speed control device for a wind tunnel is characterized by including an overload limiting circuit 91 having means 75 and SW4 for giving a signal to the integrating circuit 95 when the output of the integrating circuit 95 is zero.

Further, the present invention relates to (a) a wind velocity control device for a wind tunnel that blows air from blowers 2 and 3 through a wind pipe onto an object to be tested, and (b) means 1 for setting the wind velocity of the blown air; c) In response to the output of the wind speed setting means 1, the blowers 2 and 3
Blower control means 7, 8, 29 for generating a signal Nsoll for controlling the rotation speed of the fan, and (d) means 89, 90 for detecting an overload of the blowers 2, 3.
(E) Subtractors 33 and 107 for subtracting an input signal from the rotation speed control signal Nsoll and giving them to the blowers 2 and 3, (f) Change rate calculation for calculating a time change rate of the rotation speed control signal Nsoll 104, (g) an overload limiting circuit 91, (g1) an integrating circuit 95 which gives an integrated output as an input signal to the subtracters 33 and 107, and (g2) an output of the overload detecting means 89 and 90. Responsive means for giving a signal representing the rate of change of time to the integrating circuit 95 when an overload is detected, and for giving a signal with which the output of the integrating circuit 95 becomes zero to the integrating circuit 95 when no overload is detected. And an overload limiting circuit 91 having SW4 and SW4.

Operation According to the present invention, when an overload of the motor driving the blower and the inverter is detected, the output of the wind speed setting means is changed so that the absolute value of the output of the overload control means changes with time. Change to increase. This prevents the blower from stopping due to overload of the motor.

This overload includes not only acceleration of the blower but also deceleration by regenerative braking.

Motors and inverters are generally designed to withstand overload operation for short periods of time. For example, some inverters can be overloaded for 2 minutes at a rated 125% overload, and other conventional inverters can be overloaded for 1 minute at a rated 150% overload. As described above, the overload operation is allowed. Therefore, the motor for driving the blower and the inverter for energizing the motor can be operated in their overload regions without tripping, and the facility cost can be reduced. Further, when the wind speed control device of the existing wind tunnel is already installed, the trip can be prevented to improve the efficiency of operation. That is, it is possible to reduce the loss of power cost and the loss of personnel cost caused by the trip.

In the present invention, the operation is continued under an overload, but the overload operation for a long time is prevented. The trip is to detect the occurrence of any abnormality and stop the operation of the equipment or device. In the present invention, even if an overload occurs, it does not trip immediately. When the overload occurs continuously for a certain period of time (for example, for 1 minute), this is detected, and the operation is stopped to protect the equipment and device.

Embodiment FIG. 1 is an overall block diagram of an embodiment of the present invention. In the low wind speed region, the blower 2 is used based on the wind speed set value Vsoll from the chassis dynamo 1 which is the wind speed setting means.
The motor 3 for driving the motor is rotationally controlled at a constant speed corresponding to the minimum wind speed setting value Cmin from the minimum wind speed setting circuit 4, and at this time, the damper 5 is controlled by the feedforward control circuit 6
Thus, the feedforward control is performed. In the high wind speed region, the feedback control for driving the blower 2 is performed by the proportional and integral (abbreviated as PI) control circuit 8 based on the measured wind speed value Vist from the means 7 for detecting the actual wind speed, and the actual wind speed is also performed. Is controlled by the feedforward control circuit 9 in order to improve the response speed of the wind speed set value Vsoll, which is the output from the chassis dynamo 1, and the actual wind speed. .

FIG. 2 is a diagram showing the overall configuration of the wind tunnel. The entire air duct is covered by the air duct 10, and the blower 2 is installed inside the air duct 10.
Is installed. The blower 2 is driven by the motor 3 as described above. The motor 3 may be directly connected to the blower 2 or may be configured to be driven via a belt hook or a gear train. An air conditioner 11 is provided downstream of the blower 2. The air conditioner 11 has a heat exchanger that guides hot water to exchange heat with the air in order to adjust the temperature of the air flow, and in some cases, for example, room temperature water is supplied instead of the hot water. A guide vane 12 is provided in the air duct 10. The measurement unit 13 that performs the measurement experiment includes an object to be tested,
For example, a vehicle 14 is placed and a nozzle 15 for forming an air flow is arranged in the front. The measurement unit 13 is provided with a heater 16 that produces road surface heat, a heater 17 that produces solar heat, and the like, and can form a thermal equilibrium state together with the air conditioner 11. A bell mouth 18 is provided downstream of the measuring unit 13, and the flow of air diffused by the measuring unit 13 is drawn into the air duct again. In addition to the open type in which the measuring unit 13 is open as shown in FIG. 2, the measuring unit 13 itself may be a closed type wind tunnel covered with a wind pipe. In the case of a closed type wind tunnel, instead of the nozzle 15, an airflow restrictor called a contraction portion, and a predetermined condition forming means for obtaining the local uniformity of the wind speed are provided and covered by the housing 19.

The air sucked into the bell mouth 18 is supplied to the blower 2 again. Such a wind tunnel is called a circulation type wind tunnel. In addition, the air discharged from the blower 2 may be in the form of a wind tunnel that is discharged to the atmosphere and is not supplied to the blower 2 again.

