Centrifugal compressor assembly for use in a turbine engine and method of assembly
US-10113556-B2 · Oct 30, 2018 · US
US10704560B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10704560-B2 |
| Application number | US-201816007647-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 13, 2018 |
| Priority date | Jun 13, 2018 |
| Publication date | Jul 7, 2020 |
| Grant date | Jul 7, 2020 |
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A centrifugal impeller shroud assembly has a dynamically moveable impeller shroud for encasing a rotatable centrifugal impeller and resolving misalignment between the impeller shroud and the rotatable centrifugal impeller. The assembly comprises a static casing, an impeller shroud, a shroud arm, and a thermal member. The shroud arm is coupled between the casing and the impeller shroud. The thermal member is coupled to the impeller shroud and has a coefficient of thermal expansion (CTE) lower than the CTE of the shroud. The shroud arm comprises a flexible portion configured to flex responsive to a differential pressure across the shroud arm.
Opening claim text (preview).
What is claimed is: 1. A centrifugal impeller shroud assembly having a dynamically moveable impeller shroud for encasing a rotatable centrifugal impeller and resolving misalignment between the impeller shroud and the rotatable centrifugal impeller, said assembly comprising: a static casing; an impeller shroud facing the rotatable centrifugal impeller and extending from an inlet to an outlet; a shroud arm coupled between the casing and the impeller shroud, the shroud arm comprising a flexible portion, the shroud arm and impeller shroud at least partially defining a first cavity in fluid communication with the inlet and a second cavity in fluid communication with the outlet, the flexible portion being configured to flex responsive to a differential pressure between the first cavity and the second cavity; and a thermal member coupled to the impeller shroud proximate the outlet, the thermal member having a coefficient of thermal expansion (CTE) lower than the CTE of the shroud. 2. The impeller shroud assembly of claim 1 wherein flexion of said flexible portion of the shroud arm effects axial movement of the impeller shroud. 3. The impeller shroud assembly of claim 1 wherein said flexible portion of the shroud arm comprises a U-shaped cross section when viewed normal to an axis of rotation of the centrifugal impeller, wherein a concave surface of the U-shaped cross section is in communication with the second cavity. 4. The impeller shroud assembly of claim 1 wherein said shroud arm is coupled to the impeller shroud at a knee of the shroud. 5. The impeller shroud assembly of claim 1 wherein said second cavity is exposed to fluid at the impeller discharge pressure. 6. The impeller shroud assembly of claim 1 wherein said first cavity is exposed to fluid at the impeller inlet pressure. 7. The impeller shroud assembly of claim 1 wherein the thermal member effects deflection of the shroud proximate the outlet, said deflection responsive to changes in temperature. 8. The impeller shroud assembly of claim 7 wherein movement and deflection of the shroud resolves misalignment between the shroud and the centrifugal impeller. 9. The impeller shroud assembly of claim 1 wherein the thermal member has a CTE substantially the same as the CTE of the centrifugal impeller. 10. The impeller shroud assembly of claim 1 further comprising a static member positioned to limit aft movement of the shroud. 11. A centrifugal impeller shroud assembly having a dynamically moveable impeller shroud for encasing a rotatable centrifugal impeller and resolving misalignment between the shroud and the rotatable centrifugal impeller, said assembly comprising: a shroud extending between a forward end proximate an inlet and an aft end proximate an outlet; a thermal member coupled to said shroud proximate the aft end of the shroud, the thermal member comprising a material having a lower coefficient of thermal expansion (CTE) than the material of said shroud to thereby effect deflection of the aft end of the shroud responsive to changes in temperature; and a shroud arm coupled between the shroud and a static casing, the shroud arm comprising a flexible portion that flexes responsive to a pressure differential across said shroud arm to thereby effect axial movement of the shroud responsive to changes in the differential pressure across said shroud arm. 12. The impeller shroud assembly of claim 11 wherein said shroud comprises an impeller-facing member and a coupling member extending forward from said impeller-facing member, the thermal member being coupled to the shroud via the coupling member. 13. The impeller shroud assembly of claim 11 further comprising a static member positioned to limit aft movement of said aft end of the shroud. 14. The impeller shroud assembly of claim 11 wherein the thermal member comprises one or more of nickel alloy, Inconel, titanium, or low-a steel. 15. The impeller shroud assembly of claim 11 wherein the shroud arm is coupled to the shroud approximate a midpoint between the forward end and the aft end. 16. The impeller shroud assembly of claim 11 wherein said flexible portion of the shroud arm comprises a U-shaped cross section when viewed normal to an axis of rotation of the centrifugal impeller. 17. The impeller shroud assembly of claim 11 wherein movement and deflection of the shroud resolves misalignment between the shroud and the centrifugal impeller. 18. A method of dynamically changing the shape of a shroud encasing a centrifugal impeller, the shroud comprising a boundary member extending from an inlet end to a discharge end, the method comprising: deflecting the discharge end of the boundary member responsive to changes in the temperature of the fluid at the discharge end by mounting a thermal member to the shroud proximate the discharge end of the boundary member, the thermal member comprising a material having a coefficient of thermal expansion (CTE) that is lower than the CTE of the boundary member; and axially moving a knee portion of the boundary member responsive to changes in the differential pressure between the fluid at the inlet end and the fluid at the discharge end of the boundary member by coupling the shroud to a static casing via a shroud arm, the shroud arm having a flexible portion configured to flex responsive to a differential pressure between the inlet end and the discharge end of the boundary member. 19. The method of claim 18 comprising selecting the material of the thermal member to thereby effect thermal deflection of the discharge end of the boundary member in a manner similar to the thermal expansion of the discharge end of the centrifugal impeller during operation of the centrifugal impeller. 20. The method of claim 18 comprising selecting the flexion of the flexible portion of the shroud arm to thereby effect axial movement of the knee portion of the boundary member in a similar manner to the axial movement of the centrifugal impeller responsive to changes in the differential pressure from the inlet end to the discharge end of the centrifugal impeller during operation of the centrifugal impeller.
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