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Improved actuation assemblies are used with variable geometry turbochargers comprising a plurality of movable aerodynamic vanes attached to a movable unison ring that is coupled to an actuator. The actuation assembly includes a crank arm that is attached at a first end to the actuator, and at a seco

Improved actuation assemblies are used with variable geometry turbochargers comprising a plurality of movable aerodynamic vanes attached to a movable unison ring that is coupled to an actuator. The actuation assembly includes a crank arm that is attached at a first end to the actuator, and at a second end to the unison ring. A first gear member is attached to the crank arm second end and includes teeth. The unison ring includes a second gear member attached thereto that also comprises teeth. The teeth of the first and second gear members are cooperatively engaged with one another. The second gear member is movably attached to the unison ring to maintain predetermined distance between the first and second gear members during operation of the turbocharger and related thermal movement of the unison ring.

대표청구항 ▼

1. A method for actuating a plurality of movable aerodynamic vanes within a variable geometry turbocharger, the method comprising the step of rotating a crank arm that is disposed within a turbine housing of the turbocharger, the crank arm having a first gear member attached at one of its ends that

1. A method for actuating a plurality of movable aerodynamic vanes within a variable geometry turbocharger, the method comprising the step of rotating a crank arm that is disposed within a turbine housing of the turbocharger, the crank arm having a first gear member attached at one of its ends that is engaged with a second gear member that is attached to a moving unison ring by cooperative surface features, the unison ring being disposed within the turbocharger, wherein the step of rotating the crank arm causes the unison ring to be rotated by the engagement of the first and second gear members, and wherein the unison ring is coupled to the plurality of aerodynamic vanes to move the vanes in unison.2. An actuation assembly for moving in unison a plurality of aerodynamic vanes disposed within a variable geometry turbocharger that includes an actuator coupled to a moving unison ring, the unison ring being disposed within a turbocharger turbine housing and attached to the plurality of aerodynamic vanes, the actuator comprising a crank arm rotatably disposed within the turbine housing and attached at a first end to the actuator and to a second end to the unison ring, wherein the crank arm second end includes a first gear member comprising teeth, and the unison ring includes a second gear member comprising teeth, wherein the teeth of the first and second gear members are cooperatively engaged with one another, and wherein the second gear member is coupled to the unison ring by cooperative surface features to permit unison ring thermal expansion and contraction movement during turbocharger operation while maintaining engagement between the first and second gear members.3. The actuation assembly as recited in claim 2 wherein the first gear member is a pinion gear and the second gear member is a rack gear.4. The actuation assembly as recited in claim 2 wherein the cooperative surface features comprise a tongue that cooperates within an opening, and wherein the tongue and opening are sized to permit thermal expansion and contraction movement between the unison ring and rack gear.5. The actuation assembly as recited in claim 4 wherein the tongue projects outwardly from the unison ring, and the opening is disposed within a surface of the rack gear.6. A turbocharger assembly comprising:a turbine housing;a turbine wheel carried within the turbine housing and attached to a shaft;a plurality of vanes pivotably disposed within the turbine housing;a moving unison ring attached to the plurality of vanes to move the vanes in unison with one another, the unison ring including a first gear member having teeth attached thereto;a crank arm disposed within the turbine for moving the unison ring, the crank arm including a second gear member at one of its ends and having teeth that are engaged with the teeth of the first gear member; andmeans for maintaining engagement between the first and second gear members during operation of the turbocharger, the means being cooperative surface features between the unison ring and the first gear member.7. The turbocharger assembly as recited in claim 6 wherein the first gear member is a rack gear and the second gear member is a pinion gear.8. The turbocharger assembly as recited in claim 6 wherein the cooperative attachment surface features comprise a tongue that projects from one of the unison ring and rack gear, into an opening of the other of the unison ring and rack gear.9. A turbocharger assembly comprising:a turbine housing;a turbine wheel carried within the turbine housing and attached to a shaft;a plurality of vanes pivotably disposed within the turbine housing;a moving unison ring attached to the plurality of vanes to move the vanes in unison with one another, the unison ring including a rack gear having teeth attached thereto;a crank arm disposed within the turbine for affecting movement of the unison ring, the crank arm including a pinion gear at one of its ends that has teeth that are engaged with the teeth of the rack gear;wherein the rack gear is attached to the unison ring by cooperative surface features to permit unison ring thermal movement during turbocharger operation while maintaining a desired tolerance between the pinion gear and rack gear.