A main damper 5 is provided between the air conditioner 11 and the measuring unit 13, and a bypass duct 20 is provided in front of the main damper 5. The other end of the bypass duct 20 is connected to the wind pipe 10 on the downstream side of the measurement unit 13, and a bypass damper 21 is arranged near the inlet of the bypass duct 20. The main damper 5 and the bypass damper 21 are openable / closable, and the air passage cross-sectional areas of the main air passage air duct 10a and the bypass duct 20 can be adjusted respectively.
These dampers 5 and 21 are configured to be interlocked by a double-acting hydraulic cylinder 22 as shown in FIG.
The dampers 5, 21 are configured to operate in reverse so that the opening of one of them becomes smaller when the opening of the other becomes smaller. When the main damper 5 is closed, the bypass damper 21 is opened. , Or when the bypass damper 21 is closed, the main damper 5 is opened.

The bypass duct 20 is installed to improve the airflow performance at low wind speeds, particularly the performance of wind speed control.
The bypass duct 20 is also used to maintain a thermal equilibrium state. Depending on the purpose of the experiment in the measuring unit 13, these bypass duct 20 and damper 21
May be omitted.

The drive wheels of the vehicle 14, which is the object to be measured, provided in the measurement unit 13 drive the chassis dynamo 1 provided on the floor, whereby the speed corresponding to the wheels, that is, the output corresponding to the vehicle speed, It is derived as the aforementioned wind speed set value Vsoll. A Pitot tube 23 is provided to measure the wind speed in the measuring unit 13, and the temperature of the air supplied to the measuring unit 13 is detected by a thermometer 24. The outputs from the pitot tube 23 and the thermometer 24 are given to the wind speed calculation circuit 25, and the actual wind speed Vist is calculated based on the first equation in this way.

Here, kv is a constant, te is a temperature measured by the thermometer 24, and ΔP is a dynamic pressure detected by the pitot tube 23. Pitot tube 23, thermometer 24, and wind speed calculation circuit 2
5 constitutes the wind speed detection means 7.

A signal representing the actual wind speed Vist is derived from the wind speed calculation circuit 25 on the line 26, and the characteristic imparting circuit 5 is supplied from the subtraction circuit 27.
6 and line 28 to subtraction circuit 29.

The wind speed set value Vsoll from the chassis dynamo 1 is limited by the change rate limiting circuit 129 to an excessive change rate of the wind speed set value, and its output SV is given to the subtracter 31 from the line 30, and its output SV1 is further It is given to the subtractor 33 via the characteristic giving circuit 32, and its output SV0 is further given to the subtractor 29 from the line 34. The deviation ε between the signal from the line 34 and the signal from the line 28 is given to the PI control circuit 8 for feed back control, and its output MV goes from the line 36 to the addition circuit 37, and the addition output MV0 goes to the line 38. Derived. The signal MV0 on the line 38 is supplied to the adder circuit 39. Adder circuit 39
Is supplied with the output Cmin from the minimum rotation speed setting circuit 4 as described above, and the rotation speed setting value Nsoll thus obtained is supplied from the line 40 to the motor drive circuit 41.

The motor drive circuit 41, which is a means for controlling the rotation speed of the blower, includes a subtractor 42, a rotation speed control circuit 44, and a rotation speed detector 45 for detecting the rotation speed of the motor 3 so as to perform feed back control. Is composed of. Thus, the blower 2 is controlled by the rotation speed setting value Nsoll.

The signal SV0 from the line 34 is given to the feedforward control circuit 9, and its output FF is inputted to the adder 37, and thus the feedforward control of the blower 2 is performed according to the motor 3.

The signal SV from the line 30 is given to the feedforward control circuit 6 for the damper 5, the output SVd thereof is given to the function generating circuit 46, and a signal representing the opening degree θ of the damper 5 corresponding to the input SVd is given. It is led to the line 47 and given to the damper opening control circuit 48.

The damper opening control circuit 48 includes a subtractor 49, a servo controller 50, an electrohydraulic servo valve 51, and a detector 52 that detects the opening of the damper 5, and outputs the output of the electrohydraulic servo valve 51. Therefore, the hydraulic cylinder 22 is double-actuated, the damper 5 is controlled to an opening degree corresponding to the output θ of the function generating circuit 46, and the bypass damper 21 is also driven accordingly.

The function generating circuit 46 has a characteristic that the opening degree θ of the damper 5 increases as the output SVd of the feedforward control circuit 6 increases, and this characteristic is as shown in FIG. . Thus, the opening degree θ of the damper 5 is directly calculated based on the signal SVd. Therefore, as shown in FIG. 4 (1), as the signal SV corresponding to the speed of the vehicle 14 (that is, the vehicle speed) and, accordingly, the wind speed set value Vsoll increases, it is shown in FIG. 4 (1). As described above, the opening degree of the damper 5 increases, and when the vehicle speed is 40 km / h or more, the opening degree becomes 100%. The rotation speed of the motor 3 for driving the blower 2 is the speed of the vehicle 14, and thus the wind speed set value Vsol, as shown in FIG. 4 (2).
In the range of the signal SV corresponding to 1 from 0 to 35 km / h,
It is a value Cmin set by the minimum rotation speed setting circuit 4, and at a vehicle speed of 35 km / h or more, the rotation speed of the motor 3 increases in accordance with the increase of the signal SV. In the wind speed range of 35 to 40 km / h, both the damper 5 and the blower 2 are controlled, and a smooth change in the wind speed in the measurement unit 13 is achieved.

