PWR-82520-300W

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PWR-82520  
3-PHASE DC MOTOR TORQUE  
CONTROLLER  
DESCRIPTION  
FEATURES  
The PWR-82520 is a high-perfor-  
mance current-regulating torque loop  
controller. It is designed to accurate-  
ly regulate the current in the windings  
of 3-phase brushless DC and brush  
DC motors.  
PWR-82520 can be tuned by using  
100V Rating for 28V Motors  
an external Proportional-Integral (PI)  
regulator network in conjunction with  
the internal error amplifier.  
10 Amp Continuous Output Current  
Complementary Four-Quadrant  
Operation  
APPLICATIONS  
3% Linearity Accuracy  
Packaged in a small DIP-style hybrid,  
the PWR-82520 are ideal for applica-  
tions with limited printed circuit board  
area.  
The PWR-82520 is a completely self-  
contained motor controller that con-  
verts the analog input command sig-  
nal into motor current and uses the  
signals from Hall-effect sensors in the  
motor to commutate the current in the  
motor windings. The motor current is  
internally sensed and processed into  
an analog signal. This signal is  
summed together with the command  
signal to produce an error signal that  
controls the pulse width modulation  
(PWM) duty cycle of the output, thus  
controlling the motor current. The  
5% Current Regulating Accuracy  
User-Programmable Compensation  
10 kHz - 50 kHz PWM Frequency  
The PWR-82520 is ideal for applica-  
tion requiring current regulation  
and/or holding torque at zero input  
Operates as Current or Voltage  
Controller  
Self-Contained 3-Phase Motor  
Controller  
command.  
System applications  
include flight surface control on air-  
craft for horizontal stabilizers and  
flaps, missile fin control, fuel and  
hydraulic pumps, radar and counter-  
measures systems.  
Built-in Current Limit  
5.0V  
10K 10K 10K  
39  
HA  
HALL A  
38  
HB  
COMMUTATION  
HALL B  
LOGIC  
37  
HC  
HALL C  
40  
+15V HALL SUPPLY OUTPUT  
41  
+15V  
SUPPLY GND  
HALL  
33  
VBUS+  
4,5,6  
COMMAND OUT  
10K  
DRIVE  
A
10K  
10K  
31  
30  
PHASE  
A
+
-
COMMAND IN  
COMMAND IN  
-
100  
PHASE  
A
14,15,16  
+
COMMAND  
BUFFER  
10K  
29  
17  
COMMAND GND  
CASE GND  
5.0V  
10K  
DRIVE  
B
PWM  
LOGIC  
CIRCUITRY  
PHASE  
PHASE  
B
CASE  
PHASE  
7,8,9  
B
36  
28  
27  
ENABLE  
+15V SUPPLY  
GROUND  
VDD  
VEE  
+
+
26  
19  
DRIVE  
C
-15V SUPPLY  
PWM IN  
C
PHASE  
1,2,3  
C
20  
22  
PWM OUT  
SYNC IN  
100  
21  
32  
34  
PWM GND  
ERROR AMP OUT  
IS+  
10  
ERROR AMP IN  
-
100  
Rsense  
CURRENT  
AMP  
+
ERROR  
AMPLIFIER  
VBUS–  
11,12,13  
CURRENT  
MONITOR OUT  
90.9  
35  
-
+
FIGURE 1. PWR-82520 BLOCK DIAGRAM  
1994, 1999 Data Device Corporation  
©
TABLE 1. ABSOLUTE MAXIMUM RATINGS (TC = +25°C UNLESS OTHERWISE SPECIFIED)  
PARAMETER  
Bus Voltage  
SYMBOL  
VBUS+  
VDD  
VALUE  
100  
UNITS  
VDC  
VDC  
VDC  
A
+15V Supply  
+17.5  
-17.5  
10  
VEE  
-15V Supply  
Continuous Output Current  
Peak Output Current  
Command input +  
Command input -  
I
OC  
I
15  
A
PEAK  
Command input+  
Command input-  
±15  
VDC  
VDC  
±15  
ENABLE  
HA, HB, HC  
Logic inputs  
Sync Input  
7.0  
VDC  
VDC  
SYNC  
±15.0  
TABLE 2. PWR-82520 SPECIFICATIONS  
(Unless otherwise specified, VBUS = 28 VDC, VDD = +15V, VEE = -15V, TC = 25°C)  
VALUE  
PARAMETERS  
SYMBOL  
TEST CONDITIONS  
UNITS  
MIN  
TYP  
MAX  
OUTPUT  
Output Current Continuous  
Output Current Pulsed  
Current Limit  
IOC (note 1)  
IOP  
ICL  
IOFFSET  
RON(note 2, 3)  
RON(note 2, 3)  
10  
14  
15.4  
+0.3  
0.040  
