Adaptive variable geometry turbocharger strategy
AssigneeHoneywell International Inc.
InventorsAndrew C. Love, Gary Agnew, Baptiste Szczyrba
Life of this patent
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AssigneeHoneywell International Inc.
InventorsAndrew C. Love, Gary Agnew, Baptiste Szczyrba
Estimating the term…
A variable geometry turbocharger employs multiple vanes in the turbine inlet with a unison ring and integral cast wall in the turbine housing forming the nozzle walls. An actuator rotates the unison ring through a rack and pinion driven crank shaft to move the vanes through a range of vane positions that extends between a hard-stop closed position and a hard-stop open position, and that includes a reference position corresponding to a desired flow condition. A variable geometry turbine controller uses a sensor indicating the actuation position of the actuator to guide the operation of the vanes to the reference position. The controller intermittently directs the actuator to force the vanes to the hard-stop closed and hard-stop open positions, and uses sensor information from those positions to reestablish the reference-position information that the actuator uses to guide the actuation of the vanes.
A variable geometry turbine controller for operation with a variable geometry turbine including a variable geometry member located in an inlet of the turbine, an actuator operative through a range of actuation positions to move the variable geometry member through a first range of variable geometry member positions that extends between a hard-stop closed position and a hard-stop open position, and that includes a smaller, second range of variable geometry member positions intermediate the hard-stop closed position and the hard-stop open position corresponding to desired flow conditions, and a sensor configured for sensing actuation information indicating the actuation position of the actuator, comprising:
A method for controlling the operation of a variable geometry turbine that includes a variable geometry member located in an inlet of the turbine, an actuator configured to actuate the variable geometry member through a first range of variable geometry member positions that extends between a hard-stop closed position and a hard-stop open position and that includes a smaller, second range of variable geometry member positions corresponding to desired flow conditions, and a sensor device configured for sensing actuation information on the extent of actuator actuation, comprising:
A turbocharger including a variable geometry controller, the turbocharger including a variable geometry member located in an airway of the turbocharger, an actuator operative through a range of actuation positions to move the variable geometry member through a first range of variable geometry member positions that extends between a hard-stop closed position and a hard-stop open position, and that includes a smaller, second range of variable geometry member positions corresponding to desired flow conditions intermediate the hard-stop closed position and the hard-stop open position corresponding to desired flow conditions, and a sensor configured for sensing actuation information indicating the actuation position of the actuator, comprising:
An actuator for operation with a variable geometry turbine including a variable geometry member located in an inlet of the turbine, comprising:
Dependencies are inferred from the claim text.