C.E. Niehoff & Co. EPM Troubleshooting Guides

Troubleshooting Guide
for EPM Electric Power Manager
Hazard Defi nitions
These terms are used to bring attention to presence of hazards of various risk levels or to important information concerning product life.
Indicates presence of hazard(s) that
WARNING
can cause severe personal injury, death or substantial property damage if ignored.
Indicates presence of hazard(s) that
CAUTION
can cause minor personal injury or property damage if ignored.
Indicates special instructions on
NOTICE
installation, operation or mainte­ nance that are important but not related to personal injury hazards.
Table of Contents
Section A: Component Description ............................... 2
Section A: Start-up/Shutdown Procedures .................... 2
Section B: CAN/J1939 Diagnostics ............................... 3
Section C: Basic Troubleshooting ................................. 4
Section D: Troubleshooting the EPM ......................... 5-7
Until temperatures of electrical
NOTICE
system components stabilize, these conditions may be observed during cold start voltage tests.
Maintenance/Low Maintenance Battery: — Immediately after engine starts, system volts measure lower than regulator setpoint and system amps measure at a medium level. — 3-5 minutes into charge cycle, volts increase and amps decrease. — 5-10 minutes into charge cycle, volts reach regulator setpoint or very close, and amps decrease to a minimum. — Low maintenance battery has same characteris­ tics with slightly longer recharge times.
Maintenance-free Battery: — Immediately after engine starts, system volts measure lower than regulator setpoint with low charging amps. — Once the charge cycle begins, low volts and low amps are still present. — After the alternator energizes, voltage will increase several tenths. Amps will increase gradually, then quickly, to medium to high amps. — Finally, volts will increase to setpoint and amps will decrease. The time it takes to reach optimum voltage and amperage will vary with engine speed, load, and ambient temperature.
High-cycle Maintenance-free Battery: — These batteries respond better than standard maintenance-free. Charge acceptance of these batteries may display characteristics similar to maintenance batteries.
Battery Charge Volt and Amp Values
Volt and amp levels fluctuate depending on the battery state of charge. If batteries are in a state of discharge— as after extended cranking time to start the engine— system volts will measure lower than the regulator set­point after the engine is restarted and system amps will measure higher. This is a normal condition for the charging system; the greater the battery discharge level, the lower the system volts and the higher the system amps. The volt and amp readings will change as batter­ies recover and become fully charged: system volts will increase to regulator setpoint and system amps will decrease to low level (depending on other loads).
Low Amps: Minimum or lowest charging system amp value required to maintain battery state of charge, obtained when testing the charging system with a fully charged battery and no other loads applied. This value will vary with battery type.
Medium Amps: System amps value which can cause the battery temperature to rise above adequate charging temperature within 4-8 hours of charge time. To prevent battery damage, the charge amps should be reduced when battery temperature rises. Check battery manufacturer’s recommendations for proper charge amp rates.
High Amps: System amps value which can cause the battery temperature to rise above adequate charging temperature within 2-3 hours of charge time. To prevent battery damage, the charge amps should be reduced when battery temperature rises. Check battery manufacturer’s recommendations for proper charge amp rates.
Battery Voltage: Steady-state voltage value as mea­sured with battery in open circuit with no battery load. This value relates to battery state of charge.
Charge Voltage: Voltage value obtained when the charging system is operating. This value will be higher than battery voltage and must never exceed the regulator voltage setpoint.
B+ Voltage: Voltage value obtained when measuring voltage at battery positive terminal or alternator B+ terminal.
Surface Charge: Higher than normal battery voltage occurring when the battery is disconnected from battery charger. The surface charge must be removed to determine true battery voltage and state of charge.
Significant Magnetism: Change in strength or intensity of a magnetic field present in alternator rotor shaft when the field coil is energized. The magnetic field strength when the field coil is ener­gized should feel stronger than when the field is not energized.
Voltage Droop or Sag: Normal condition occurring when the load demand on alternator is greater than rated alternator output at given rotor shaft RPM.
TG0051A
Page 1
Section A: Component Description and Operation
EPM Description and Operation
EPM Electric Power Manager used with these units
• is rated for continuous current at 200 A on 28 V side. The 14 V side is rated for continuous current at 100 A.
• manually connects batteries after battery connect switch on vehicle is pressed.
• automatically disconnects batteries from vehicle loads 3 minutes after engine shuts down.
• provides 28 V auxillary output power for up to four 20 A channels and 14 V auxillary output power for one 20 A channel, protected by an internal, reset­table, electronic circuit breaker.
• keeps batteries connected to system when emergency flashers are activated.
Normal Start-Up Procedure
1. Press the vehicle battery-connect switch for about one second to connect batteries to electrical system.
2. Turn START-RUN switch to RUN.
3. Wait until glow plug light goes off.
4. Turn START-RUN switch to START and crank engine.
5. Return switch to RUN when engine starts.
6. If engine fails to crank, turn START-RUN switch to OFF, repeat steps 1-5 above.
Emergency Start-Up Procedure
WARNING
1. Connect slave vehicle Nato connector to vehicle.
2. Follow steps 2-5 under “Normal Start-Up Procedure.”
3. Disconnect slave NATO connector after engine is running.
This procedure will bypass EPM and batteries in system. Use this procedure ONLY when vehicle must be removed immediately from location in an EMERGENCY.
Shutdown Procedure
1. Place gear shift in park or neutral and set parking brake.
2. Turn start-run switch to OFF to stop engine.
3. Batteries will be disconnected from vehicle in 3 min. unless emergency flashers are on, then batteries will stay connected until f lashers are turned off or battery is discharged.
Page 2
Figure 1 – Battery Connect Switch
TG0051A
Section B: CAN/J1939 Diagnostics
CAN/J1939 Interface
DESCRIPTION AND OPERATION
The EPM is compatible with CAN bus standard for digital networks and uses the SAE J1939 communications protocol.
CEN uses MIL-STD connector MS3112E12-10P to interface between the EPM and the DPA adapter used to monitor the broadcast messages on the CAN bus line. The readouts of these messages are shown in Table 2 for the EPM.
TABLE 1 – J1939 Connector
Circuit Identifi cation
Pin
A
B
C
D
E
F
G
H
J
K
Identifi cation
CAN High
CAN Low
CAN Shield
Ground
Restricted use
Restricted use
Restricted use
unused
unused
+28V p o wer
Figure 2 – J1939
Connector Pins
TABLE 2 – EPM/J1939 Readout Diagnostics (With Engine Running)
EPM Readout
Load Voltage 28 V System
Load Voltage 14 V System
Alternator Speed
Battery Voltage 28 V System
Battery Voltage 14 V System
EPM Temperature
Charging and Discha rging Current of 28 V Battery
Batt Charging 28 V LED
Batt Charging 14 V LED
Main Switches On
Cranking Detected
Emergency Flasher Detected
10 A (varies according to battery condition)
Expected Reading
27–29 V
13.5–14.5 V
1200 to 6000 RPM
27–29 V
13.5–14.5 V
–50ºF (–46ºC) to 200ºF (93ºC)
OK
OK
OK
OK
OK
T
EPM Connector to Regulator
Figure 3 – EPM Electric Power Manager
T
J1939 Connector Under Cap
TG0051A
Page 3
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