0.055  
A
A
A
12.0  
-0.3  
14.0  
-
Current Offset  
VDF = 0V  
+25°C  
+85°C  
A
Output On-Resistance  
Output On-Resistance  
Output Conductor Resistance  
Load Inductance  
µH  
R
LMIN  
+85°C  
note 3  
C
100  
COMMAND IN+/-  
Differential Input  
VDIF  
-10  
+10  
VDC  
VDC  
COMMAND OUT  
Internal Voltage Clamp  
VCLMP  
-11.5  
+11.5  
CURRENT COMMAND  
Transconductance ratio  
Non-Linearity  
G
0.95  
-3.0  
1.0  
1.05  
+3.0  
A/V  
%
See FIGURE 9  
CURRENT MONITOR AMP  
Current Monitor Gain  
Current Monitor Offset  
Output Current  
0.97  
-0.1  
-10  
1.0  
0
1.03  
0.1  
10  
V/A  
VDC  
mA  
VDF = 0V  
Output Resistance  
ROUT  
100  
VBUS+ SUPPLY  
Nominal Operating Voltage  
VNOM  
+18  
+28  
+70  
VDC  
VDC  
VBUS- To PWM GND  
Voltage differential  
VGNDDIF  
0.250  
+15 VDC  
Voltage  
Current  
VS +  
I +  
+14.25  
-15.75  
+15.0  
100  
+15.75  
150  
VDC  
mA  
-15 VDC  
Voltage  
Current  
VS -  
I -  
-15.0  
80  
-14.25  
150  
VDC  
mA  
SYNC (Note 2)  
Voltage  
Pulse Width  
Sync range as % of free-run  
frequency  
±7.5  
130  
0
V
ns  
%
See FIGURE 7  
+20  
Note:  
1) IOC is average current as measured in motor winding  
2) Guaranteed by design, not tested.  
3) The maximum output conductor resistance and on-resistance of FETs at +85°C are:  
ΦAU = 0.20Ω, ΦAL = 0.16Ω, ΦBU = 0.08Ω, ΦBL = 0.08Ω, ΦCU = 0.08Ω, ΦCL = 0.20Ω  
2
TABLE 2. PWR-82520 SPECIFICATIONS (CONTINUED)  
(Unless otherwise specified, VBUS = 28 VDC, VDD = +15V, VEE = -15V, TC = 25°C)  
VALUE  
PARAMETERS  
PWM IN  
SYMBOL  
TEST CONDITIONS  
UNITS  
MIN  
TYP  
MAX  
+Peak  
-Peak  
Frequency  
Non -linearity  
Duty Cycle  
VP+  
VP-  
f
9.8  
-10.2  
10  
-2  
49  
10.0  
-10.0  
10.2  
-9.8  
60  
+2  
51  
V
V
KHz  
%
LIN  
D CYCLE  
50  
50  
%
PWM OUT  
Free Run Frequency  
45  
55  
50  
KHz  
mA  
HALL POWER SUPPLY  
Max Current Draw  
IMDRW  
HALL SIGNALS  
Logic 1  
Logic 0  
HA, HB,  
HC  
3.5  
0.7  
VDC  
VDC  
ENABLE INPUT  
Enabled  
ENABLE  
0.7  
Disabled  
3.5  
VDC  
ISOLATION  
CASE to PIN  
500 VDC HIPOT  
10  
MΩ  
SWITCHING CHARACTERISTICS  
Upper drive  
125  
200  
ns  
ns  
Turn-on Rise Time  
Turn-off Fall Time  
Lower drive  
Turn-on Rise Time  
Turn-off Fall Time  
Diode Forward Voltage Drop  
tr  
tf  
Ip = 4 A  
ID = 1A  
200  
200  
1.25  
ns  
ns  
V
tr  
tf  
VF  
PROPAGATION DELAY  
Ip = 4A  
Td (on)  
Td (off)  
From 0.7V on ENABLE  
to 10% of VOUT  
From 3.5V on ENABLE  
to 90% of VOUT  
40  
20  
µs  
µs  
THERMAL  
Thermal Resistance  
Junction - Case  
Case - Air  
Junction Temperature  
Case Operating Temperature  
Case Storage Temperature  
6
10  
+175  
+125  
+150  
°C/W  
°C/W  
°C  
°C  
°C  
θJ-C  
θC-A  
TJ  
TC  
TCS  
-55  
-65  
WEIGHT  
1.7(48)  
oz(gr)  
over the operating temperature range and the total error due to  
all the factors such as offset, initial component accuracies etc. is  
maintained well below 5% of the rated output current.  
INTRODUCTION  
The PWR-82520 is high performance current control (torque  
loop) hybrid which use complementary four quadrant switching  
topology (See BASIC OPERATION) to provide linearity through  
zero current. The high Pulse Width Modulation (PWM) switching  
frequency makes it suitable for even low inductance motors. The  
PWR-82520 hybrid can accept single-ended or differential mode  
command signals. The current gain can be easily programmed  
to match the end user system requirements. With the compen-  
sation network externally wired, the hybrid can provide optimum  
control of a wide range of loads.  
