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“PROPOSED PHILIPPINE NATIONAL STANDARDS FOR RENEWABLE ENERGY TECHNOLOGIES” SOLAR PV SYSTEM COMPONENTS BATTERY CHARGE CONTROLLERS GENERAL SAFETY AND PERFORMANCE REQUIREMENTS DESIGN QUALIFICATION AND TEST APPROVAL JUNE 2006 GENERAL SAFETY AND PERFORMANCE REQUIREMENTS INTRODUCTION This proposed standard covers general safety, performance and test requirements for battery charge controllers (BCC) used in photovoltaic systems. Note: Safety requirements ensure that electrical equipment constructed in accordance with these standards does not endanger the safety of person or property when properly installed, maintained, and used in applications for which it was intended. SECTION ONE - GENERAL REQUIREMENTS 1. SCOPE This standard specifies general, safety, performance and test requirements for battery charge controllers in photovoltaic systems specifically those with rated voltage ratings of 12 and 24 V DC. 2. DEFINITIONS 2.1. Charging current: Amount of D.C. current being delivered by the PV generator to the battery 2.2. Rated voltage: D.C. voltage over which the charge controller is intended to be operated 2.3. Hysteresis: The range of voltages in between the switching thresholds within which switching does not take place. 2.4. Low Voltage Disconnect (LVD): The threshold battery voltage which, when attained, triggers the disconnection of the load from the battery to protect it from deep discharge cycles. 2.5. Low Voltage Reconnect (LVR): The threshold battery voltage which, when attained, triggers the reconnection of the load to the battery. 2.6. PV array: A mechanically integrated assembly of PV modules or panels with a support structure, tracking and thermal controls, and other components, required to form a direct-current power-producing unit. 2.7. PV array High Voltage Disconnect (HVD): The threshold battery voltage which, when attained, triggers the disconnection of the battery from the PV generator to protect it from overcharging and excessive gassing. 2.8. High Voltage Reconnect (HVR): The threshold battery voltage which, when attained, triggers the reconnection of the battery to the PV generator. 2.9. Stand-by current consumption: The current consumption of the controller at no load condition. Also referred to as ‘parasitic load’, it is the current consumed by the controller internal circuits with no power component activated. -1- 2.10. Rated Solar Current: The maximum current from the PV array that the controller can safely handle 2.11. Rated Load Current: The maximum load current the controller can safely handle. 3. GENERAL COMPLIANCE REQUIREMENTS Battery charge controllers should be designed and constructed such that in normal use they do not cause danger to the users and surroundings. In general, compliance for battery charge controllers may be checked by carrying out all the tests specified and described in Section 2 (Standard Test Methods) of Battery Charge Controller for Photovoltaic Applications-Design Qualification and Type Approval. 4. MARKINGS 4.1. Battery charge controllers should be clearly marked with the following mandatory markings: a. b. c. d. e. f. g. h. i. j. Name, monogram or symbol of manufacturer Model number or type reference of the manufacturer Date and place of manufacture Serial number Rated voltage Maximum PV array current Maximum load current Terminals identification Low Voltage Disconnect (LVD) and High Voltage Disconnect (HVD) Type and current rating of fuse 4.2. Markings should be durable and legible. The steps for checking compliance are specified in Design Qualification and Type Approval – Section One – General Requirements – Item 4 – Markings. 5. INDICATORS 5.1. As a minimum, light emitting diodes (LED) should be present in the front panel of the charge regulator to indicate voltage conditions of the battery. A red LED indicator may be used to indicate a fully discharged battery and a green LED indicator for a fully charged battery. 5.2. Other indicators such as but not limited to analog gauges and liquid crystal display (LCD) may be used in addition to LED indicators. -2- SECTION TWO - SAFETY REQUIREMENTS 6. TERMINALS 6.1 Terminals should permit the connection of conductors from each component and should adapt to the amperage requirement of the PV system. 6.2 Terminals should be prominently marked for polarities for each component in the PV system. 7. CONSTRUCTIONAL REQUIREMENTS 7.1 The battery charge controller should be mechanically robust and should be designed such that it minimizes the effects of moisture and temperature during use and prevents the ingress of insects, dust and water spray. 7.2 Adequately robust means of fixing should also be ensured. 8. BATTERY CHARGE CONTROLLER ENCLOSURE The enclosure of the battery charge controller should provide sufficient protection to the controller circuitry from the ingress of water spray, dust and small insects. 