Segmented compressor inner band for variable vanes in gas turbine engines
US-2024280032-A1 · Aug 22, 2024 · US
US9353643B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9353643-B2 |
| Application number | US-73324207-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 10, 2007 |
| Priority date | Apr 10, 2007 |
| Publication date | May 31, 2016 |
| Grant date | May 31, 2016 |
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Official abstract text for this publication.
A stator assembly for a turbine engine includes a support structure, such as an outer case, providing a bore. A non-metallic bushing is arranged in the bore and extends radially between inner and outer diameters providing a one-piece structure. The outer diameter of the bushing engages the bore in a press-fit relationship, in one example. A stator includes a trunnion arranged within and engaging the bushing inner diameter. In one example, the non-metallic bushing is constructed from an electrographitic carbon. The bushing is installed into the bore such that an end of the bushing is generally flush with or recessed from a wall on the support structure.
Opening claim text (preview).
What is claimed is: 1. A stator assembly for a turbine engine comprising: an outer case providing a bore; a non-metallic bushing arranged in the bore in an interference fit relationship and extending radially between inner and outer diameters, the outer diameter engaging the bore; a stator including a trunnion arranged within and engaging the bushing inner diameter; wherein the trunnion is an outer trunnion received within the bore; wherein the outer case provides a boss having the bore and extending away from the stator in an axial direction of the bore; and wherein the outer case provides a recess defining a wall surface, and the bore extends radially outwardly from the recess of the outer case. 2. The stator assembly according to claim 1 , wherein a chamfer is provided in the outer case and extends between the recess and the bore, the recess arranged on an inner side of the outer case and opposite the boss. 3. The stator assembly according to claim 2 , wherein the non-metallic bushing includes an inner end that is flush with an intersection between the chamfer and the bore, the inner end recessed from the wall surface, and the non-metallic bushing includes an outer end opposite the inner end and recessed into the bore. 4. The stator assembly according to claim 3 , wherein the non-metallic bushing is cylindrical in shape with a uniform diametral cross-section, the non-metallic bushing arranged entirely within the bore. 5. The stator assembly according to claim 1 , wherein the non-metallic bushing is constructed from an electrographitic carbon. 6. A stator assembly for a turbine engine comprising: an outer case providing a bore; a non-metallic bushing arranged in the bore in an interference fit relationship and extending radially between inner and outer diameters, the outer diameter engaging the bore; and a stator including a trunnion arranged within and engaging the bushing inner diameter wherein the non-metallic bushing is cylindrical in shape with a uniform diametral cross-section. 7. The stator assembly according to claim 6 , wherein the non-metallic bushing is constructed from an electrographitic carbon.
by a press fit connection · CPC title
Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles · CPC title
for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title
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