Method for controlling an inlet-adjustment mechanism for a turbocharger compressor
A method for controlling an inlet-adjustment mechanism in an air inlet for a compressor so as to switch the mechanism between open and closed positions for adjusting a flow area of the inlet. The method includes an algorithm for determining when the inlet-adjustment mechanism is in a failure mode. In accordance with the method, when the operating point on the compressor map is on the high-flow side of a threshold line at which the inlet-adjustment mechanism is switched from one position to the other, a measured speed or pressure ratio is compared to a theoretical value for the speed or pressure ratio based on a compressor map for the open position of the mechanism. If the measured value differs from the theoretical value by more than a predetermined tolerance, a failure mode is indicated.
1. A method of failure-detection for a compressor inlet-adjustment mechanism disposed in an air inlet defined by a compressor housing upstream of a compressor wheel of a compressor of a turbocharger for boosting intake pressure of an internal combustion engine, the inlet-adjustment mechanism comprising a variable-geometry orifice, the variable-geometry orifice in a closed position having an inner diameter that is smaller than an inner diameter of a shroud surface of the compressor housing at an inducer portion of the compressor wheel, the variable-geometry orifice being positioned such that an effective diameter of the air inlet at the inducer portion is determined by the inner diameter of the variable-geometry orifice, the variable-geometry orifice in the open position being moved such that the effective diameter of the air inlet at the inducer portion is determined by the shroud surface, the method comprising:
identifying a threshold line on a compressor map specifying interrelationships between compressor pressure ratio PR, flow rate W, and one of turbocharger speed N and engine speed Ne, the threshold line being a line at which the inlet-adjustment mechanism is to be switched between the open position and the closed position when an operating point of the compressor on the compressor map reaches the threshold line;
determining a measured compressor flow rate W m , a measured compressor pressure ratio PR m , and one of a measured turbocharger speed N m and a measured engine speed Ne m for a current operating point of the turbocharger and engine;
determining a theoretical value for a characteristic compressor performance parameter for the current operating point, where is one of PR and N and where the theoretical value for is derived from a first compressor map MAP O specifying an interrelationship between flow rate W, pressure ratio PR, and one of turbocharger speed N and engine speed Ne, when the inlet-adjustment mechanism is open;
determining whether the current operating point is on a high-flow side of the threshold line or is on a low-flow side of the threshold line; and
when the current operating point is determined to be on the high-flow side of the threshold line at which a desired state of the inlet-adjustment mechanism is open, if a measured value for differs from the theoretical value for by more than a predetermined tolerance, determining that the inlet-adjustment mechanism is in a failure mode, and if the measured value for is within the predetermined tolerance of the theoretical value for , determining that the inlet-adjustment mechanism is operating normally.
2. The method of claim 1 , further comprising:
when the current operating point is determined to be on the low-flow side of the threshold line at which a desired state of the inlet-adjustment mechanism is closed, checking for flow instability in the air inlet of the compressor, and if flow instability is detected, determining from the first compressor map MAP O a flow rate W S-O at surge, at the measured compressor pressure ratio PR, and if W m differs from W S-O by less than a predetermined tolerance, determining that there is a risk of surge, and if no flow instability is detected, determining that the inlet-adjustment mechanism is operating normally.
3. The method of claim 1 , wherein the characteristic performance parameter is turbocharger speed N.
4. The method of claim 1 , wherein the characteristic performance parameter is compressor pressure ratio PR.
5. A computer program product comprising at least one computer-readable storage medium having computer-executable program code instructions stored therein for controlling a compressor inlet-adjustment mechanism disposed in an air inlet defined by a compressor housing upstream of a compressor wheel of a compressor of a turbocharger for boosting intake pressure of an internal combustion engine, the inlet-adjustment mechanism comprising a variable-geometry orifice, the variable-geometry orifice in a closed position having an inner diameter that is smaller than an inner diameter of a shroud surface of the compressor housing at an inducer portion of the compressor wheel, the variable-geometry orifice being positioned such that an effective diameter of the air inlet at the inducer portion is determined by the inner diameter of the variable-geometry orifice, the variable-geometry orifice in the open position being moved such that the effective diameter of the air inlet at the inducer portion is determined by the shroud surface, the compressor having a compressor map specifying interrelationships between flow rate W, compressor pressure ratio PR, and one of turbocharger speed N and engine speed Ne, the compressor map including a threshold line at which the inlet-adjustment mechanism is to be switched between the open position and the closed position, the computer-executable program code instructions comprising:
program code instructions for determining a measured compressor flow rate W m , a measured compressor pressure ratio PR, and one of a measured turbocharger speed N m and a measured engine speed Ne m for a current operating point of the turbocharger and engine;
program code instructions for determining a theoretical value for a characteristic compressor performance parameter for the current operating point, where is one of pressure ratio PR and turbocharger speed N and where the theoretical value for is derived from a first compressor map MAP O specifying an interrelationship between flow rate W, pressure ratio PR, and one of turbocharger speed N and engine speed Ne, when the inlet-adjustment mechanism is open;
program code instructions for determining whether the current operating point is on a high-flow side of the threshold line or is on a low-flow side of the threshold line; and
program code instructions for determining that the inlet-adjustment mechanism is in a failure mode when the current operating point is determined to be on the high-flow side of the threshold line at which a desired state of the inlet-adjustment mechanism is open and when a measured value for differs from the theoretical value for by more than a predetermined tolerance, and if the measured value for is within the predetermined tolerance of the theoretical value for , determining that the inlet-adjustment mechanism is operating normally.
6. The computer program product of claim 5 , further comprising program code instructions for checking for flow instability in the air inlet of the compressor when the current operating point is determined to be on the low-flow side of the threshold line, and if flow instability is detected, determining a flow rate W S-O at surge, at the measured compressor pressure ratio PR, based on the first compressor map MAP O , and for determining that there is a risk of surge when W m differs from W S-O by less than a predetermined tolerance, and if no flow instability is detected, determining that the inlet-adjustment mechanism is operating normally.