The Hall sensor interface for current commutation has built-in  
decoder logic that separates illegal codes and ensures that there  
is no cross conduction. The hybrid also has a +15V supply out-  
put for powering the Hall sensors. The Hall sensor inputs are  
internally pulled up to +5V and they can be driven from open-col-  
lector outputs.  
The PWM frequency can be programmed externally by adding a  
capacitor from PWM OUT to PWM GND. In addition, multiple  
PWR-82520s can be synchronized by using one device as a  
master and connecting its PWM OUT pin to the PWM IN of all  
the other slave devices in a system or by applying a SYNC pulse  
to pin 22.  
The PWR-82520 uses unique current sense technology and a  
non-inductive hybrid sense resistor which yields a highly linear  
current output over the wide military temperature range (see  
FIGURE 9). The output current non-linearity is better than 3%  
3
The ENABLE input signal provides quick start and shutdown of  
the output power switches. In addition, built-in power sequence  
fault protection turns off the output in case of low power supply  
voltages.  
VBUS  
The hybrid features dual current limiting functions. The input  
command amplifier output is limited to 10.8V thus limiting the  
current under normal operation. In addition, there is a built in  
over current limit which trips at 14 Amps, protecting the hybrid as  
well as the load.  
PHASE A  
UPPER  
PHASE B  
UPPER  
ON  
OFF  
I
PHASE A  
PHASE B  
-
+
BASIC OPERATION  
PHASE C  
PHASE A  
LOWER  
PHASE B  
LOWER  
The PW-82520 utilizes a complimentary four-quadrant drive  
technique to control current in the load. The complimentary  
drive has the following advantages over the standard drive:  
OFF  
ON  
1. Maximum holding torque and position accuracy  
2. Linear current control through zero  
3. No deadband at zero  
Rsense  
The complementary drive design uses a 50% PWM duty cycle  
for a zero command signal. For a zero input command, a pair of  
MOSFETs are turned on in the drive, Phase A upper & Phase B  
lower as shown in FIGURE 2A, to supply current into the load for  
the first half of the PWM cycle. This is the same mode of oper-  
ation for the standard four-quadrant drive as shown in FIGURE  
3A/B. During the second half of the PWM cycle, a second pair  
of transistors are turned on, Phase A lower & Phase B upper as  
shown in FIGURE 2B, for the flyback current and to provide load  
current in the opposite direction.  
FIGURE 2A. COMPLEMENTARY FOUR-QUANDRANT  
DRIVE FIRST HALF OF PWM CYCLE  
This is normally the dead time for standard four-quadrant drive  
as shown in FIGURE 3B. The result is current flowing in both  
directions in the motor for each PWM cycle. The advantage this  
has over standard four-quadrant drive is that at 50% duty cycle,  
which corresponds to zero average current in the motor, holding  
torque is provided. The motor current at 50% duty cycle is sim-  
ply the magnetizing current of the motor winding.  
VBUS  
Using the complimentary four-quadrant technique allows the  
motor direction to be defined by the duty cycle. Relative to a  
given switch pair i.e., Phase A upper and Phase B lower, a duty  
cycle greater than 50% will result in a clockwise rotation where-  
as a duty cycle less than 50% will result in a counter clockwise  
rotation. Therefore, with the use of average current mode con-  
trol, direction can be controlled without the use of a direction bit  
and the current can be controlled through zero in a very precise  
and linear fashion.  
PHASE A  
UPPER  
PHASE B  
UPPER  
OFF  
ON  
I
PHASE A  
PHASE B  
+
_
PHASE C  
PHASE A  
LOWER  
PHASE B  
LOWER  
ON  
OFF  
The PW-82520 contains all the circuitry required to close an  
average current mode control loop around a complimentary four-  
quadrant drive. The PWR-82520 use of average current mode  
control simplifies the control loop by eliminating the need for  
slope compensation and eliminating the pole created by the  
motor inductance. These two effects are normally associated  
with 50% duty cycle limitations when implementing standard  
peak current mode control.  
Rsense  
FIGURE 2B. COMPLEMENTARY FOUR-QUADRANT DRIVE  
SECOND HALF OF PWM CYCLE  
4
FUNCTIONAL AND PIN DESCRIPTIONS:  
V
BUS  
COMMAND IN+, COMMAND IN- (Pins 30 & 31)  
The command amplifier has a differential input that operates  
from a ±10 V analog current command. The differential input  
voltage may vary between ±10 VDC, maximum, corresponding  
to ±maximum voltage or current for the output. Either input  
(COMMAND IN + or COMMAND IN-) may be referenced to the  
command ground (Pin 29) and the other input varied from ±10  
VDC to obtain full output. The COMMAND OUT signal is inter-  
nally limited to approximately ±11.5 VDC; that is, inputs above or  
below ±11.5 VDC will be clamped to ±11.5 VDC. The input  
impedance of the Command Amplifier is 10K Ohms.  