In order to control the blower 2, the signal SV on the line 30
Is given to the subtractor 31 as described above, and the subtractor 3
The output SVmin from the lower limit wind speed setting circuit 55 is given to 1. The signal SVmin output from the lower limit wind speed setting circuit 55 is the vehicle speed 3 described with reference to FIG.
It is a value corresponding to 5 km / h. The subtractor 31 calculates the output SV1 (= SV-SVmin) and supplies it to the characteristic imparting circuit 32. As shown in FIG. 5, the characteristic imparting circuit 32 derives an output that is zero when the output SV1 of the subtractor 31 is negative, and outputs the output SV1 when the output of the subtractor 31 is zero or more. Is derived with an amplification factor of 1 and given to the subtractor 33. In this way, the blower 2 has the wind speed SV.
Below min (= value corresponding to, for example, a vehicle speed of 35 km / h), the output of the characteristic imparting circuit 32 is zero, and it is controlled at a constant rotation speed of the rotation speed Cmin set by the minimum rotation speed setting circuit 4. become.

In this way, in the low wind speed range where the vehicle speed is 40 km / h or less,
The opening of the damper 5 is adjusted to adjust the wind speed in the measuring unit 13, which prevents malfunction due to difficulty in generally detecting the wind speed with low accuracy and high accuracy, and the low rotation speed range of the motor 3. The instability of the operation due to the low stability of the inverter included in the control circuit 44 that drives the motor 3 at low frequency is prevented. At a vehicle speed of 40 km / h or more, the damper 5 is fully opened, and the rotation speed of the motor 3 that drives the blower 2 is stably controlled.

The output of the lower limit wind speed setting circuit 55 is also given to the subtractor 27, and the output of this subtractor 27 is the above-mentioned characteristic giving circuit 32.
Is given to the characteristic imparting circuit 56 having the same configuration as described above, whereby the output derived from the characteristic imparting circuit 56 to the line 28 is zero when the wind speed is less than the lower limit value SVmin. The rotation speed control circuit 44 may have an inverter, but may be configured to control the rotation speed of the motor 3 by another configuration.

A power amplifier circuit and a servo motor may be used instead of the double-acting hydraulic cylinder 22 that drives the damper 5 and the electro-hydraulic servo valve 51, or may be realized by another configuration.

The signal representing the deviation ε derived from the subtractor 29 is given to the PI control circuit 8 from the line 35 as described above. The proportional gain Kp in the PI control circuit 8 is changed by the proportional gain changing circuit 57 according to the actual wind speed Vist, as shown in FIG. The integration time Ti of the PI control circuit 8 is also changed by the integration time changing circuit 58 according to the actual wind speed Vist, as shown in FIG. In this way, good wind speed control is realized in accordance with a large change in plant characteristics from the low wind speed region to the high wind speed region.

The PI control circuit 8 responds to the input signal of the deviation ε, and calculates the output MV thereof as in the second equation based on the outputs Kp and Ti of the circuits 57 and 58.

Here, Kp and Ti are shown by the third and fourth equations, respectively, and fi and fp are functions of the actual wind speed Vist.

Kp = p (Vist) (3) Ti = i (Vist) (4) By appropriately calculating the proportional gain Kp and the integral constant Ti in this manner, the control performance can be improved.

The feedforward control circuit 9 is provided to improve the followability of the wind speed control. That is, the wind speed set value V
A motor 3 for directly driving the blower 2 according to the soll
The delay and instability of the response peculiar to the feedback control means including the PI control circuit 8 can be eliminated by controlling the control of (1) to realize stable control with good followability. The specific structure of the feedforward control circuit 9 is shown in FIG. The feedforward control circuit 9 has two paths, one is a path through the first amplifier circuit 59 having a gain K _NFF , and its output U _FF1 is given to the adder 60. One is a path through which a differentiator 61 and an amplifier circuit 62 having a gain K _DFF are provided, and an output U _FF2 thereof is given to an adder 60. The output FF of the adder 60 is given to the adder 37, added to the output MV of the PI control circuit 8, and used as an output MV0 for commanding the rotation speed.

In the differentiator 61, when the signal SV0 from the line 34 is in the accelerating state as shown in FIG. 9 (1), the output ΔSV given to the amplifier circuit 62 has a level corresponding to the time change rate. Thus, the differentiator 61 functions to add energy when the blower 2 is accelerated or decelerated.

By providing the differentiation circuit 61 in the feedforward control circuit 9, the energy required for accelerating the air in the blower 2 and the wind pipe 10 is controlled at the same time as the wind speed set value Vsoll of the chassis dynamo 1 is increased. Since it can be reflected in the output and the blower 2 and the damper 5 can be quickly driven, the followability can be further improved.

By providing the amplifying circuit 62 after the differentiating circuit 61 and adjusting the gain K _DFF of the differentiating circuit 61, an acceleration state suitable for the equipment can be obtained.

