JAJU858 December   2022

 

  1.   概要
  2.   リソース
  3.   特長
  4.   アプリケーション
  5.   5
  6. 1System Description
    1.     7
    2. 1.1 EV Charging Station Challenges
      1. 1.1.1 SAE J1772 or Equivalent Standard Compliant EV Charging Stations
      2. 1.1.2 AC and DC Leakage, Residual Current Detection (RCD)
      3. 1.1.3 Efficient Relay and Contactor Drive
      4. 1.1.4 Contact Weld Detection
    3. 1.2 Key System Specifications
  7. 2System Overview
    1. 2.1 Block Diagram
    2. 2.2 Design Considerations
      1. 2.2.1 Isolated AC/DC Power Supply Design
        1. 2.2.1.1  Input Bulk Capacitance and Minimum Bulk Voltage
        2. 2.2.1.2  Transformer Turns-Ratio, Primary Inductance, and Primary Peak Current
        3. 2.2.1.3  Transformer Parameter Calculations: Primary and Secondary RMS Currents
        4. 2.2.1.4  Main Switching Power MOSFET Selection
        5. 2.2.1.5  Rectifying Diode Selection
        6. 2.2.1.6  Output Capacitor Selection
        7. 2.2.1.7  Capacitance on VDD Pin
        8. 2.2.1.8  Open-loop Voltage Regulation Versus Pin Resistor Divider, Line Compensation Resistor
        9. 2.2.1.9  Feedback Elements
        10. 2.2.1.10 Backup Power Supply
        11. 2.2.1.11 Supercapacitor Selection
        12. 2.2.1.12 Supercapacitor Charger Design
      2. 2.2.2 Control Pilot Signal Interface
        1. 2.2.2.1 J1772 Duty Cycle
          1. 2.2.2.1.1 Control Pilot Signal States
          2. 2.2.2.1.2 Control Pilot Signal Circuit
      3. 2.2.3 Relay Drive and Weld Detect
      4. 2.2.4 Residual Current Detection
        1. 2.2.4.1 Auto-Oscillation Circuit
          1.        37
        2. 2.2.4.2 DRV8220 H-Bridge
        3. 2.2.4.3 Saturation Detection Circuit
        4. 2.2.4.4 H-Bridge Controlled by DFF
        5. 2.2.4.5 Filter Stage
        6. 2.2.4.6 Differential to Single-Ended Converter
        7. 2.2.4.7 Low-Pass Filter
        8. 2.2.4.8 Full-Wave Rectifier
        9. 2.2.4.9 MCU Selection
    3. 2.3 Highlighted Products
      1. 2.3.1  UCC28742
      2. 2.3.2  TLV1805
      3. 2.3.3  DRV8220
      4. 2.3.4  ISO1212
      5. 2.3.5  ADC122S051
      6. 2.3.6  TPS7A39
      7. 2.3.7  TPS7A20
      8. 2.3.8  ATL431
      9. 2.3.9  TL431
      10. 2.3.10 TPS563210A
      11. 2.3.11 TPS55330
      12. 2.3.12 TPS259470
      13. 2.3.13 TL7705A
  8. 3Hardware, Testing Requirements, and Test Results
    1. 3.1 Hardware Requirements
    2. 3.2 Test Requirements
      1. 3.2.1 Power Supply Test Setup
      2. 3.2.2 Weld Detect Test Setup
    3. 3.3 Test Results
      1. 3.3.1 Isolated AC/DC Power Supply Based on UCC28742
        1. 3.3.1.1 Efficiency and Output Voltage Cross Regulation
        2. 3.3.1.2 Efficiency and Output Voltage Regulation of TPS563210
        3. 3.3.1.3 Output Voltage Ripple Waveforms
        4. 3.3.1.4 Start, Shutdown, Backup Power, and Transient Response Waveforms
        5. 3.3.1.5 Thermal Performance
      2. 3.3.2 TLV1805-Based Control Pilot Interface
        1. 3.3.2.1 TLV1805 Output Rise and Fall Time
        2. 3.3.2.2 Control Pilot Signal Voltage Accuracy in Different States
      3. 3.3.3 DRV8220-Based Relay and Plug Lock Drive
      4. 3.3.4 ISO1212-Based Isolated Line Voltage Sensing
  9. 4Design and Documentation Support
    1. 4.1 Design Files
      1. 4.1.1 Schematics
      2. 4.1.2 Bill of Materials
    2. 4.2 Documentation Support
    3. 4.3 サポート・リソース
    4. 4.4 Trademarks
  10. 5About the Author

2.2.2.1 J1772 Duty Cycle

The duty cycle of the pilot signals communicate the limit of current the EVSE is capable of supplying to the vehicle; the vehicle can then use up to that amount of current for the charging circuitry. This current rating is primarily determined by the electromechanical components in the EVSE, such as conductors, relays, contactors, and the service connection.

The relationship between duty cycle and current is defined by two different equations depending on the current range specified; for a 6- to 51-A service, is:

Equation 60. GUID-5C435E85-5A5D-420F-92D3-DC0A8C1CD2CF-low.gif

For a higher service in the 51- to 80-A range, is:

Equation 61. GUID-16CA16E8-1A87-4FE8-986C-70C84FCDA844-low.gif

To demonstrate this relationship further, Table 2-2 shows some of the common service ratings.

Table 2-2 Pilot Signal Example Duty Cycle
AMPSDUTY CYCLE
58.3%
1525%
3050%
4066.6%
6590%
8096%

In this design, the PWM is generated by a timer module on the MSP430™ MCU. The current rating can typically be set as a permanent value in the firmware because the current rating is so tightly coupled to the external hardware.

Advanced EVSEs with a human machine interface (HMI) can enable the current to be derated if the service line is unable to provide enough current with a stable voltage. A significant voltage drop as a result of wire loss is possible in these high-current applications.