Surface treatment for variable geometry turbine
View Patent ↗An exemplary vane fronting surface for a variable geometry turbine includes a white layer that comprises nitrides. Such a layer may be formed using gas nitriding. As described, trials demonstrate that such nitriding reduces friction between a vane fronting surface and vanes of a variable geometry turbine. Consequently, nitriding can enhance longevity and controllability of a variable geometry turbine.
1. A variable geometry exhaust turbine comprising:
a turbine housing;
a vane base;
a vane side space and a command side space defined in part by opposite sides of the vane base wherein a pressure differential forms between the vane side space and the command side space during operational transients;
a plurality of vanes set in the vane base wherein each vane comprises a post extending from the command side space to the vane side space, that defines a pivot axis, wherein the vane base receives each post to allow for pivoting of a vane about its pivot axis and wherein the pressure differential forms in a direction of the pivot axis; and
an insert positioned at least partially between the turbine housing and the vane base wherein the insert comprises a nitrided surface that fronts the plurality of vanes, wherein contact exists between the vanes and the nitride surface due to formation of the pressure differential during operational transients, wherein the contact and the pressure differential cause vane actuation hysteresis and wherein the nitrided surface of the insert reduces friction between the vanes and the insert and reduces the vane actuation hysteresis.
2. The variable geometry turbine of claim 1 wherein each vane comprises a lower surface adjacent the vane base and an upper surface fronting the nitrided surface of the insert.
3. The variable geometry turbine of claim 1 wherein gas nitriding creates the nitrided surface.
4. The variable geometry turbine of claim 3 wherein the gas nitriding comprises providing ammonia.
5. The variable geometry turbine of claim 1 wherein the nitrided surface withstands an exhaust gas temperature of 860° C.
6. The variable geometry turbine of claim 1 wherein the nitride surface comprises a thickness of approximately 25 μm.
7. The variable geometry turbine of claim 1 wherein the nitrided surface comprises a hardness that resists pitting from contact between the nitrided surface and the vanes.
8. The variable geometry turbine of claim 1 wherein the nitrided surface comprises a hardness that exceeds the hardness of a surface of the vanes.
9. The variable geometry turbine of claim 1 wherein the nitrided surface comprises less than the entire surface of the insert.
10. The variable geometry turbine of claim 1 wherein the insert is nitrided.
11. The variable geometry turbine of claim 1 wherein each vane comprises a nitrided surface.
12. The variable geometry turbine of claim 1 wherein the vane base comprises a nitrided surface.
13. A method of manufacturing a turbocharger comprising:
providing a turbine housing;
providing a vane base wherein opposite sides of the vane base define in part a vane side space and a command side space;
providing a plurality of vanes for setting in the vane base wherein each vane comprises a post extending from the command side space to the vane side space;
providing an insert for positioning at least partially between the turbine housing and the vane base;
nitriding a surface of the insert; and
assembling a turbocharger using the turbine housing, the vane base, the vanes and the insert wherein the nitrided surface of the insert fronts the plurality of vanes, wherein contact exists between the vanes and the nitride surface due to a pressure differential between the command side space and the vane side space during operational transients of the turbocharger, wherein the contact and the pressure differential cause vane actuation hysteresis, and wherein the nitrided surface reduces friction between the vanes and the insert and reduces the vane actuation hysteresis.