PHASE A  
UPPER  
PHASE B  
UPPER  
ON  
OFF  
I
PHASE A  
PHASE B  
-
+
PHASE C  
The PWR-82520 can be used either as a current or voltage  
mode controller. When the PWR-82520 is used as a torque  
amplifier (current mode) as shown in FIGURE 13, the transfer  
function of the command amplifier is 1.0 A/V. The input com-  
mand signal is processed through the command buffer. The out-  
put of the buffer (COMMAND OUT) is summed with the current  
monitor output into the error amplifier. When external compen-  
sation is used on the error amp, as shown in FIGURE 6A, the  
response time can be adjusted to meet the application.  
PHASE A  
LOWER  
PHASE B  
LOWER  
OFF  
ON  
Rsense  
When used in the voltage mode the Voltage Command uses the  
same differential input terminals to control the voltage applied to  
the motor (see FIGURE 12). The error amp directly varies the  
PWM duty cycle of the voltage applied to the motor phase. The  
transfer function in the voltage mode is 4.7% /V ±5% variation of  
the PWM duty cycle vs. input command. The duty cycle range of  
the output voltage is limited to approximately 5-95% in both cur-  
rent and voltage modes.  
FIGURE 3A. STANDARD FOUR QUANDRANT DRIVE FIRST  
HALF OF PWM CYCLE  
TRANSCONDUCTANCE RATIO AND OFFSET  
VBUS  
When the PWR-82520 is used in the Current Mode, the com-  
mand inputs (COMMAND IN+ and COMMAND IN-) are designed  
such that ±10 VDC on either input, with the other input connect-  
ed to Ground, will result in ±10 DC Average Amperes of current  
into the load. The DC current transfer ratio accuracy is ±5% of  
the rated output current. The initial output DC current offset with  
both COMMAND IN+ and COMMAND IN- tied to the Ground will  
be less than 100 mA when measured using a load of 0.5 mH and  
1.0 Ohms at room ambient with standard current loop compen-  
sation (see FIGURE 6A). The winding phase current error shall  
be within the cumulative limits of the transconductance ratio  
error and the offset error.  
PHASE A  
UPPER  
PHASE B  
UPPER  
OFF  
OFF  
PHASE A  
PHASE B  
+
_
I
Flyback  
PHASE C  
PHASE A  
LOWER  
PHASE B  
LOWER  
HALL A,B,C SIGNALS (Pins 37, 38 and 39)  
OFF  
OFF  
These are logic signals from the motor Rotor Position Sensors  
(HA, HB, HC). They use a phasing convention referred to as 120  
degree spacing; that is, the output of HA is in phase with motor  
back EMF voltage VAB, HB is in phase VBC, and HC is in phase  
with VCA. Logic 1(or HIGH) is defined by an input greater than  
3.5 VDC or an open circuit to the controller; Logic 0(or LOW)  
is defined as any Hall voltage input less than 0.7 VDC. Internal  
to the PWR-82520 are 5K pull-up resistors tied to +5 VDC on  
each Hall input.  
Rsense  
The PWR-82520 will operate with Hall phasing of 60° or 120°  
electrical spacing. If 60° commutation is used, then the output of  
FIGURE 3B. STANDARD 4 QUANDRANT DRIVE SECOND  
HALF OF PWM CYCLE  
5
HC must be inverted as shown in FIGURES 4 and 5. In FIGURE 4,  
the Hall sensor outputs are shown with the corresponding volt-  
age they are in phase with.  
HALL-EFFECT SENSOR PHASING vs.  
MOTOR BACK EMF FOR CW ROTATION (120° Commutations)  
300°  
60°  
180°  
300°  
360°/0°  
0°  
120°  
240°  
60°  
VAB  
VBC  
VCA  
BACK EMF  
OF MOTOR  
ROTATING  
CW  
Hall Input Signal Conditioning: When the motor is located  
more than two feet away from the PWR-82520 controller the Hall  
inputs require filtering from noise. It is recommended to use a  
1 kresistor in series with the Hall signal and a 2000 pF capac-  
itor from the Hall input pin to the Hall supply ground pin as shown  
in FIGURE 12 and 13.  
CW  
COMPENSATION  
In Phase  
with VAB  
The PI regulator in the PWR-82520 can be tuned to a specific  
load for optimum performance. FIGURE 6A shows the standard  
current loop configuration and tuning components, and FIGURE  
6B shows the frequency response for the PI regulator. By adjust-  
ing R1, R2 and C1, the amplifier can be tuned. The value of R1,  
C1 will vary, depending on the loop bandwidth requirement.  
