Exhaust gas variable turbine assembly
An exhaust gas variable geometry turbine assembly can include a number of pivotable vanes that define throats within an exhaust gas nozzle where each of the pivotable vanes includes a corresponding post, where each of the pivotable vanes is made of a first alloy that includes a first amount of nickel by mass, where each of the corresponding posts is made of a second alloy that includes a second amount of nickel by mass and where the second amount of nickel by mass exceeds the first amount of nickel by mass.
1. An exhaust gas variable geometry turbine assembly comprising:
an actuator;
vane control arms operatively coupled to the actuator;
a shroud component that comprises an inner perimeter, an outer perimeter and a shroud component surface that extends from the inner perimeter to the outer perimeter;
an annular component made from an alloy that comprises nickel wherein the annular component comprises an inner perimeter, an outer perimeter, an annular component surface that extends from the inner perimeter to the outer perimeter, a number of bore openings disposed in the annular component surface and a corresponding number of bores wherein each of the bore openings comprises a bore surface;
at least one spacer that defines a nozzle height of an exhaust gas nozzle defined by a planar portion of the shroud component surface and a planar portion of the annular component surface; and
a number of pivotable vanes that define throats within the exhaust gas nozzle wherein each of the pivotable vanes comprises a corresponding post portion that comprises a bushing that is received at least in part by a corresponding one of the bores of the annular component and contacts a corresponding bore surface wherein each of the pivotable vanes couples to a corresponding one the vane control arms for pivoting thereof responsive to force applied by the actuator, wherein each of the pivotable vanes comprises a first alloy that comprises a first amount of nickel by mass that is greater than 18 percent nickel by mass and less than 30 percent nickel by mass, wherein each of the corresponding bushings comprises a second alloy that reduces susceptibility to sticking between the bushings and the bore surfaces and that comprises a second amount of nickel by mass that is greater than 40 percent nickel by mass, and wherein each of the bushings is fixed to a corresponding one of the pivotable vanes.
2. The exhaust gas variable geometry turbine assembly of claim 1 wherein the first alloy comprises at least 50 percent iron by mass.
3. The exhaust gas variable geometry turbine assembly of claim 1 wherein each of the bushings comprises a key or a keyway that operatively engages a keyway or a key of the post portion of a corresponding one of the pivotable vanes.
4. An exhaust gas variable geometry turbine assembly comprising:
a shroud component that comprises an inner perimeter, an outer perimeter and a shroud component surface that extends from the inner perimeter to the outer perimeter;
an annular component made from an alloy that comprises nickel wherein the annular component comprises an inner perimeter, an outer perimeter, an annular component surface that extends from the inner perimeter to the outer perimeter, a number of bore openings disposed in the annular component surface and a corresponding number of bores;
at least one spacer that defines a nozzle height of an exhaust gas nozzle defined by a planar portion of the shroud component surface and a planar portion of the annular component surface;
a number of pivotable vanes that define throats within the exhaust gas nozzle; and
a number of bushings wherein each of the bushings is operatively coupled to the annular component and disposed in a respective one of the bores of the annular component, wherein each of the pivotable vanes comprises a corresponding post that is received at least in part by a corresponding one of the bushings, wherein each of the pivotable vanes comprises a first alloy that comprises a first amount of nickel by mass that is greater than 18 percent nickel by mass and less than 30 percent nickel by mass, and wherein each of the corresponding bushings comprises a second alloy that reduces susceptibility to sticking between the bushings and the posts and that comprises a second amount of nickel by mass that is greater than 40 percent nickel by mass.