The fuel delivery rate and the fuel cutoff are controlled in the ISIS (Intelligent Safety Integration System).
The fuel pump is a 2-stage internal gear pump.
The fuel pump is driven via a collector. The speed of the collector is fed back to the processor of the SBSR (satellite, B-pillar, right) as an input variable.
Supply:
The following control modules are involved in the message transmission for electronic control of the fuel pump:
Fuel is supplied depending on consumption. The DME (digital engine electronics) determines a fuel requirement in liters per hour.
The DME sends that fuel volume request via the PT-CAN bus (powertrain CAN bus) -> ZGM (central gateway module) -> BYTEFLIGHT bus -> SIM (safety information module) -> BYTEFLIGHT-Bus -> to the SBSR (satellite, B-pillar right) control module.
The required volume of fuel is converted into a nominal speed for the fuel pump.
The pump speed is controlled by the pulse duty factor of a pulse-width modulated square-wave signal. This square-wave signal provides the voltage supply at the motor of the fuel pump: the longer the pause between the vertical flanks of the square-wave signal, the lower the voltage supply at the fuel pump. The delivery rate of the fuel pump is correspondingly lower.
If the DME fails to issue the fuel requirement signal, the fuel pump is activated with the adjustable maximum speed.
If the ISIS system detects a crash of sufficient severity, the flow of fuel is interrupted. This prevents the fuel from leaking out and igniting.
The fuel pump can be reactivated by switching the ignition off and on.
The pump is operated on an adjustable maximum supply rate if, with terminal R ON,
This ensures that the full supply rate remains available. The fuel cutoff in an emergency is unaffected by this.
In all cases, only perform work on the fuel pump with the ignition off.