HA  
In Phase  
with VBC  
HB  
HC  
In Phase  
with VCA  
In Phase  
with VAC  
(60˚)  
HC  
EXTERNAL PI REGULATOR  
FIGURE 4. HALL PHASING  
10.0 K  
R1  
4700 pF  
C1  
1 MEG  
R7  
HA  
120°  
120°  
ERROR  
AMP INPUT  
32  
N
S
470 pf  
34  
ERROR  
AMP OUT  
-
R2B  
R2A  
O
10.0 K  
10.0 K  
+
HC  
HB  
COMMAND  
OUT  
33  
35  
CURRENT  
MONITOR OUT  
REMOTE POSITION SENSOR (HALL) SPACING FOR  
120 DEGREE COMMUTATION  
FIGURE 6A. STANDARD PI CURRENT LOOP  
60°  
200  
120°  
HA  
100  
HC  
A, dB  
S
N
0
60°  
-100  
HC  
HB  
180  
θ, degree  
REMOTE POSITION SENSOR (HALL) SPACING FOR  
60 DEGREE COMMUTATION  
90  
0
1.0KHz  
10KHz  
FREQUENCY  
100Hz  
100MHz  
10Hz  
100KHz  
1.0MHz  
10MHz  
FIGURE 5. HALL SENSOR SPACING  
FIGURE 6B. PI REGULATOR FREQUENCY RESPONSE  
6
(
)
ENABLE Pin 36  
SYNC PERIOD  
This is a logic input to the controller that enables or disables the  
controller. In the disabled state, no voltage shall be applied to the  
motor phases. The disabled state occurs when the Enable input  
is greater than 3.5 VDC or is left open; to enable the controller,  
this input must be pulled to less than 0.7 VDC. The Enable input  
has a 10K pull-up resistor tied to +5 VDC.  
+7.5V  
-7.5V  
VBUS+ (Pins 4, 5 and 6)  
130ns  
The VBUS+ supply is the power source for the motor phases and  
is nominally +28 VDC. The normal operating voltage may actu-  
ally vary from +18 to +48 VDC with respect to Vbus-. The power  
stage MOSFETS in the hybrid have an absolute maximum  
VBUS+ Supply voltage rating of 100V. The recommended oper-  
ating voltage must not exceed +70 VDC, and is subject to the  
safe operating curve within FIGURE 10. The user must supply  
sufficient external capacitance or circuitry to prevent the bus  
supply from exceeding +70 VDC at the hybrid power terminals  
under any conditions.  
FIGURE 7. SYNC INPUT SIGNAL  
PWM FREQUENCY  
The PWM frequency from the PWM OUT pin will free-run at a  
frequency of 50 kHz ±10 kHz. The user can adjust this frequen-  
cy down to 10 kHz through the addition of an external capacitor.  
The PWM triangle wave generated internally is brought out to  
the PWM OUT pin. This output, or an external triangle waveform  
generated by the user, may be connected to PWM IN on the  
hybrid.  
The VBUS should be applied at least 50 ms after ±15 VDC to  
allow the internal analog circuitry to stabilize. If this is not possi-  
ble, the hybrid must be powered up in the disabledmode.  
VBUS- (Pins 11, 12, and 13)  
WARNING: Never apply power to the hybrid without connect-  
ing either PWM OUT or an external triangular wave to PWM IN!  
Failure to do so may result in one or more outputs latching on.  
This is the high current ground return for VBUS+. This point  
must be externally connected to Ground for proper operation of  
the current loop. The voltage difference between Vbus- and the  
Ground connections must be less than 0.250 VDC including  
transients.  
PWM OUT (Pin 20)  
This is the output of the internally generated PWM triangle wave  
form. It is normally connected to PWM In. The frequency of this  
output may be lowered by connecting an NPO capacitor (Cext)  
between PWM OUT and PWM GND. The typical PWM frequen-  
cy is determined by the following formula:  
GROUNDS  
SUPPLY GND (Pin 27): This is the return line for the ±15 VDC  
supplies. The phase current sensing technique of the  
PWR-82520 requires that VBUS- and Supply Ground be con-  
nected together externally (see VBUS- supply).  
16.5E-6  
PWM GND (Pin 21): This is used for the return side of the exter-  
nal PWM capacitor (Cext) when switching frequencies below  
50 KHz are required.  
330 pF + CEXT pF  
COMMAND GND (Pin 29): This is used when the command  
buffer is used single-ended and the COMMAND IN- or COM-  
MAND IN+ are tied to COMMAND GND.  
CASE (Pin 17)  
This pin is internally connected to the hybrid case. In some appli-  
cations the user may want to tie Pin 17 to Ground for EMI con-  
siderations.  
HALL GND (Pin 41): This is used for the return of the +15V HALL  
supply and should be tied to SUPPLY GROUND.  