9. MOISTURE RESISTANCE AND INSULATION 9.1 The Battery charge controller should be moisture resistant. It should not show any appreciable damage after being subjected to the insulation test described below. Before the insulation test, visible drops of water, if any, are removed with a blotting paper. Immediately after the moisture treatment, the insulation resistance is measured 1 min after the application of a D.C. voltage higher than the rated voltage. The insulation resistance should not be less than 2 Mohm. 9.2 Insulation should be adequate between the input terminals bonded together and all exposed metal parts. 10. POLARITY REVERSAL To check if the battery charge controller is proof against supply voltage polarity reversals, operate it with reverse voltage for about 5 minutes at the maximum voltage range. At the end of this period, the supply is reconnected correctly and the battery charge controller should operate normally. -3- 11. SHORT CIRCUIT The battery charge controller should be adequately protected from short circuit conditions that may arise from PV array and load. 12. OVER-VOLTAGE The battery charge controller should be protected from lightning flashes and inductive over voltage if applicable. 13. CONNECTION SEQUENCE The battery charge controller should be protected from connection sequence reversals and should be tested according to the procedure described in the Battery Charge Controller for Photovoltaic Applications - Design Qualification and Type Approval – Section 2 – Test Methods. At the end of this test, the correct sequence of connection of each component to the battery charge controller is re-connected; and the battery charge controller should operate normally. SECTION THREE - PERFORMANCE REQUIREMENTS 14. ELECTRICAL CHARACTERISTICS Electrical characteristics of the battery charge controller should be faithful to the manufacturer's data and should be tested according to the test procedures described in Section 2 of the Battery Charge Controller for Photovoltaic Applications - Design Qualification and Type Approval. The battery charge controller should be tested for the following: a. b. c. d. e. f. g. Load low voltage disconnect (LVD) Load low voltage reconnect (LVR) PV array high voltage disconnect (HVD) PV array high voltage reconnect (HVR) Stand-by current consumption PV solar current Load current 15. ENVIRONMENTAL CHARACTERISTICS The battery charge controller should be subjected to environmental and electrical cycling tests described below to determine potential failures. The sample is tested for the voltage hysteresis at conditions described in Section 2 of the Battery Charge Controller for Photovoltaic Applications - Design Qualification and Type Approval. At the end of these tests, the battery charge controller should operate normally. -4- DESIGN QUALIFICATION AND TYPE-APPROVAL INTRODUCTION This standard covers the requirements for the design qualification and type approval of battery charge controllers used in photovoltaic systems. SECTION ONE - GENERAL REQUIREMENTS 1. SCOPE This section lays down the requirements for the design qualification and type approval of battery charge controllers used in photovoltaic systems suitable for long-term operations. 2. PURPOSE To determine the electrical and environmental characteristics of battery charge controllers. The actual life expectancy, so qualified, of battery charge controllers will depend on their design, their environment and the conditions under which they operate. 3. SAMPLING Three battery charge controllers for qualification testing (plus spares as desired) will be taken at random from a production batch or batches. The battery charge controllers should have been subjected to the manufacturer's normal inspection, quality control and production acceptance procedures. The battery charge controllers should be complete in every detail and must be accompanied by the manufacturers handling, mounting and connection instructions, including the maximum permissible voltage. When the battery charge controllers are prototypes of a new design and not from production, the fact should be noted in the test report (see Section One - Item 9 Report). 4. MARKING Each battery charge controller should carry the markings specified in General Safety and Performance Requirements - Section One – Item 4 - Markings: Compliance is checked by inspection and by trying to remove the markings by rubbing lightly for 15 seconds with two pieces of cloth: one soaked in water and the other with petroleum spirit. Note: The petroleum spirit should consist of a solvent hexane with a maximum of 0.1 volume percentage aromatics content, a kauri-butanol value of 29, an initial boiling-point of approximately 65°C, a dry-point of approximately 69°C and a density of approximately 0.68 g/cm3. -5- 5. TESTING The battery charge controllers should be subjected to the tests in Figure 1, in the specified order. The test procedures and severities including initial and final measurements, where necessary, are detailed in Section 2 – Standard Test Methods. In carrying out the tests, the manufacturer's handling, mounting and connection instructions should be strictly observed. 