The feedforward control circuit 6 for the damper 5 has the same configuration as the feedforward control circuit 9 described above.

As another embodiment of the present invention, the feedforward control circuit 6 for the damper may be omitted and the signal SV may be directly supplied to the function generating circuit 46.

FIG. 10 is a block diagram of a part of another embodiment of the present invention. As the feedforward control circuit 9, only the amplifier circuit 59 having the gain K _NFF as shown in FIG. 10 may be used. This gain K _NFF may be 1, or may be zero to deactivate its function,
Its value is variable.

FIG. 11 shows a part of still another embodiment of the present invention.
The feedforward control circuit 9 may include a differentiating circuit 61 and an amplifying circuit 62 having a gain K _DFF .

Furthermore, as shown in FIG. 12, in the feedforward control circuit 9, a filter 64 may be interposed between the differentiating circuit 61 and the amplifying circuit 62. This filter 64
Reduces the excessive rate of change of the rotation speed of the motor 3, performs stable wind speed control with good followability, reduces the mechanical load on the mechanical structure, and prevents failures.

FIG. 13 is a waveform diagram for explaining the operation of the feedforward circuit 9 shown in FIG. Differentiator circuit 6
When the step waveform shown in FIG. 13 (1) is input as the input x of 1, the differentiating circuit 61 derives the pulse shown in FIG. 13 (2) as the output y to the filter 64, and outputs it to this. Therefore, the filter 64 derives its filter output z with a waveform that relaxes the excessive change rate of y shown in FIG. 13 (3).

FIG. 14 is a waveform diagram for explaining another operation of the feedforward control circuit 9 shown in FIG. When a waveform as shown in FIG. 14 (1) is input to the differentiating circuit 61 as input x, the differentiating circuit 61 outputs y.
As a result, the pulsed waveform shown by the solid line in FIG. 14 (2) is derived. The filter 64 derives the waveform shown by the broken line in FIG. 14 (2) as the output z. In this way
The filter 64 functions to stabilize the rotation speed of the motor 3 as described above.

FIG. 15 shows a specific structure of the filter 64. The filter 64 is realized by an operational amplifier 65, resistors R1 to R3, and a capacitor C1, and its transfer function G is represented by the fifth equation when the time constant is T and the Laplace converter is s.

FIG. 16 is a block diagram showing another specific structure of the filter 64. The output y of the differentiating circuit 61 is given to the subtractor 67 from the line 66 and inputted to the limiter 68.
The limiter 68 has the input / output characteristics shown in FIG. 17, and derives a constant upper or lower limit output when the input level is excessive. The output of the limiter 68 is input to the integrating circuit 69. The transfer function G of the integrating circuit is as shown in the sixth equation.

The output z of the integrating circuit 69 is input to the subtractor 67 and is also given to the subsequent amplifying circuit 62 shown in FIG.

To execute the filter 64 by a computer program, when the input of the filter 64 is yi, the output of the filter 64 is zi, i is the number of samplings, and α is a constant representing the magnitude of delay. , The calculation shown in the seventh equation is performed.

z _i = (1−α) · y _i + α · z _i-1 (7) FIG. 18 is a block diagram showing a part of still another embodiment of the present invention. In this embodiment, the feedforward control circuit 9 includes a differentiating circuit 61, a limiter 71, and a gain K.
It is realized by the amplifier circuit 62 having _DFF . That is, the limiter 71 is used in place of the filter 64 of the embodiment shown in FIG. Limiter 71
Serves to limit the output of the differentiation circuit 61 when the output is excessive.

FIG. 19 shows a specific configuration of the change rate limiting circuit 129. This rate-of-change limiting circuit 129 is equivalent to the first rate-of-change limiting circuit 7
2 and a second change rate limiting circuit 73. The first change rate limiting circuit 72 uses the manual input means 74 to switch S.
W1, SW2 and SW3 are operated in conjunction with each other. The switching states of the switches SW1, SW2, SW3 shown in FIG. 19 are in normal operation, that is, when the wind speed is not set to zero. As a result, a signal from the setting circuit 75 for setting zero wind speed is derived, and the contact SW1b is cut off, the switch SW2 is cut off, the contact SW3a is made conductive, and the contact SW3b is cut off.

In the first change rate limiting circuit 72, the signal from the chassis dynamo 1 is given to the subtractor 76 via the contact SW1b, and the signal SVA is input to the second change rate limiting circuit 73 from the line 77a. The output on line 77a is also provided to contact SW3a. The signal from the wind speed setting circuit 75 is given to the subtraction circuit 77 from the contact SW3b. The output of the subtraction circuit 77 is input to the limiter 78. The output of the limiter 78 is limited when its input is excessive as shown in FIG. The output of the limiter 78 is input to the integrating circuit 79. The integrating circuit 79 has a time constant T _SV and a transfer function G shown by the eighth equation.

The output of the integrating circuit 79 is given to the subtracting circuit 76 and also to the subtracting circuit 77 via the switch SW2.