PHASES A, B, C (Pin A 14-16, B 7-9, C 1-3)  
±15 VDC (+15V Supply, Pin 28 / -15V Supply, Pin 26)  
These inputs are used to power the small signal analog and dig-  
ital circuitry of the hybrid. An internal +5 VDC supply is derived  
from the +15 VDC source. These inputs should not vary more  
than ±5%, maximum. The absolute maximum voltage ratings of  
these inputs are ±17.5 VDC. Reversal of the power supplies  
will result in destruction of the hybrid.  
These are the power drive outputs to the motor and switch  
between VBUS+ Input and VBUS- Input or become high imped-  
ance - see TABLE 3.  
+15 VDC HALL SUPPLY OUTPUT (Pin 40)  
SYNC IN (Pin 22)  
This output provides power to the Hall Sensors in the motor.  
Maximum current drawn from this supply by the user must not  
exceed 50 mA.  
The Sync pulse, as shown in FIGURE 7, can be used to syn-  
chronize the switching frequency up to 20% faster than the free  
running frequency of all th slave devices.  
7
TABLE 3. COMMUTATION TRUTH TABLE  
6
5
INPUTS  
OUTPUTS  
VBUS+  
+28V  
4
PHASE A PHASE B PHASE C  
ENABLE DIR ** HA  
HB  
0
HC  
0
16  
15  
14  
9
PHASE  
A
PHASE  
A
B
C
CW  
CW  
1
1
0
0
0
1
1
0
0
0
1
1
L
L
L
L
L
L
L
L
L
L
L
L
H
H
H
Z
L
L
Z
H
H
Z
L
Z
L
1
0
8
PHASE  
PHASE  
7
CW  
1
1
0
L
3
PHASE  
C
2
CW  
1
Z
H
H
L
1
13  
12  
11  
CW  
0
1
L
VBUS-  
GND  
CW  
0
1
Z
Z
H
H
Z
L
39  
38  
37  
41  
40  
HALL A  
HALL B  
HALL C  
+5V  
+5V  
CCW  
CCW  
CCW  
CCW  
CCW  
CCW  
0
1
H
Z
L
0
1
L
1
1
Z
H
H
Z
Z
HALL SUPPLY GND  
1
0
L
+15V HALL SUPPLY OUT  
1
0
Z
H
Z
0
0
L
Z
FIGURE 8. BRUSH MOTOR HOOK UP  
OUTPUT CURRENT  
1=Logic Voltage >3.5 VDC, 0=Logic voltage < 0.7 VDC  
** DIR is based on the convention shown in Figure 4. Actual  
motor set up might be different.  
Output current derating as a function of the hybrid case temper-  
ature is provided in FIGURE 10. The hybrid contains internal  
pulse by pulse current limit circuitry to limit the output current dur-  
ing fault conditions.(See TABLE 2) Current Limit accuracy is  
+10/-15%.  
CURRENT MONITOR OUT (Pin 35)  
This is a bipolar analog output voltage representative of motor  
current. The Current Monitor Output will have the same scaling  
as the Current Command input, 1.0 V/A. The output resistance  
will be less than 100 .  
WARNING: The PWR-82520 does not have short circuit pro-  
tection. The PWR-82520 must see a minimum of 100uH  
inductive load or enough line-to-line resistance to limit the  
output current to <10A at all times. Operation into a short or  
a condition that requires excessive output current will damage  
the hybrid.  
BRUSH MOTOR OPERATION  
The PWR-82520 can also be used as a brush motor controller  
for current or voltage control in an H-Bridge configuration. The  
PWR-82520 would be connected as shown in FIGURE 8. All  
other connections are as shown in either FIGURE 12 or 13  
depending on current or voltage mode operation. The Hall inputs  
are wired per TABLE 4. A positive input command will result in  
positive current to the motor out of Phase A.  
THERMAL OPERATION  
It is recommended the PWR-82520 be mounted to a heat sink.  
This heat sink shall have the capacity to dissipate heat generat-  
ed by the hybrid at all levels of current output, up to the peak  
limit, while maintaining the case temperature limit as per FIG-  
URE 10.  
10  
TABLE 4. HALL INPUTS FOR H-BRIDGE CONTROLLER  
INPUT  
OUTPUT  
5
Accuracy = ± 5% (of  
rated output)  
Current  
COMMAND  
IN  
ENABLE  
HA  
HB  
HC PH A PH B PH C  
0
(Amps)  
L
L
Positive  
Negative  
1
1
1
1
1
1
0
0
0
H
L
Z
Z
Z
L
H
Z
-5  
H
Z
-10  
-10  
-8  
-6  
-4  
-2  
0
2
4
6
8
10  
Input Command (Volt), Inductive Load  
FIGURE 9. LINEARITY CURVE  
8
11  
10  
9
8
28V,  
Cont. Cur.  
7
6
42V,  
Cont. Cur.  
5
4
70V,  
3
Cont. Cur.  
