BSI PD IEC/TS 62763:2013:2014 Edition
$167.15
Pilot function through a control pilot circuit using PWM (pulse width modulation) and a control pilot wire
Published By | Publication Date | Number of Pages |
BSI | 2014 | 36 |
This Technical Specification describes the pilot wire function designed as a control mechanism for the supply of electrical energy to electric vehicles, principally for the charging of the traction batteries of the vehicle. It concerns all charging systems that ensure the pilot function with a pilot wire circuit with PWM for mode 2, mode 3 and mode 4 charging as described in the IEC 61851 series.
This document describes the functions and sequencing of events for this circuit based on the recommended typical implementation circuit parameters. The parameters indicated also ensure the interoperability of control pilot wire systems designed according to SAE J1772.
This document is not applicable to vehicles using pilot functions that are not based on a PWM signal and a pilot wire.
NOTE 1 In the context of this document the words “EV supply equipment” designate any one of the following: the AC EV supply equipment in mode 3, the in cable control box in mode 2 and/or the DC EV supply equipment in mode 4.
NOTE 2 The control pilot wire is a supplementary conductor, in addition to the power lines linking the vehicle to EV supply equipment via the vehicle coupler.
PDF Catalog
PDF Pages | PDF Title |
---|---|
4 | CONTENTS |
6 | FOREWORD |
8 | INTRODUCTION |
9 | 1 Scope 2 Normative references 3 Control pilot circuit 3.1 General |
10 | 3.2 Typical pilot electric equivalent circuit Figures Figure 1 – Typical control pilot electric equivalent circuit |
11 | 3.3 Simplified pilot electric equivalent circuit 3.4 Other requirements Figure 2 – Simplified control pilot electric equivalent circuit |
12 | 4 Requirements for parameters Tables Table 1 – Maximum allowable carrier signal voltages on pilot wire Table 2 – Control pilot circuit parameters (see Figures 1 and 2) |
13 | Table 3 – Vehicle control pilot circuit values and parameters |
14 | Table 4 – System states detected by the EV supply equipment |
16 | Table 5 – State behavior |
17 | Figure 3 – State machine diagram for typical control pilot Figure 4 – State machine diagram for simplified control pilot |
18 | Table 6 – List of sequences |
26 | Table 7 – Pilot duty cycle provided by EV supply equipment Table 8 – Maximum current to be drawn by vehicle |
27 | 5 Test procedures for immunity of EV supply equipment to wide tolerances on the pilot wire and the presence of high frequency data signals on the pilot wire 5.1 General 5.2 Constructional requirements of the EV simulator 5.3 Test procedure Table 9 – Test resistance values |
28 | 5.4 Test list – Oscillator frequency and generator voltage test Table 10 – Parameters of control pilot voltages |
29 | 5.5 Duty cycle test 5.6 Pulse wave shape test 5.7 Sequences diagnostic – normal charge cycle Figure 5 – Normal operation cycle Table 11 – Test parameters of control pilot signalsat the measure point according to Figure 8 |
30 | Figure 6 – Simplified control pilot cycle Table 12 – Normal charge cycle test |
31 | 5.8 Open earth wire test 5.9 Test of short circuit values of the voltage 5.10 Example of a test simulator of the vehicle (informative) Figure 7 – Optional charge cycle test |
32 | Figure 8 – Example of a test circuit (EV simulator) |
33 | 5.11 Optional hysteresis test 5.11.1 General Table 13 – Position of switches Table 14 – Initial settings of the potentiometer at the beginning of each test |
34 | 5.11.2 Test sequence for hysteresis between states B and C 5.11.3 Test sequence for hysteresis between states C-E, D-E 5.11.4 Test sequence for hysteresis between states C-D |