Turbocharger variable-nozzle assembly with vane sealing arrangement
View Patent ↗A variable-nozzle assembly for a turbocharger includes a generally annular nozzle ring and an array of vanes rotatably mounted to the nozzle ring such that the vanes can be pivoted about their axes for regulating exhaust gas flow to the turbine wheel. A unison ring engages vane arms that are affixed to axles of the vanes, such that rotation of the unison ring causes the vanes to pivot between a closed position and an open position. The vanes have proximal ends that are adjacent a face of the nozzle ring. A vane sealing member is supported on the nozzle ring and has a portion disposed between the proximal ends of the vanes and the face of the nozzle ring. The unison ring includes cams that engage cam followers. Rotational movement of the unison ring causes the cam followers to be moved axially and thereby urge the vane sealing member against the proximal ends of the vanes.
1. A turbocharger having a variable-nozzle assembly, comprising:
a compressor housing and a compressor wheel mounted in the compressor housing and connected to a rotatable shaft, and a turbine housing and a turbine wheel mounted in the turbine housing and connected to the rotatable shaft, the turbine housing defining a chamber surrounding the turbine wheel for receiving exhaust gas from an engine and for supplying the exhaust gas through a nozzle leading from the chamber generally radially inwardly to the turbine wheel;
a nozzle ring having opposite first and second faces, the nozzle being defined between the second face and an opposite wall, the nozzle ring having a plurality of circumferentially spaced-apart bearing apertures each extending axially from the first face to the second face;
a plurality of vanes disposed in the nozzle and each having a proximal end and a distal end, the proximal ends of the vanes being proximate the second face of the nozzle ring, axles being joined to the proximal ends and being received into the bearing apertures of the nozzle ring and being rotatable in the bearing apertures, the vanes being rotatable between a closed position and an open position;
a plurality of vane arms adjacent the first face of the nozzle ring and respectively affixed rigidly to the axles, each vane arm having a free end;
a unison ring positioned generally coaxially with the nozzle ring with a face of the unison ring opposing the first face of the nozzle ring, the unison ring being engaged with the free ends of the vane arms and being rotatable about an axis of the nozzle ring so as to pivot the vane arms, thereby pivoting the vanes in unison, the unison ring being rotatable between a closed position corresponding to the closed position of the vanes and an open position corresponding to the open position of the vanes;
a vane sealing member having a portion disposed between the second face of the nozzle ring and the proximal ends of the vanes; and
a cam arrangement by which the unison ring engages the vane sealing member during rotation of the unison ring to the closed position, the cam arrangement being configured to move the vane sealing member in a first axial direction against the proximal ends of the vanes when the unison ring is moved to the closed position such that clearances between the vane sealing member and the proximal ends are reduced or eliminated, and being configured to allow the vane sealing member to move in a second axial direction opposite to the first axial direction when the unison ring is moved out of the closed position.
2. The turbocharger of claim 1 , wherein the cam arrangement comprises a plurality of circumferentially spaced cams formed on the unison ring, each cam being sloped along a direction in which the cam moves when the unison ring is rotated to the closed position, the cam arrangement further comprising a plurality of cam followers, each cam follower having a first end that engages a respective one of the cams and an opposite second end that urges the vane sealing member in the first axial direction when the unison ring is rotated to the closed position.
3. The turbocharger of claim 2 , wherein the cam followers comprise integrally formed portions of the vane sealing member.
4. The turbocharger of claim 3 , wherein the vane sealing member is generally annular and has a radially inner edge and a radially outer edge, and wherein the cam followers comprise protrusions that extend from the radially outer edge, each protrusion having a portion that extends generally axially and terminates in an end configured for engaging a respective one of the cams.
5. The turbocharger of claim 4 , wherein the vane sealing member comprises a sheet metal part and the protrusions comprise sheet metal portions that are bent to form the portions that extend generally axially.
6. The turbocharger of claim 5 , wherein the ends of the protrusions define foot portions that are bent to extend generally perpendicular to the portions that extend generally axially, the foot portions engaging the cams of the unison ring.
7. The turbocharger of claim 2 , wherein the cam followers are formed separately from the vane sealing member.
8. The turbocharger of claim 7 , wherein the nozzle ring defines a plurality of bores extending axially therethrough, and the cam followers extend through the bores.
9. The turbocharger of claim 8 , wherein the cam followers comprise pins.
10. The turbocharger of claim 1 , wherein the vanes are free to move axially relative the nozzle ring, and the vane sealing member urges the vanes axially such that the distal ends of the vanes are pushed against the opposite wall of the nozzle when the unison ring is in the closed position such that clearances between the opposite wall and the distal ends are reduced or eliminated.