2
1
0
-60  
-40  
-20  
0
20  
40  
60  
80  
100  
120  
140  
Case Temperature (°C)  
FIGURE 10. MOTOR CURRENT DRIVE  
2. Switching Losses (Ps)  
PWR-82520 POWER DISSIPATION (SEE FIGURE 11)  
Ps = [ Vcc ( IOA (ts1) + IOB (ts2) ) fo] / 2  
Ps = [ 28 V ( 3 A (125 ns) + 7 A (200 ns) ) 50 kHz] / 2  
Ps = 1.24 Watts  
There are two major contributors to power dissipation in the  
motor driver: conduction losses and switching losses.  
VBUS = +28 V (Bus Voltage)  
IoA = 3 A, IOB = 7 A (see FIGURE 11)  
ton = 36 µs, T = 40 µs (period) (see FIGURE 11)  
Ron = 0.055 (on-resistance, see TABLE 2)  
Rc = 0.133 (conductor resistance, see TABLE 2,)  
ts1 = 125 ns, ts2 = 200 ns (see FIGURE 11)  
fo = 50 kHz (switching frequency)  
TRANSISTOR POWER DISSIPATION ( PQ  
PQ = PT + Ps  
)
PQ = 1.30 + 1.24 = 2.54 Watts  
OUTPUT CONDUCTOR DISSIPATION  
2
PC = (Imotor rms) x (Rc)  
2
PC = (4.87) x (0.133)  
PC = 3.15 Watts  
1. Transistor Conduction Losses (PC)  
2
TRANSISTOR POWER DISSIPATION FOR CONTINUOUS  
COMMUTATION  
PT = (Imotor rms) x (Ron)  
(IOB - IOA)2  
ton  
PQC = PQ (0.33)  
Imotor rms =  
(IOBIOA +  
)( )  
3
T
PQC = (2.54) X (0.33)  
PQC = 0.84 Watts  
(7 - 3)2  
3
36  
40  
Imotor rms =  
(7 * 3 +  
)(  
)
TOTAL HYBRID POWER DISSIPATION  
PTOTAL = (PQ + PC) x 2  
2
PT = (4.87) x (0.055)  
PTOTAL = (2.54 +3.15) x 2  
PTOTAL = 11.38 Watts  
PT = 1.30 Watts  
t
on  
VBUS  
IOB  
I
OA  
IO  
ts1  
ts2  
FIGURE 11. OUTPUT CHARACTERISTICS  
9
6
5
OPTIONAL  
VBUS+  
+28V  
17  
19  
20  
21  
26  
27  
28  
29  
30  
31  
32  
33  
34  
35  
36  
CASE GND  
PWM IN  
4
16  
15  
14  
9
PHASE  
A
B
PWR-82520  
PHASE  
A
B
C
PWM OUT  
Cext  
-15V  
GND  
+15V  
PWM GND  
PHASE  
PHASE  
8
PHASE  
PHASE  
7
+
+
-15V SUPPLY  
SUPPLY GND  
+15V SUPPLY  
COMMAND GND  
3
C
2
1
13  
12  
11  
MOTOR BLDC  
VBUS-  
GND  
-
+
COMMAND IN  
COMMAND IN  
-
-
R4  
1K  
COMMAND  
SIGNAL  
HALL A  
39  
38  
37  
+
HALL A  
HALL B  
HALL C  
+
R3  
1K  
HALL B  
HALL C  
ERROR AMP OUT  
COMMAND OUT  
R1  
R2  
1K  
470 pF  
-
R5  
10K  
+
ERROR AMP INPUT  
CURRENT  
MONITOR  
OUT  
C4  
2000pF  
C3  
2000pF  
C5  
2000pF  
10K  
CURRENT MONITOR OUT  
ENABLE  
HALL SUPPLY GND  
41  
40  
HALL SUPPLY GND  
ENABLE  
+15V HALL SUPPLY OUTPUT  
+15V HALL SUPPLY OUT  
FIGURE 12. VOLTAGE CONTROL HOOK-UP  
6
OPTIONAL  
5
VBUS+  
+28V  
17  
19  
20  
21  
26  
27  
28  
29  
30  
31  
32  
33  
34  
35  
36  
CASE GND  
4
16  
15  
14  
9
PWM IN  
PHASE  
A
B
PWR-82520  
PHASE  
PHASE  
PHASE  
A
B
C
PWM OUT  
Cext  
-15V  
PWM GND  
PHASE  
8
7
-15V SUPPLY  
SUPPLY GND  
+15V SUPPLY  
COMMAND GND  
+
+
3
PHASE  
C
GND  
+15V  
2
1
13  
12  
11  
MOTOR BLDC  
VBUS-  
GND  
-
+
COMMAND IN  
COMMAND IN  
-
-
R4  
1K  
HALL A  
HALL B  
HALL C  
39  
38  
37  
+
HALL A  
HALL B  
HALL C  
COMMAND  
SIGNAL  
+
R3  
1K  
ERROR AMP OUT  
COMMAND OUT  
R2A  
R2  
1K  
C1  
4700pF  
470 pF  
R1  
-
+
10K  
R2B  
ERROR AMP INPUT  
10K  
C4  
2000pF  
C3  
2000pF  
C5  
2000pF  
CURRENT MONITOR OUT  
ENABLE  
HALL SUPPLY GND  
+15V HALL SUPPLY OUTPUT  
41  
40  
R7 1MEG  
10K  