FIG. 21 shows the first rate-of-change limiting circuit 7 shown in FIG.
6 is a graph for explaining the second operation. Before time t1 in FIG. 21 (1), the contacts SW1a and SW are
When the signal SV of the line 77a outputs the wind speed of 0 km / h, the damper 5 is fully closed, and the blower 2 has the minimum rotation speed set value Cmin.
Are being driven in. At time t1, the manual input means 7
4 to operate switches SW1 and SW shown in FIG.
2, when the switching state of SW3 is reached, time t1 to
During the period of t2, the signal SVA changes so as to increase with the passage of time, and reaches the value of the output Vsoll of the chassis dynamo 1 at time t2. Thus output SV
Prevent A's sudden change.

As shown in FIG. 21 (2), the switch SW
When the switching state of SW1, SW2 and SW3 is the state shown in FIG. 19, the output of the line 77a is the value Vsoll of the chassis dynamo 1, and the manual input means 74 is operated at time t3 to switch SW1. , SW
2, SW3 changing the switching state, contact SW
When 1a and Sw3a are turned on, the signal SWA on the line 77a decreases with time from time t3 to t4 and becomes zero at time t4. In this way, the output SVA of the line 77 is prevented from changing suddenly. This prevents the output of the differentiating circuit 61 (see FIGS. 8, 11, 12, and 18 described above) included in the feedforward control circuit 9 from becoming excessively large. Also, it prevents sudden changes in wind speed and protects the machine.

The second change rate limiting circuit 73 derives its output SV according to the time change rate of the input signal SVA. Where Δ
When T (s) is the sampling period and j is the number of times of sampling, (a1) SVA _(j) -SV _(j-1) 6 km / h / s.ΔT ... (9), SV _(j) = SV _(j-1) + 6km / h / s · ΔT ... (10) (b1) SVA _{(j )} −SV _(j-1) −6km / h / s · ΔT …… (11), SV _{( j)} = SV _(j-1) -6 km / h / s · ΔT ... (12) (c1) When other than the above (a1) and (b1), SV _(j) = SVA _(j) (13) No. FIG. 22 is a block diagram showing a specific configuration of the second change rate limiting circuit 73. This second change rate limiting circuit 73
Has a differentiating circuit 81, a limiter 82, and an integrating circuit 83. The limiter 82 has the same configuration as the limiter 78 described above. When the input of the differentiating circuit 81 is x1 and the output thereof is y1, in the analog system, Further, in the digital system, when i is the number of samplings, the differentiating circuit 81 is y1 _i = x1 _i −x1 _i-1 (15) Further, as shown in FIG. And a resistor R5 and a capacitor C2, and may be configured to perform the operation represented by the sixteenth equation. Here, C11 is a constant.

The integrating circuit 83 sets its input as x2 and its output as y2.
Then, the operation of the 17th equation is performed.

y2 = ∫x2 · dt (17) In the digital system, when i is the number of samplings and ΔT is the sampling period, As shown in FIG. 24, the integrating circuit 83 may be realized by an operational amplifier circuit 85, a resistor R6, and a capacitor C3, and may be configured to perform the operation of Expression 19.

y2 = −C21 · ∫x2 · dt (19) Here, C21 in the nineteenth expression is a constant.

Referring to FIG. 25, the second change rate limiting circuit 73
When ΔSV is ΔSV = SVA _(j) -SV _(j-1) (20) when the signal shown in FIG. 1 is input, as shown in FIG. 25B for ΔSV. When the upper limit value is 6 km / h / s · ΔT or more and the equation 9 is satisfied, the output SV changes according to the equation 10 during the period from the time t5 to t5a, and becomes as shown in FIG. 25 (3). Further, since ΔSV is not more than the lower limit value −6 km / h / s · ΔT at the times t6 to t6a and t to t7a, the above-mentioned 11th
When the expression is satisfied, the SV gradually changes according to the twelfth expression.

Similarly, when the signal SVA is input to the second rate-of-change limiting circuit 73 as shown in FIG. 26 (1), its output SV becomes as shown in FIG. 26 (2). That is, when the signal SVA changes suddenly from time t8 to t8a,
From time t8 to t8b, the above-mentioned formula 9 is satisfied, and the output SV
Changes slowly. Similarly, from time t9 to t9a
When the signal SVA suddenly changes at, the above-mentioned formula 11 is satisfied from time t9 to t9b, and the output SV changes gently.

It should be noted that, as shown in FIG. 27, when the input SVA does not satisfy either of the expressions 9 and 11 as shown in FIG. 27 (1), that is, when the signal SVA changes gently, As shown in FIG. 27 (2), the output SV has the same waveform as the input SVA, and at this time, the above-mentioned expression 13 is established. In this way, the set value SV for the blower 2 is prevented from changing suddenly.

Since the rate-of-change limiting unit 29 is provided in front of the PI control circuit 8 and the feedforward control circuit 9 and the feedforward control circuit 6 for the feed back, the wind speed set value Vsoll from the chassis dynamo 1 is a noise. It is possible to prevent the control system from being disturbed due to the output of the subsequent differentiating circuit 61 or the like due to fluctuations caused by the resolution of the analog / digital conversion circuit.