6. PASS CRITERIA A battery charge controller will be judged to have passed the qualification tests if each test sample meets the following criteria: The voltage set points for the deep discharge and overcharge protection does not exceed 0.5% of the prescribed limit after each test. No sample exhibited any short-circuit or open circuit conditions during the tests. There is no visual evidence of a major defect, as defined in Section One - Item 7 – Major Visual Defects. The insulation test requirements are met after the tests. All three (3) samples should pass the tests to be judged as meeting the qualification requirements. Should one sample fail in any test, a new batch of battery charge controllers should be subjected to all relevant tests, following the same sequence. If any one of the battery charge controllers fails, the design will be deemed not meeting the qualification standard. 7. MAJOR VISUAL DEFECTS For the purpose of design qualification and type approval, the following are considered to be major visual defects: shorted terminals shorted routes in the printed circuit board shorted electronic parts in the printed circuit board 8. VALIDITY AND COMPLIANCE MONITORING The certification of those which pass the design qualification and type approval tests will have a validity of six (6) months to be renewed thereafter. The test agency should monitor compliance of the same. 9. REPORT The test agency must prepare a certified test report of the qualification tests with the measured performance characteristics, details of any failures, and re-tests. A copy of this report should be provided to the manufacturer and kept for reference purposes. -6- 10. MODIFICATIONS Any change in the design, materials, components or processing of the battery charge controller may require a repetition of some or all the qualification tests to maintain type approval. SECTION TWO - STANDARD TEST METHODS 11. STANDARD TEST CONDITIONS 11.1 Ambient temperature and test room Tests should be made in a room free of draughts and at room temperature stabilized to plus or minus 1◦C. 11.2 Test voltage Unless otherwise specified, the battery charge controller to be tested should be operated at its design voltage. 12. BATTERY CHARGE CONTROLLER VOLTAGE HYSTERESIS TEST 12.1 LOW BATTERY VOLTAGE HYSTERESIS Purpose: To determine the low battery voltage hyteresis of the charge controller Procedure: a) Set up the apparatus for low voltage hysteresis test as shown in Figure 2a. b) Apply 12V at the battery terminals of the controller. Determine if the current is passing through the load circuit. c) Decrease the voltage applied at a rate not greater than 0.1 V/s. Continue until the load is disconnected from the battery. This is the low voltage disconnect level of the controller. d) Increase the voltage applied at the same rate as above. Continue until the load is reconnected to the battery. This is the low voltage reconnect voltage. The low voltage disconnect should be set at no more than 10% below the nominal battery voltage. The cut-in voltage for reconnecting the load should be set at about 5% above the nominal battery voltage. -7- 12.2 HIGH BATTERY VOLTAGE HYSTERESIS Purpose: To determine the high battery voltage hyteresis of the charge controller Procedure: a) Set up the apparatus for high voltage hysteresis test as shown in Figure 2b. b) Apply the nominal voltage required at the battery terminals of the controller. Determine if current is passing through the load circuit. c) Increase the voltage applied at a rate not greater than 0.1 V/s. Continue until the PV module is disconnected from the battery. This is the high voltage disconnect level of the controller. d) Decrease the voltage applied at the same rate as above. Continue until the PV module is reconnected to the battery. This is the high voltage reconnect voltage. The high voltage disconnect shall be set at no more than 20% above the nominal battery voltage. The reconnect voltage for reconnecting the PV generator should be set at about 8% above the nominal battery voltage. 13. NO-LOAD LOSS TEST Purpose: To determine the no-load loss of a charge controller. Procedure: a) Set-up the apparatus for no-load loss as shown in Figure 3. b) Set the variable dc source to the required nominal voltage. c) Measure the current consumption of the charge controller without load. The no-load loss of the battery charge controller should not exceed 0.5% of the rated load current. 14. VERIFICATION OF RELIABILITY OF SERVICE WITH APPLIED FULL PV MODULE VOLTAGE AT NO-LOAD CONDITION Purpose: To determine the robustness and ruggedness of the charge controller when full PV module voltage is applied at no-load condition. Procedure: -8- a) Set up the apparatus as shown in Figure 4. b) Increase the voltage applied at a rate not greater than 0.1 V/s until the voltage is equal to the rated solar generator voltage. c) Maintain this voltage for about 1 hour. d) Decrease the voltage applied at a rate not greater than 0.5 V/s. Note any shorted terminals or shorted routes in the printed circuit board or damaged component. e) Do voltage hysteresis tests as described in Sections 12.1 and 12.2. The Battery Charge Controller is subjected to no-load conditions by removing the battery, allowing the BCC to absorb the short circuit current (Isc) of the solar generator. The BCC should be able to handle the full current from the solar generator. The BCC passes if after being subjected to the above-mentioned test still functions normally. 