HALL SUPPLY GND  
+15V HALL SUPPLY OUT  
ENABLE  
FIGURE 13. TORQUE CONTROL HOOK-UP  
10  
TABLE 5. PIN ASSIGNMENTS  
FUNCTION FUNCTION  
PIN  
1
PIN  
41  
40  
39  
38  
37  
36  
35  
34  
33  
32  
31  
30  
29  
28  
27  
26  
25  
24  
23  
22  
21  
20  
19  
18  
17  
PHASE C  
PHASE C  
PHASE C  
VBUS +  
VBUS +  
VBUS +  
PHASE B  
PHASE B  
PHASE B  
IS+  
HALL SUPPLY GND  
+15V HALL SUPPLY OUTPUT  
HA  
2
29.21  
3
4
HB  
5
HC  
6
ENABLE  
7
CURRENT MONITOR OUTPUT  
ERROR AMP INPUT  
COMMAND OUT  
ERROR AMP OUT  
COMMAND IN +  
COMMAND IN -  
COMMAND GND  
+15V SUPPLY  
SUPPLY GND  
-15V SUPPLY  
N/C  
8
9
10  
11  
12  
13  
14  
15  
16  
VBUS -  
VBUS -  
VBUS -  
PHASE A  
PHASE A  
PHASE A  
N/C  
N/C  
SYNC  
PWM GND  
PWM OUT  
PWM IN  
FIGURE 14. MECHANICAL OUTLINE  
N/C  
CASE GND  
Note:  
1. N/C pins have internal connections for factory test purposes.  
11  
ORDERING INFORMATION  
PWR-82520-XX0X  
Supplemental Process Requirements:  
S = Pre-Cap Source Inspection  
L = Pull Test  
Q = Pull Test and Pre-Cap Inspection  
K = One Lot Date Code  
W = One Lot Date Code and PreCap Source  
Y = One Lot Date Code and 100% Pull Test  
Z = One Lot Date Code, PreCap Source and 100% Pull Test  
Blank = None of the Above  
Process Requirements:  
0 = Standard DDC Processing, no Burn-In (See table below.)  
1 = MIL-PRF-38534 Compliant  
2 = B*  
3 = MIL-PRF-38534 Compliant with PIND Testing  
4 = MIL-PRF-38534 Compliant with Solder Dip  
5 = MIL-PRF-38534 Compliant with PIND Testing and Solder Dip  
6 = B* with PIND Testing  
7 = B* with Solder Dip  
8 = B* with PIND Testing and Solder Dip  
9 = Standard DDC Processing with Solder Dip, no Burn-In (See table below.)  
Temperature Grade/Data Requirements:  
1 = -55°C to +125°C  
2 = -40°C to +85°C  
3 = 0°C to +70°C  
4 = -55°C to +125°C with Variables Test Data  
5 = -40°C to +85°C with Variables Test Data  
8 = 0°C to +70°C with Variables Test Data  
*Standard DDC Processing with burn-in and full temperature test see table below.  
STANDARD DDC PROCESSING  
MIL-STD-883  
TEST  
METHOD(S)  
CONDITION(S)  
INSPECTION  
SEAL  
2009, 2010, 2017, and 2032  
1014  
1010  
2001  
A and C  
TEMPERATURE CYCLE  
CONSTANT ACCELERATION  
BURN-IN  
C
A
1015, Table 1  
The information in this data sheet is believed to be accurate; however, no responsibility is  
assumed by Data Device Corporation for its use, and no license or rights are  
granted by implication or otherwise in connection therewith.  
Specifications are subject to change without notice.  
105 Wilbur Place, Bohemia, New York 11716-2482  
For Technical Support - 1-800-DDC-5757 ext. 7420  
Headquarters - Tel: (631) 567-5600 ext. 7420, Fax: (631) 567-7358  
Southeast - Tel: (703) 450-7900, Fax: (703) 450-6610  
West Coast - Tel: (714) 895-9777, Fax: (714) 895-4988  
Europe - Tel: +44-(0)1635-811140, Fax: +44-(0)1635-32264  
Asia/Pacific - Tel: +81-(0)3-3814-7688, Fax: +81-(0)3-3814-7689  
World Wide Web - http://www.ddc-web.com  
PRINTED IN THE U.S.A.  
C-12/99-1M  
12  

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