Further, according to the present invention, the following configuration is adopted to prevent the inverter included in the motor 3 and the rotation speed control circuit 44 from stopping due to overload and tripping. With this configuration, the operation is continued under an overload, but the overload operation for a long time is prevented. The trip is to detect the occurrence of any abnormality and stop the operation of the equipment or device. In this embodiment, there is no immediate tripping when an overload occurs. When the overload occurs continuously for a certain period of time (for example, for 1 minute), this is detected, and the operation is stopped to protect the equipment and device. The purpose of this configuration is to prevent the operation from being stopped due to overload and to improve the efficiency of the experiment. Another objective is to reduce the equipment capacity and cost. That is, this configuration is intended to detect the occurrence of an overload and prevent the facility or device from staying in the overload region for a long time.

A line 88 to which electric power is supplied from the rotation speed control circuit 44 of the motor 3 is provided with a current transformer 89 for detecting its load current as shown in FIG. The output of the current transformer 89 is input to the comparison circuit 90 shown in FIG.
The comparison circuit 90 has a so-called hysteresis characteristic, as shown in FIG. This comparison circuit 90 derives a logic "1", that is, an output of ON when the load current becomes equal to or more than a predetermined overload value Ia (for example, 120% of the rated current), and then the load current is less than the rated current. Ib
When it becomes less than (for example, 90% of the rated current), a logic "0", that is, an output of OFF is derived. Comparison circuit 90
Is output to the overload limiting circuit 91 which is the overload control means.

The specific structure of the overload limiting circuit 91 is shown in FIG. In FIG. 30, the line 35 from which the signal representing the deviation ε is derived is the gain (that is, the multiplier) 99 from the line 100 via the contact SW4a of the switch SW4.
The signal representing the deviation ε is multiplied by a predetermined value and then input to the subtractor 93 from the line 92. The output of the subtractor 93 is given to the limiter 94 to limit its excessive input.
Given to 5. The integrating circuit 95 has a transfer function G represented by the twenty-first equation.

Here, T _LMT represents a time constant.

The output of the integration circuit 95 is supplied to the subtraction circuit 33 and the subtraction circuit 93. The output of the zero wind speed setting circuit 75 is given to the line 92 via the contact SW4b. The switch SW4 responds to the output of the comparison circuit 90, and when the output is a logic "1", the contact SW4a is turned on and the contact SW4b is turned off, and the comparison circuit 90 is turned on.
When the output of is the logic "0", the contact SW4a is set to the 30th
As shown in the figure, it is cut off and the contact SW4b is made conductive.

For example, when the output of the Chassis Dynamo 1 is accelerating,
When the output of the comparison circuit 90 becomes a logic "1" and is turned on, the deviation ε> 0, and therefore the output LMT of the integration circuit 95.
Is positive and the signal SV2 given through the characteristic giving circuit 32 is made small by the subtracting circuit 33, so that the wind speed set value from the chassis dynamo 1 is apparently limited to a small value. Become. In other words, since the sudden acceleration that causes overload is weakened and the signal SV0 on the line 34 is reduced, the inverter provided in the motor 3 and the rotation speed control circuit 44 that controls the motor 3 is removed from the overload region. To do.

Referring to FIGS. 30 and 31, as the deviation ε derived on the line 35 of the subtractor 29 changes, the positive output given from the integrating circuit 95 to the subtracting circuit 33 changes with time. The signal on line 92 and the integration circuit 95
From the subtraction circuit 93 to the signal applied to the subtraction circuit 93 via the line 96.
The signal given to the integrating circuit 95 via the limiter 94 via 7 becomes zero, and the output LMT of the integrating circuit 95 becomes the deviation ε.
Proportional to.

Therefore, as shown in FIG. 32, during the rapid acceleration, the time change rate of the signal SV0 from the subtraction circuit 33 is
The angle .theta.1 corresponding to the output LMT of the integrating circuit 95 is reduced by a value to weaken the sudden acceleration. Thus, as mentioned above, the motor 3 and the inverter are prevented from coming out of the overload region and tripping them.

It is detected by the current transformer 89 that the load current of the motor 3 has decreased, and the load current has a value Ib (see FIG. 29).
When the value becomes less than the value, the output of the comparison circuit 90 becomes the logic "0", so that the switching state of the switch SW4 is the third.
Switching from the state shown in FIG. 0, a signal indicating that the wind speed is zero is given from the wind speed zero setting circuit 75. As a result, the output of the integrating circuit 95 decreases with the passage of time, and the output of the integrating circuit 95 becomes zero. As a result, the overload limiting circuit 9
1 has no influence on the PI control circuit 8 and the feedforward control circuit 9 for the blower 2.

FIG. 33 shows the next embodiment. That is, the output of the means for calculating the rate of change of the wind speed setting means may be used for the input of the overload limiting circuit, in addition to the deviation. The means for calculating the rate of change of the wind speed setting means includes a rate of change calculator 104 and a gain 105.
Have. The output SV derived from the line 101 is input to the change rate calculator 104. The calculation formula of the rate-of-change calculator 104 is represented by Formula 22 with J as the number of times of sampling.

DSV = SV _(J) -SV _(J-1) (22) where DSV is the output of the change rate calculator.

The output of the rate-of-change calculator 104 is amplified by the gain 105 via the line 102 and is input to the overload limiting circuit as DSV1 via the line 103 in the same manner as the deviation.
The description after the DSV1 is input to the overload limiting circuit is the same as the description of the embodiment when the deviation is input.

