Granted Patent B2

US 10,947,861 · App. 15/905,098 · Granted Mar 16, 2021

Inventors: Arthur Jeanson (Chatel sur Moselle, FR); Philippe Arnold (Hennecourt, FR)

Assignee: GARRETT TRANSPORTATION I INC

F01D17/165F02B37/24F02C9/22F05D2220/40F05D2230/40F05D2230/41F05D2230/90F05D2250/90

Abstract

Claims (56)

1. A turbocharger system comprising:

a housing;

a wheel configured to rotate within the housing;

a variable vane mechanism configured to move between a first position and a second position to affect a gas stream relative to the wheel, the variable vane mechanism including:

a support ring with a first bearing surface, the first bearing surface being arcuate;

a continuous, one-piece unison ring that is supported for rotation about an axis of rotation relative to the support ring as the variable vane mechanism moves between the first position and the second position;

a plurality of vanes that are operatively connected to the unison ring and configured to move substantially synchronously relative to the support ring as the unison ring rotates relative to the support ring to affect the gas stream; and

at least one bearing member that is fixed to the unison ring and that includes a second bearing surface, the second bearing surface abutting the first bearing surface, the at least one bearing member supported for sliding movement on the first bearing surface to support rotation of the unison ring relative to the support ring, the bearing member abutting the support ring to support radial loads and axial loads between the unison ring and the support ring, the radial loads directed radially relative to the axis of rotation and the axial loads directed along the axis of rotation; and

the unison ring and the at least one bearing member having independent material characteristics, and the first bearing surface and the second bearing surface formed of the same material.

2. The turbocharger system of claim 1 , wherein the unison ring is coated with a heat treat coating; and

wherein the first bearing surface and the second bearing surface are free of the heat treat coating.

3. The turbocharger system of claim 2 , wherein the heat treat coating is a nitride coating.

4. The turbocharger system of claim 1 , wherein the at least one bearing member includes at least three bearing members;

wherein the unison ring and the at least three bearing members are configured to rotate about the axis of rotation relative to the support ring; and

wherein the at least three bearing members are spaced apart substantially equally about the axis of rotation.

5. The turbocharger system of claim 1 , wherein the bearing member is integrally attached to the unison ring.

6. The turbocharger system of claim 1 , wherein the unison ring is made from a first material and the at least one bearing member is made from a second material that is different from the first material.

7. The turbocharger system of claim 1 , wherein the variable vane mechanism further includes a plurality of arms;

wherein ones of the plurality of arms operatively connect corresponding ones of the plurality of vanes to the unison ring; and

wherein the plurality of vanes and the plurality of arms are configured to move substantially synchronously relative to the support ring as the variable vane mechanism moves between the first position and the second position.

8. The turbocharger system of claim 7 , wherein the unison ring and the plurality of arms are coated with a nitride coating; and

wherein the first bearing surface and the second bearing surface are free of the nitride coating.

9. The turbocharger system of claim 7 , wherein the unison ring includes a plurality of inner diameter notches; and

wherein ones of the plurality of inner diameter notches receive corresponding ones of the plurality of arms to interconnect the unison ring and the plurality of arms.

10. The turbocharger system of claim 1 , wherein the bearing member and the support ring are constructed from a common material;

wherein the unison ring is coated with a heat treat coating; and

wherein the first bearing surface and the second bearing surface are free of the heat treat coating.

11. The turbocharger system of claim 1 , wherein the first bearing surface defines a groove of the support ring; and

wherein the groove receives the bearing member.

12. The turbocharger system of claim 1 , wherein the bearing member includes at least one end that is fixed to the unison ring;

wherein the bearing member includes a raised portion that is raised from the at least one end and the unison ring; and

wherein the raised portion includes the second bearing surface.

13. The turbocharger system of claim 1 , wherein the bearing member includes at least one end that is fixed to the unison ring;

wherein the bearing member includes a raised portion that is raised from the unison ring, wherein the raised portion includes a radial projection that projects radially inward from the raised portion, and wherein the radial projection includes the second bearing surface.

14. A turbocharger system comprising:

a housing;

a wheel configured to rotate within the housing;

a variable vane mechanism configured to move between a first position and a second position to affect a gas stream relative to the wheel, the variable vane mechanism including:

a support ring with a first bearing surface, the first bearing surface being arcuate;

a unison ring that is supported for rotation relative to the support ring as the variable vane mechanism moves between the first position and the second position;

a plurality of vanes that are operatively connected to the unison ring and configured to move substantially synchronously relative to the support ring as the unison ring rotates relative to the support ring to affect the gas stream;

at least one bearing member that is fixed to the unison ring and that includes a second bearing surface, the second bearing surface abutting the first bearing surface and supported for sliding movement on the first bearing surface to support rotation of the unison ring relative to the support ring;

the unison ring and the at least one bearing member having independent material characteristics;

wherein the bearing member includes at least one end that is fixed to the unison ring;

wherein the bearing member includes a raised portion that is raised from the unison ring;

wherein the raised portion includes a radial projection that projects radially inward from the raised portion; and

wherein the radial projection includes the second bearing surface.

15. A method of manufacturing a variable vane mechanism of a turbocharger, the variable vane mechanism configured to move between a first position and a second position to affect a gas stream relative to a wheel of the turbocharger, the method comprising:

heat treating a continuous, one-piece unison ring of the variable vane mechanism to add a heat treat coating to the unison ring;

attaching the heat treated unison ring with an affixed bearing member to a support ring including abutting a first bearing surface of the support ring and a second bearing surface of the bearing member, the heat treated unison ring and the bearing member having independent material characteristics, the first bearing surface being annular and configured to support sliding movement of the second bearing surface on the first bearing surface, the unison ring supported for rotation about an axis of rotation relative to the support ring as the variable vane mechanism moves between the first position and the second position to substantially synchronously move a plurality of vanes of the variable vane mechanism, the bearing member abutting the support ring to support radial loads and axial loads between the unison ring and the support ring, the radial loads directed radially relative to the axis of rotation and the axial loads directed along the axis of rotation, the first bearing surface and the second bearing surface being free of the heat treat coating and formed of the same material.

16. The method of claim 15 , further comprising machining a groove in the support ring to form the first bearing surface in the support ring.

17. The method of claim 15 , wherein heat treating the unison ring includes nitriding the unison ring to add a nitride coating to the unison ring.

18. The method of claim 15 , further comprising integrally attaching the bearing member to the unison ring.

19. The method of claim 18 , wherein integrally attaching includes welding the bearing member to the unison ring.

20. The method of claim 15 , further comprising fixing at least one end of the bearing member to the unison ring such that a raised portion of the bearing member is raised from the unison ring and such that a radial projection of the bearing member projects radially inward from the raised portion; and

wherein the radial projection includes the second bearing surface.

Assignments (8)

Continuity (1)