ENCYCLOPEDIA OF RADIO ELECTRONICS AND ELECTRICAL ENGINEERING Current source to compensate for self-discharge of the battery. Encyclopedia of radio electronics and electrical engineering Encyclopedia of radio electronics and electrical engineering / Chargers, batteries, galvanic cells Since the self-discharge of chemical current sources is an inevitable matter, attention has always been paid to its compensation in amateur radio literature. The scheme of the automatic set-top box, which, after a simple refinement of any existing charger, can be used for this purpose, is given in [1]. There is a second option - the use for this purpose of a low-power current source (IT), permanently connected to the battery during its long-term storage. Such devices were even produced by the industry. As a base (Fig. 1) in the first version (Fig. 2) IT, a circuit of a recharger of the type UP-N12-0,05-UHL3.1 was used, which in December 1992 was released by Zakarpatmash Production Association in the city of Zakarpatmash. Uzhgorod. Since during the experiments with the circuit there was only an operating manual, in addition to the parameters given in it for the power consumption (5,5 W in short circuit mode) of IT in short circuit mode (short circuit), and the value of the short circuit current of 250 mA, other design data on the device was not. Based on these data, an approximate calculation of the power transformer was carried out. The value of the input voltage was determined: 5,5 W / 0,25 A \u22d 24 V. Of the transformers available at hand, the step-down transformer (PT) for a 25-volt 2.940.005-watt soldering iron from an electric soldering kit 3TU, produced by the Vinnitsa plant, turned out to be the most suitable " Lighthouse", the diagram of which is shown in Fig. 24. This transformer provides voltages of 28 and 25 V on two regular sockets of the SGZ type, has a fairly low "idle" current (100 mA). The problem of electrical safety is also structurally solved: the primary and secondary windings are located in separate sections of the frame. The resistance of the primary winding is approximately XNUMX ohms. The device (Fig. 1) is an IT with high internal resistance, made on a powerful transistor VT1. The constancy of the output current parameters is ensured by supplying a stabilized voltage from the reference voltage source (ION) to the VT1 base, and therefore its output current is practically independent of the load in the collector circuit. With simple circuitry, IT has good temperature stability [2]. High parameters are obtained due to the use of an LED as an ION, which acts as a stabistor. As a result of mutual compensation of the positive temperature coefficient h21э(+2 mV / deg) of a bipolar transistor and a negative temperature coefficient of voltage drop change from LED temperature, it was possible to obtain the stability of the charge current parameters from temperature, which is essential for a long period of operation of the device. A certain disadvantage of the schemes in Fig. 1 and Fig. 2 is the possibility of erroneous connection of the battery to the IT in the opposite polarity, with all the ensuing consequences. In [3], this shortcoming is eliminated, but the IT scheme is somewhat complicated. A simpler circuit solution compared to [3] is used in the second version of the IT circuit shown in Fig.4. Unlike the circuits in Fig. 1 and Fig. 2, instead of the resistor R2, a transistor switch is used here, controlled by the voltage from the battery being charged, similarly [1]. Due to the fact that the LED indication should unambiguously determine the state of the device at the moment, more attention is paid to the circuit in Fig. 4 compared to [3]. A two-color LED indicator has been introduced into the circuit, which clearly indicates one or another polarity of the battery connection to the IT. The introduction of a transistor switch makes it possible to completely eliminate the discharge of the battery through the IT with an inverse connection, as well as to eliminate the short circuit mode, since when XS1 and XS2 are closed, the control voltage in the required polarity is not supplied to the VT2 base, it is closed, and the possible battery discharge circuit is interrupted. The polarity indicator for connecting the battery to the IT consists of two LEDs: VD5 type AJ1307A and VD6 type AL307V red and green, respectively. His work is clear. Schematically, the LEDs in the indicator, in addition to signaling, perform the function of self-protection: a diode that glows protects against the effects of reverse voltage (Uobr.max = 4 V); C. Instead of two LEDs of a different glow color, you can use a two-color LED. The value of the battery discharge current through the LED indicator when the 1,6 V mains voltage is off is determined by resistor R1,8. For this design, it is equal to 220mA. Variants of possible states of LED indicators are given in the table. To reduce useless losses in the 220 V mains connection indication circuits, the VD8 diode is connected to the FET winding with an alternating voltage of 4 V (T1, Fig. 3). Diode VD8 is also protected from reverse voltage using a silicon diode VD7 connected in the opposite direction. There was no