Further, as shown in FIG. 34, the input Nsoll of the means for calculating the change rate of the means for controlling the rotation speed of the blower may be used as the input of the overload limiting circuit.

The difference between the means for calculating the rate of change of the wind speed setting means and the means for calculating the rate of change of the means for controlling the rotation speed of the blower is that the input of the means for calculating the rate of change of the wind speed setting means is the wind speed set value. The input of the means for calculating the rate of change of the means for controlling the rotation speed of the blower is to use the input of the means for controlling the rotation speed of the blower.

The next embodiment is shown in FIG. That is, the output of the overload limiting circuit may be subtracted from the input of the unit that controls the rotation speed of the blower, instead of being subtracted from the output of the wind speed setting unit. The output LMT of the overload limiting circuit is line 10
6 is subtracted via a subtractor 107 from the input Nsoll which is derived from line 40. Output Nso of subtractor
11 is input to the means for controlling the rotation speed of the blower via the line 108.

FIG. 36 shows a configuration in which the input of the overload control means is the output of the means for calculating the change rate of the output of the wind speed setting means, and the output of the overload control means is subtracted from the output of the wind speed setting means. .

In FIG. 37, the input of the overload control means is the output of the means for calculating the change rate of the output of the wind speed setting means, and the output of the overload control means is subtracted from the input of the means for controlling the rotation speed of the blower. The configuration in the case is shown.

In FIG. 38, the input of the overload control means is the output of the means for calculating the change rate of the means for controlling the rotation speed of the blower, and the output of the overload control means is subtracted from the output of the wind speed setting means. The configuration is shown.

FIG. 39 is an output of the means for calculating the rate of change of the means for controlling the rotation speed of the blower when the input of the overload control means is
The structure when the output of the overload control means is subtracted from the input of the means for controlling the rotation speed of the blower is shown.

Such an overload limiting circuit 91 is used for the chassis dynamo 1
Rapidly decelerates, which causes the motor 3 to operate again when performing regenerative braking.

The invention can be implemented in connection with circular and single-flow wind tunnels, and also with respect to wind tunnels that do not have dampers 5,21. The servo system may be configured not only by a motor type and an electric type but also by a pneumatic type.
The rotation speed control may be controlled not only by the inverter but also by other configurations.

In the above embodiment, the current transformer 89 is taken as an example of the overload detecting means, but the electric energy supplied to the motor may be used instead. The amount of electric power can be detected by a known means. Further, a torque meter may be attached to the motor shaft, and this torque meter may be used as the overload detecting means. Further, an electronic thermal circuit including a motor drive circuit and a bimetal may be provided to detect overload.

As another embodiment of the present invention, a vane opening control device may be provided instead of the rotation speed control device using an inverter device or the like.

Generally, the wind speed can be adjusted even if the rotation speed of the blower is changed, but the inverter device is expensive. The electric motor that drives the blower is rotated at a constant speed synchronized with the power supply frequency, and a vane that adjusts the circuit cross-sectional area is installed at the inlet (upstream) or outlet (downflow) of the blower, and the vane opening is adjusted to change the wind speed. You can also In the case of the wind tunnel equipment having such a configuration, the present invention can be implemented by placing a device for controlling the opening of the vane instead of the rotation speed control device.

As described above, according to the present invention, the overload of the blower is detected, and when the overload is detected, the absolute value of the overload limiting circuit is changed so as to increase with the passage of time. It is possible to prevent the tripping of the driving motor and the inverter for energizing the motor from stopping due to overload. Therefore, the facility cost can be reduced and the operation efficiency can be improved.

[Brief description of drawings]

FIG. 1 is an overall block diagram of one embodiment of the present invention, FIG. 2 is a system diagram of a wind tunnel of one embodiment of the present invention, and FIG. 3 is a function generator 46 having a characteristic for compensating the nonlinear characteristic of a damper. 5 is a graph showing the characteristics of the characteristic applying circuits 32 and 56, FIG. 4 is a graph showing the control characteristics of the damper 5 and the motor 3, and FIG. 6 is a graph showing the characteristics of the gain changing circuit. 7 is a graph showing the characteristic of the integration time changing circuit 58, FIG. 8 is a block diagram showing the configuration of the feed forward circuit 9, and FIG. 9 is a graph showing the characteristic of the feed forward circuit 9. FIG. 10 is a block diagram showing another configuration of the feedforward control circuit 9, FIG. 11 is a block diagram showing another configuration of the feedforward control circuit 9, and FIG. 12 is a feedforward control circuit. Block showing another configuration of 9. , Figure 13 and Figure 14 is a 12
Waveform diagram showing characteristics of the filter 64 shown in FIG.
FIG. 16 is a graph showing a specific structure of the filter 64, 16th
The figure is a block diagram showing another specific configuration of the filter 64,
17 is a graph showing the characteristics of the limiter 68, FIG. 18 is a block diagram showing another configuration of the feedforward control circuit 9, and FIG. 19 is a block diagram showing a concrete configuration of the change rate limiting means 29. 20 shows the first change rate limiting circuit 72.
21 is a graph for explaining the operation of the limiter 78, FIG. 21 is a waveform diagram for explaining the operation of the first change rate limiting circuit 72, and FIG. 2 is a block diagram showing a concrete structure of the change rate limiting circuit 73, FIG. 23 is an electric circuit diagram showing a concrete structure of the differentiating circuit 81, and FIG. 24 is an electric circuit showing a concrete structure of the integrating circuit 83. 25, 26, and 27 are waveform diagrams for explaining the operation of the second rate-of-change limiting circuit 73, and FIG. 28 is an electrical diagram showing the configuration of a current transformer 89 for overload detection. 29 is a circuit diagram, FIG. 29 is a diagram for explaining the operation of the comparison circuit 90, FIG. 30 is a block diagram showing a specific configuration of the overload limiting circuit 91, and FIGS. 31 and 32 are overload limiting circuits. FIG. 33 is a diagram for explaining the operation of 91,
FIGS. 34, 35 are block diagrams showing another embodiment having an overload limiting circuit, and FIGS. 36, 37, 38 and 39 show another embodiment having an overload limiting circuit. It is a block diagram which shows the structure of an example. 1 ... Shashi dynamo, 2 ... Blower, 3 ... Motor, 5,21 ... Damper, 6,9 ... Feed forward control circuit, 7 ... Wind speed detecting means, 8 ... PI control circuit, 10 ... Wind pipe, 13 ... Measuring part, 14 ... Object to be tested, 129 ... Change rate limiting circuit, 89 ... Current transformer, 90 ...
… Comparison circuit, 91 …… Overload limiting circuit

