FUEL PUMP CONTROL [SKYACTIV-G 1.3, SKYACTIV-G 1.5]


id0140q1004100


With Fuel Pump Control Module


Outline

•  By switching the fuel pump discharge amount, reduced power consumption and improved fuel economy have been achieved.
•  The PCM determines the optimum fuel pump discharge amount according to the engine operation conditions, and sends the fuel pump drive signal to the fuel pump control module.


Block Diagram

am2zzn00004969


Operation

Fuel pump relay
•  The PCM switches the fuel pump relay on/off according to the engine operation conditions.

Relay ON/OFF

Control conditions

ON
•  When any of the following conditions is met:
―  When ignition is switched ON (for approx. 1 s)
―  During engine cranking
―  While engine is running
―  When engine is stopped by i-stop control
OFF
•  When engine is stopped (excludes engine stop by i-stop control)
•  Immobilizer system related information (engine start prohibited) received from start stop unit
•  Collision signal from SAS control module is received


Fuel pump control module

•  The PCM determines the fuel pump discharge amount according to the engine operation conditions, and controls the output duty ratio to the fuel pump control module according to the discharge amount.

Output duty ratio

Control conditions

95%
•  When any of the following conditions is met:
―  At engine start
―  Fuel pump control module malfunction (if request voltage is unobtainable)
10—90%
•  Except for control conditions with output duty ratio of 5% or 95%
5%
•  When engine is stopped by i-stop control

Fuel pump operation circuit diagram

am2zzn00003565


Without Fuel Pump Control Module


Outline

•  Performs energization of fuel pump relay only when engine is running (operates the fuel pump) to improve safety and durability.


Block Diagram

am2zzn00003566


Operation

•  The PCM controls energization of the circuit opening relay according to the engine operation conditions to switch the circuit opening relay on/off.

Relay ON/OFF

Control conditions

ON
•  When any of the following conditions is met:
―  When ignition is switched ON (engine off) (for approx. 1 s)
―  During engine cranking
―  While engine is running
OFF
•  When engine is stopped (excludes engine stop by i-stop control)