Guide vane assembly

Patent metadata

Field	Value
Publication number	US-12392250-B2
Application number	US-202418909133-A
Country	US
Kind code	B2
Filing date	Oct 8, 2024
Priority date	Oct 26, 2023
Publication date	Aug 19, 2025
Grant date	Aug 19, 2025

Abstract

A guide vane assembly includes a guide vane and a sealing assembly slidable along a span of the guide vane relative to the guide vane and extending along a chordal axis and the span of the guide vane. The sealing assembly includes a plate configured to be disposed around at least a portion of an external surface of the guide vane. The sealing assembly further includes a manifold coupled to the plate and configured to receive pressurized fluid therein. The manifold is disposed around the plate. The sealing assembly further includes a plurality of flow tubes extending between the manifold and the plate. Each of the plurality of flow tubes are configured to receive the pressurized fluid from the manifold.

First claim

The invention claimed is:

1. A guide vane assembly comprising:
a guide vane including an aerofoil including a leading edge, a trailing edge, a suction surface, a pressure surface, a root, and a tip, the aerofoil defining a chordal axis of the guide vane between the leading edge and the trailing edge, the aerofoil further defining a span of the guide vane between the root and the tip, the pressure surface and the suction surface together defining an external surface of the guide vane; and
a sealing assembly slidable along the span of the guide vane relative to the guide vane and extending along the chordal axis and the span of the guide vane, the sealing assembly including:
a plate configured to be disposed around at least a portion of the external surface of the guide vane, wherein the plate is spaced apart from the external surface of the guide vane to define a clearance therebetween, wherein the plate defines a plurality of openings extending therethrough, and wherein each of the plurality of openings is in fluid communication with the clearance between the plate and the guide vane;
a manifold coupled to the plate and configured to receive pressurized fluid therein, wherein the manifold is disposed around the plate; and
a plurality of flow tubes extending between the manifold and the plate, wherein each of the plurality of flow tubes defines a flow passage that is in fluid communication with a corresponding one of the openings in the plate, wherein each of the plurality of flow tubes are configured to receive the pressurized fluid from the manifold, and wherein each opening in the plate receives the pressurized fluid from a corresponding flow tube of the plurality of flow tubes to direct a jet of pressurized fluid towards the external surface of the guide vane to seal the clearance between the plate and the guide vane.

2. The guide vane assembly of claim 1 , wherein a width of the sealing assembly parallel to the span is less than a span length of the guide vane along the span, such that the sealing assembly divides the external surface of the guide vane between a flow region extending from the tip and an intended non-flowing region extending from the root, wherein the sealing assembly is configured to prevent a leakage of fluid between the flow region and the intended non-flowing region, and wherein the sealing assembly is further configured to vary an area of the flow region by sliding along the span of the guide vane.

3. The guide vane assembly of claim 1 , further including an actuator operatively coupled to the sealing assembly, wherein the actuator is configured to slide the sealing assembly along the span of the guide vane relative to the guide vane.

4. The guide vane assembly of claim 1 , wherein at least some of the plurality of flow tubes include different average cross-sectional areas.

5. The guide vane assembly of claim 1 , wherein each of the plurality of flow tubes has a variable cross-sectional area.

6. The guide vane assembly of claim 1 , wherein at least some of the plurality of openings in the plate include different cross-sectional areas.

7. The guide vane assembly of claim 1 , wherein at least some of the plurality of flow tubes extend orthogonally relative to the plate of the sealing assembly.

8. The guide vane assembly of claim 1 , wherein at least some of the plurality of flow tubes extend obliquely relative to the plate of the sealing assembly.

9. A guide vane system comprising:
a circumferential array of guide vane assemblies of claim 1 ; and
an annular ring fixedly coupled to each guide vane assembly and including an annular chamber disposed in fluid communication with the manifold of the sealing assembly of each guide vane assembly, wherein the annular chamber is configured to receive the pressurized fluid and direct the pressurized fluid towards the manifold of the sealing assembly of each guide vane assembly.

10. The guide vane system of claim 9 , further comprising a pair of end plates coupled to the guide vane of each guide vane assembly, wherein the pair of end plates are spaced apart from each other along the span of the guide vane, and wherein the sealing assembly is slidable along the span of the guide vane between the pair of end plates.

11. A rotary machine comprising:
a rotor assembly including an upstream end and a downstream end; and
the guide vane system of claim 9 , wherein the annular chamber of the guide vane system is configured to receive the pressurized fluid from the upstream end or the downstream end of the rotor assembly.

12. The rotary machine of claim 11 , wherein the rotor assembly includes a compressor.

13. The rotary machine of claim 11 , wherein the guide vane system is disposed downstream of the rotor assembly.

14. The rotary machine of claim 11 , wherein the guide vane system is disposed upstream of the rotor assembly.

Assignees

• Rolls Royce Plc

Inventors

• Murray Christopher A
• Howarth Nicholas

Classifications

• F01D17/141

  by means of shiftable members or valves obturating part of the flow path · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F05D2240/24

  for turbines · CPC title

• F05D2240/55

  Seals · CPC title

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title