Claims (4)

[Claims] 1. A wind speed control device for a wind tunnel, in which (a) air from blowers 2 and 3 is blown to an object to be tested through a wind tube, (b) means 1 for setting the wind speed of the blown air, c) In response to the output of the wind speed setting means 1, the blowers 2 and 3
Fan control means 7, 8 and 29 for generating a signal ε for controlling the rotation speed of the fan, and (d) means 89 and 90 for detecting overload of the fans 2 and 3.
(E) Subtractors 33, 107 for subtracting the input signal from the rotation speed control signal ε and giving the blowers 2, 3; (f) Overload limiting circuit 91, (f1) Subtracting the integrated output (F2) In response to the outputs of the overload detection means 89, 90 in response to the outputs of the overload detection means 89, 90, when the overload is detected, the rotation speed control means ε is applied to the integration circuit 95, A wind tunnel wind speed control device comprising: an overload limiting circuit 91 having means 75 and SW4 for giving a signal to the integrating circuit 95 to make the output of the integrating circuit 95 zero when no overload is detected. . 2. The blower control means 7, 8 and 29 are means 7 for detecting the wind speed of the blown air, and the rotation speed control signal representing the deviation between the output of the wind speed setting means 1 and the output of the wind speed detecting means 7. Generates ε and blowers 2 and 3
The negative feed back control means 8 and 29 for controlling the rotational speeds of the blowers 2 and 3 so that the deviation becomes zero.
The wind speed control device for a wind tunnel according to claim 1, characterized in that: 3. A wind speed control device for a wind tunnel, wherein: (a) air from blowers 2 and 3 is blown to an object to be tested through a wind pipe; (b) means 1 for setting the wind speed of the blown air; c) In response to the output of the wind speed setting means 1, the blowers 2 and 3
Blower control means 7, 8, 29 for controlling the rotation speed of the fan, and (d) means 89, 90 for detecting overload of the blowers 2, 3.
(E) Subtractors 33, 10 that subtract the input signal from the output of the wind speed setting means 1 and give it to the air blowing control means 7, 8, 29.
7, (f) a rate-of-change calculator 104 for calculating the time rate of change of the output of the wind speed setting means 1, (g) an overload limiting circuit 91, and (g1) the integrated output of the subtracters 33, 107. (G2) In response to the outputs of the overload detection means 89 and 90 and an integrator circuit 95 given as an input signal, when an overload is detected, a signal representing the time change rate is given to the integrator circuit 95 to detect the overload. The wind speed control device for a wind tunnel, comprising: an overload limiting circuit 91 having means 75 and SW4 for giving a signal to the integrating circuit 95 when the output of the integrating circuit 95 is zero. 4. A wind speed control device for a wind tunnel, in which (a) air from blowers 2 and 3 is blown to an object to be tested through a wind pipe, (b) means 1 for setting the wind speed of the blown air, c) In response to the output of the wind speed setting means 1, the blowers 2 and 3
Blower control means 7, 8, 29 for generating a signal Nsoll for controlling the rotation speed of the fan, and (d) means 89, 90 for detecting an overload of the blowers 2, 3.
(E) Subtractors 33 and 107 for subtracting an input signal from the rotation speed control signal Nsoll and giving them to the blowers 2 and 3, (f) Change rate calculation for calculating a time change rate of the rotation speed control signal Nsoll 104, (g) an overload limiting circuit 91, (g1) an integrating circuit 95 which gives an integrated output as an input signal to the subtracters 33 and 107, and (g2) an output of the overload detecting means 89 and 90. Responsive means for giving a signal representing the rate of change of time to the integrating circuit 95 when an overload is detected, and for giving a signal with which the output of the integrating circuit 95 becomes zero to the integrating circuit 95 when no overload is detected. And an overload limiting circuit 91 having SW4 and SW4.