15. DETERMINATION OF RATED SOLAR CURRENT Purpose: To determine the rated solar current capacity of a charge controller. Procedure: a) Set-up the apparatus as shown in Figure 5. b) Increase the voltage applied at a rate not greater than 0.1 V/s until the rated voltage of the charge controller for high voltage disconnect is reached. Slowly increase the current until the rated solar current is reached. c) Maintain this voltage and current for about 1 hour. d) Decrease the voltage and current applied at a rate not greater than 0.1 V/s. Note any shorted terminals or shorted routes in the printed circuit board or damaged component. The BCC should be able to handle the maximum solar current as specified in the nameplate rating. The battery charge controller passes if after being subjected to the test still functions normally. 16. DETERMINATION OF RATED LOAD CURRENT Purpose: To determine the rated load current capacity of a charge controller. Procedure: -9- a) Set-up the apparatus as shown in Figure 6. b) Increase the voltage applied at a rate not greater than 0.1 V/s until the rated operating voltage of the charge controller is reached. Slowly increase the current until the rated load current is reached. c) Maintain this voltage and current for about 1 hour. d) Decrease the voltage and current applied at a rate not greater than 0.1 V/s. Note any shorted terminals or shorted routes in the printed circuit board or damaged component. The BCC shall be able to handle the maximum load current as specified. The battery charge controller passes if after being subjected to the test still functions normally. 17. SHORT CIRCUIT PROTECTION TEST Purpose: To determine the ability of the controller to withstand short-circuit conditions. Procedure: a) Short-circuit the load terminals. The BCC should be protected against shortcircuits by a fuse, circuit breaker or by any other means. b) The BCC should function normally after the fuse is replaced or the circuit breaker reset by applying the voltage hysteresis tests as described in Section 2 – Items 12.1 and 12.2. The battery charge controller passes if after being subjected to the test still functions normally. 18. REVERSE POLARITY PROTECTION TEST, SOLAR GENERATOR Purpose: To determine the ability of the controller to withstand reverse polarity effects. Procedure: a) Reverse the polarity of the solar generator terminals. b) The BCC should function normally after the fuse is replaced or the circuit breaker reset by applying the voltage hysteresis tests as described in Sections 12.1 and 12.2. The battery charge controller passes if after being subjected to the test still functions normally. - 10 - 19. REVERSE POLARITY PROTECTION TEST, BATTERY Purpose: To determine the ability of the controller to withstand reverse polarity effects on the battery. Procedure: a) Reverse the polarity of the battery terminals. b) The BCC should function normally after the fuse is replaced or the circuit breaker reset by applying the voltage hysteresis tests as described in Sections 12.1 and 12.2. The BCC should be protected against reverse polarity, at least, with a fuse, or a circuit breaker. The battery charge controller passes if after being subjected to the test still functions normally. 20. ENVIRONMENTAL CYCLING The battery charge controller is conditioned for 24 hours at 50% relative humidity and 48 hours at 95% humidity. The temperature of the air at all places where samples can be located is maintained within 1°C at about 40oC. The sample is tested at these conditions for the voltage hysteresis as described in Sections 12.1 and 12.2. At the end of these tests, the battery charge controller should operate normally. - 11 - APPENDIX A - TEST CIRCUITS Voltage Hysteresis No Load Loss No Battery Connection Maximum PV Array Current Maximum Load Current Environmental Cycling Figure 1. Test Sequence - 12 - Battery Charge Controller S+ + S- B+ B- L+ Variable DC load L- A Variable DC supply V - A a. Circuit for measurement of load low voltage hysteresis Battery Charge Controller S+ S- B+ B- L+ L- 4.9 V - A Ohmmeter Variable DC supply V + b. Circuit for measurement of PV generator high voltage hysteresis Figure 2. Circuits for voltage hysteresis measurements Battery Charge Controller S+ + S- B+ B- L+ L- A Variable DC supply V - Figure 3. Circuit for measurement of internal power consumption - 13 - Battery Charge Controller S+ + S- B+ B- L+ Variable DC load L- A Variable DC Supply V - Figure 4. Circuit for testing no battery connection Battery Charge Controller S+ S- B+ B- L+ L- Variable DC load A A Variable DC supply V Figure 5. Circuit for the determination of maximum PV module current Battery Charge Controller S+ + S- B+ A Variable DC supply B- L+ L- Variable DC load A V - Figure 6. Circuit for the determination of maximum load current - 14 -