Thermally compensated synchronization ring of a variable stator vane assembly
A variable vane assembly including a variable stator vane disposed in a main flow gaspath, the variable stator vane having a vane stem. The assembly also includes a case located at a radially outward location of the variable stator vane, the vane stem extending through a port of the case, the port defined by a port wall, a clearance defined by the vane stem and a port wall to allow gas from the main flow gaspath to pass therethrough. The assembly further includes a synchronization ring spaced from the case to define a gap. The assembly yet further includes a vane arm operatively coupled to a synchronization ring and to the vane stem, the vane arm redirecting gas from the main flow gaspath to the synchronization ring.
1. A variable vane assembly comprising:
a variable stator vane disposed in a main flow gaspath, the variable stator vane having a vane stem;
a case located at a radially outward location of the variable stator vane, the vane stem extending through a port of the case, the port defined by a port wall, a clearance defined by the vane stem and a port wall to allow gas from the main flow gaspath to pass therethrough;
a synchronization ring spaced from the case to define a gap; and
a vane arm operatively coupled to the synchronization ring and to the vane stem, the vane arm having at least one channel to redirect gas from the main flow gaspath to the synchronization ring.
2. The variable vane assembly of claim 1 , wherein the variable stator vane is a buttonless stator vane.
3. The variable vane assembly of claim 1 , wherein the gas redirected to the synchronization ring reduces a temperature difference between the synchronization ring and the case.
4. The variable vane assembly of claim 1 , the case comprising a bumper pad extending radially outwardly from the case, the synchronization ring axially aligned with the bumper pad.
5. The variable vane assembly of claim 1 , further comprising a bushing disposed within the port of the case.
6. The variable vane assembly of claim 5 , wherein the bushing is press fit to the port wall.
7. A variable vane assembly comprising:
a case at least partially defining a main flow gaspath;
a synchronization ring radially spaced from the case to define a gap therebetween;
a plurality of variable stator vanes disposed in the main flow gaspath and circumferentially spaced from each other; and
a plurality of vane arms, each of the vane arms operatively coupled to the synchronization ring and to one of the plurality of variable stator vanes, each of the variable stator vanes having a vane stem extending through a port of the case, the port defined by a port wall, a clearance defined by the vane stem and a port wall to allow gas from the main flow gaspath to pass therethrough, wherein at least one of the plurality of vane arms having at least one channel to redirect gas from the main flow gaspath to the synchronization ring.
8. The variable vane assembly of claim 7 , wherein the vane arm is shaped to redirect gas from the main flow gaspath to the synchronization ring.
9. The variable vane assembly of claim 7 , wherein the variable stator vane is a buttonless stator vane.
10. The variable vane assembly of claim 7 , wherein the gas redirected to the synchronization ring reduces a temperature difference between the synchronization ring and the case.
11. The variable vane assembly of claim 7 , the case comprising a bumper pad extending radially outwardly from the case, the synchronization ring axially aligned with the bumper pad.
12. The variable vane assembly of claim 7 , further comprising a bushing disposed within the port of the case.
13. The variable vane assembly of claim 12 , wherein the bushing is press fit to the port wall.
14. A gas turbine engine comprising:
a compressor section;
a combustor section;
a turbine section; and
a variable vane assembly comprising:
a case at least partially defining a main flow gaspath;
a synchronization ring radially spaced from the case to define a gap therebetween, the case comprising a bumper pad extending radially outwardly from the case, the synchronization ring axially aligned with the bumper pad;
a buttonless stator vane disposed in the main flow gaspath and circumferentially spaced from each other; and
a vane arm operatively coupled to the synchronization ring and to the buttonless stator vane, the buttonless stator vane having a vane stem extending through a port of the case, the port defined by a port wall, a clearance defined by the vane stem and a port wall to allow gas from the main flow gaspath to pass therethrough, the vane arm having at least one channel to redirect gas from the main flow gaspath to the synchronization ring.
15. The gas turbine engine of claim 14 , wherein the gas redirected to the synchronization ring reduces a temperature difference between the synchronization ring and the case.
16. The gas turbine engine of claim 14 , wherein the variable vane assembly is located proximate an inlet of the compressor section.
17. The gas turbine engine of claim 14 , further comprising a bushing disposed within the port of the case.