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US 7,568,339 B2Granted
Control for variable geometry compressor
AssigneeHoneywell International Inc.
InventorsPhillipe Noelle, Nicolas Vazeille
Life of this patent
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Abstract
An exemplary controller for a variable geometry compressor includes one or more inputs for receiving engine operating information and for receiving a signal representative of geometry of a variable geometry compressor and control logic to call for actuation of an actuator based at least in part on the engine operating information received by the one or more inputs and to call for actuation of the actuator based at least in part on the signal received by the one or more inputs whereby actuation of actuator causes a change in geometry of a variable geometry compressor. Various other exemplary technologies are also disclosed.
Claims8
A method comprising:
- providing a variable geometry compressor and an internal combustion engine wherein the variable geometry compressor comprises a plurality of vanes to vary geometry of a diffuser section of the compressor;
- operating the engine according to a series of operating condition;
- for each operating condition, determining a position for the vanes to optimize compressor efficiency;
- providing a non-linear model for position of the vanes based on one or more engine operating parameters wherein the non-linear model comprises one or more coefficients;
- performing a statistical analysis to fit the non-linear model using the determined positions of the vanes and the series of operating conditions to thereby determine values for the one or more coefficients;
- and
- programming a controller with control logic, the control logic stored in one or more computer-readable storage media, the controller thereby configured to control a variable geometry compressor based on the fit non-linear model and engine operating information wherein the engine operating information comprises engine throttle position and engine rotational speed.
4 more elements
A controller for a variable geometry compressor comprising:
- one or more inputs for receiving engine operating information wherein the engine operating information comprises engine throttle position and engine rotational speed and for receiving a signal representative of geometry of a variable geometry compressor;
- and
- control logic to call for actuation of an actuator based at least in part on the engine operating information received by the one or more inputs and to call for actuation of the actuator based at least in part on the signal received by the one or more inputs whereby actuation of actuator causes a change in geometry of a variable geometry compressor, wherein the control logic comprises a non-linear model that calculates vane position of a variable geometry compressor based on a received engine rotational speed and a received engine throttle position, wherein the non-linear model comprises coefficients and wherein a statistical analysis of data determines a value for each of the coefficients.
A controller for a variable geometry compressor comprising:
- one or more inputs for receiving engine operating information wherein the engine operating information comprises engine throttle position and engine rotational speed;
- an actuator;
- a sensor for sensing, directly or indirectly, geometry of a variable geometry compressor;
- and
- control logic, configured to operate according to a non-linear model based on a received engine throttle position and a received engine rotational speed, to actuate the actuator based at least in part on the engine operating information received by the one or more inputs and to actuate the actuator based at least in part on geometry sensed by the sensor whereby actuation of actuator causes a change in geometry of a variable geometry compressor wherein the non-linear model comprises coefficients and wherein a statistical analysis of data determines a value for each of the coefficients.
2 more elements
One or more computer-readable media comprising instructions executable by a processor to perform control logic for controlling a variable geometry compressor comprising, the control logic configured:
- to call for actuation of an actuator based at least in part on engine operating information received by one or more inputs and
- to call for actuation of the actuator based at least in part on a received signal representative of geometry of a variable geometry compressor whereby actuation of actuator causes a change in geometry of the variable geometry compressor,
- wherein the control logic comprises a non-linear model that calculates vane position of a variable geometry compressor based on a received engine rotational speed and a received engine throttle position,
- wherein the non-linear model comprises coefficients and
- wherein a statistical analysis of data determines a value for each of the coefficients.
2 more elements
A compressor for an internal combustion engine comprising:
- a variable geometry diffuser section;
- one or more inputs for receiving engine operating information wherein the one or more inputs receive engine rotational speed and engine throttle position;
- an actuator;
- and
- control logic to control the actuator based at least in part on the engine operating information to thereby vary the geometry of the diffuser section wherein the control logic comprises a non-linear model for calculation of geometry of the diffuser section based at least in part on a received engine rotational speed and a received engine throttle position wherein the non-linear model comprises coefficients and wherein a statistical analysis of data determines a value for each of the coefficients.
2 more elements
A turbocharger having a compressor, the compressor comprising:
- a variable geometry diffuser section;
- one or more inputs for receiving engine operating information wherein the one or more inputs receive engine rotational speed and engine throttle position;
- an actuator;
- and
- control logic to control the actuator based at least in part on the engine operating information to thereby vary the geometry of the diffuser section wherein the control logic comprises a non-linear model for calculation of geometry of the diffuser section based at least in part on a received engine rotational speed and a received engine throttle position wherein the non-linear model comprises coefficients and wherein a statistical analysis of data determines a value for each of the coefficients.
2 more elements
Dependencies are inferred from the claim text.