Gasoline reid vapor pressure detection system and method for a vehicle propulsion system
A vehicle propulsion system includes a first pump having an inlet for receiving fuel from a fuel reservoir and an outlet for providing pressurized fuel to a fuel feed line at a first pressure, a fuel feed line pressure sensor, a second pump having an inlet for receiving fuel from the fuel feed line and an outlet for providing pressurized fuel to an engine fuel rail at a second pressure, the second pressure being higher than the first pressure, a fuel temperature sensor, and a controller controlling the first pump to reduce the pressure of the fuel in the fuel feed line and determining whether the pressure of the fuel in the fuel feed line has reached a vaporization pressure of a component in the fuel.
1. A gasoline reid vapor detection system in vehicle propulsion system comprising:
a first pump having an inlet for receiving fuel from a fuel reservoir and an outlet for providing pressurized fuel to a fuel feed line at a first pressure;
a fuel feed line pressure sensor that generates a fuel feed line pressure signal that is based upon a pressure of fuel in the fuel feed line;
a second pump having an inlet for receiving fuel from the fuel feed line and an outlet for providing pressurized fuel to an engine fuel rail at a second pressure, the second pressure being higher than the first pressure;
a fuel temperature sensor that generates a fuel temperature signal that is based upon a temperature of the fuel;
a fuel rail pressure sensor that generates a fuel rail pressure signal based upon a pressure of fuel in the fuel rail; and
a controller in communication with the first pump for controlling the first pump to control the pressure of the fuel in the fuel feed line, wherein the controller controls the first pump to reduce the pressure of the fuel in the fuel feed line, and wherein the controller determines whether the pressure of the fuel in the fuel feed line has reached a vaporization pressure of a component in the fuel, wherein the controller monitors a performance characteristic of the second pump to determine whether the pressure of the fuel in the fuel feed line has reached a vaporization pressure of a component in the fuel, wherein the second pump performance characteristic comprises a fuel rail pressure rise in the fuel rail per stroke of the second pump, wherein the controller generates a slow filtered signal based upon a slow filter of the fuel rail pressure rise in the fuel rail per stroke of the second pump and a fast filtered signal based upon a fast filter of the fuel rail pressure rise in the fuel rail per stroke of the second pump, and wherein the controller determines whether the pressure of the fuel in the fuel feed line has reached a vaporization pressure of a component in the fuel based upon a comparison of the slow filtered signal to the fast filtered signal.
2. The system of claim 1 , wherein the controller determines whether the pressure of the fuel in the fuel feed line has reached a vaporization pressure of a component in the fuel based upon a determination that the slow filtered signal has a value that exceeds a value of the fast filtered signal.