data on the used radiator in [4]. In the first version of the real design, a powerful silicon transistor KT803 was used, which, as follows from the reference book [5], dissipates power without a heatsink of 5 W. Since the most difficult mode for VT1 (Fig. 2) is the short circuit mode (as possible), it was in this mode (200 mA) that the operation of the circuit was tested. Power dissipated in this mode on the regulating transistor: Р=240,2=4,8 (W). During the experiments, the transistor VT1 heated up significantly, so it was installed on an additional radiator (plate) made of duralumin with dimensions of 46x85x1,5 mm. The plate itself was mounted on the top cover of the PT housing on three threaded posts 12 mm high. The physical meaning of a larger short-circuit current than the self-discharge compensation current (TCS) during IT operation on a battery (as a chemical current source), in a certain simplification, can be represented as the subtraction of the battery voltage from the supply voltage at constant internal resistances of IT, battery and other conditions. After finalizing the circuit in Fig. 2 with a transistor switch (Fig. 4), the thermal regime of VT1 improved significantly (P = 24 V0,06A = 1,44 W), however, the design of the plate radiator with VT1 installed on it was left for reasons of maintaining the mounting volume. The elements of the rectifier and IT are mounted between the plate and the upper plane of the PT case by a hinged method. Four holes with a diameter of 5 mm are drilled in the plate, in which the LEDs are installed. The LEDs and the plate are mutually fixed with a molecular adhesive. Connecting IT to the battery is carried out using the SSH5 connector and a flexible two-wire line with clamps of the appropriate design. As XS1 and XS2 (Fig. 2 and Fig. 4), free sockets XS2.4 and XS2.5 PT (Fig. 3) were used, in which additional petals were installed. As a result of this refinement, the PT has fully retained its original functions. Details. It is desirable to use silicon transistors in IT for a power of 20 W and more, preferably in a metal case, with a voltage of 1) eq of at least 50 V. Resistor R1 type MLT1, R2 MLT-0,5. Transformer T1 (Fig. 3) can be made independently, for example, on a magnetic circuit Ш16x24 (S = 3,84 cm2) from the ULF output transformer of a tube color TV. Transformer steel, from which its magnetic circuit was made, has low watt losses at a frequency of 50 Hz, which is important for T1 with the expected long-term operation. The calculation of the number of turns T1 was carried out according to the recommendations [6] according to the formula 50/S (taking into account the use of high-quality magnetic cores, the empirical number is reduced to 50). From where N \u50d 2 / S (cm50) \u3,84d 13 / 220 \u13d 2870 (turns / V). Number of turns of the primary winding 13x24=1,2, secondary 370x13x 4=1,2 + 63x20x0,8=XNUMX (the number of turns of the secondary winding is increased by XNUMX%). Winding wire diameter is calculated by the formula: d=XNUMX(l)0,5. For the primary winding, for reasons of reducing the active resistance, a diameter of 0,15 mm was adopted. For example, for the secondary winding at a short circuit current of 0,2 A d=0,8(0,2)0,5=0,36 (mm). The "idling" current of two manufactured transformers, calculated according to the above formulas and assembled on the mentioned magnetic circuits, was about 5 mA. Setting up the scheme (Fig. 2). Disconnect the VD2 LED (Fig. 2) from the transistor and connect it directly to the rectifier bridge. Connect to the open circuit VD2 (point A) an avometer, connected by an ammeter. Instead of resistor R2, a 4,7 kΩ potentiometer is connected, turned on by a rheostat and set to maximum resistance. By changing the resistance of the potentiometer, set the current through VD2 10 mA. Connect VD2 to the transistor. Instead of the emitter resistor R1, a wire-wound potentiometer 47 ... 100 ohms is installed, turned on by a rheostat and set to maximum resistance. Connect to XS1 and XS2 an avometer, turned on by an ammeter to the maximum measurement limit. By changing the resistance of the potentiometer, the short circuit current is set to 200 mA. The TCR value of the battery, recommended [3], with the connected (preliminarily charged) battery should be 45 mA. Note Due to the shunting of the E-B transition of the transistor VT1 ION, the VD2 LED (Fig. 1 and Fig. 2) without load (in the absence of a battery connection or a short circuit in the output) should not light. Setting up the scheme (Fig. 4). Connect a charged battery with a voltage of 14,5 V to the IT output. Replace the resistor R4 with a 470 kΩ potentiometer, turned on by the rheostat and set to maximum resistance. Set the potentiometer current through the milliammeter 10 mA. Setting the output current of the IT fig. 4 is similar to setting the output current of the IT fig. 2, but should only be carried out with the battery connected in the appropriate polarity. The value of the output current IT fig. 4 should be equal to the sum of the TCS of the battery plus the current passing through the battery connection indicator, i.e. 45+15=60 (mA). References:
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