Stator device for a continuous-flow machine with a housing appliance and multiple guide vanes

Patent metadata

Field	Value
Publication number	US-10344616-B2
Application number	US-201615192417-A
Country	US
Kind code	B2
Filing date	Jun 24, 2016
Priority date	Jun 25, 2015
Publication date	Jul 9, 2019
Grant date	Jul 9, 2019

Abstract

A stator device for a continuous-flow machine with guide vanes circumferentially distributed on a housing. The guide vanes are respectively embodied with a blade leaf and at least one platform. The platforms form a surface of an annular channel through which working fluid flows. A flow area is provided via which, during operation of the stator device, a working fluid flows on a side of the platform that is facing away from the annular channel from a pressure side of the blade leaf to a suction side of the blade leaf at least in certain areas in the radial direction of the stator device. At least one suction appliance is provided which adjoins the flow area and is formed by a recess, and via which working fluid can be conducted out of the flow area during operation of the stator device.

First claim

The invention claimed is:

1. A stator device for a continuous-flow machine with a housing appliance and a plurality of guide vanes that are arranged in a circumferentially distributed manner at the housing appliance,
wherein each of the plurality of guide vanes includes a blade with a pressure side and a suction side and a platform,
wherein the platform, at least in certain areas, forms a surface of an annular channel through which working fluid flows during operation of the stator device, and is mounted so as to be adjustable with respect to the housing appliance, and
wherein a flow area is provided via which a working fluid flows during operation of the stator device at least in certain areas in a radial direction of the stator device on a side of the platform that is facing away from the annular channel from the pressure side of the blade to the suction side of the blade,
wherein the flow area is formed by a gap extending circumferentially about a central axis of a spindle-shaped area of the platform in a radial direction of the each of the plurality of guide vanes between the platform and the housing appliance in the area of the surface of the annular channel, with the gap extending outwards from the surface of the annular channel in an axial direction of the central axis, and by a distance between a surface of the platform that is facing away from the annular channel in the radial direction of the stator device with respect to the housing appliance;
a suction appliance which adjoins the flow area and is formed by a recess, and via which working fluid can be conducted out of the flow area during operation of the stator device;
wherein the suction appliance is connected to the flow area to conduct working fluid out of the stator device for all adjustment positions of the platform.

2. The stator device according to claim 1 , wherein the suction appliance directly adjoins the surface of the annular channel.

3. The stator device according to claim 1 , wherein the suction appliance adjoins the flow area at a distance to the surface of the annular channel in the radial direction of the stator device.

4. The stator device according to claim 1 , wherein the suction appliance extends substantially in the radial direction of the stator device.

5. The stator device according to claim 1 , wherein the suction appliance is connected to the flow area in an area that is facing towards the pressure side of the blade.

6. The stator device according to claim 1 , wherein the suction appliance extends in the circumferential direction of the each of the plurality of guide vanes across an angular range that is larger than 20°.

7. The stator device according to claim 1 , wherein the suction appliance extends inside the housing appliance so as to substantially run along the circumference with respect to the central axis.

8. The stator device according to claim 1 , wherein the housing appliance includes a recess that adjoins the annular channel in the area of the each of the plurality of guide vanes.

9. The stator device according to claim 1 , wherein the platform is arranged in an axial direction of the stator device between two reference points of the annular channel, wherein a first reference point represents a boundary point of the annular channel, which is arranged upstream of a front end of the platform by 10% of an axial extension of the platform with respect to the central axis, and wherein a second reference point represents a boundary point of the annular channel, which is arranged downstream of a rear end of the platform by 10% of the axial extension of the platform with respect to the central axis, wherein an edge area of the platform projects into the annular channel with respect to a rectilinear connection of the two reference points in the radial direction of the stator device.

10. The stator device according to claim 9 , wherein the edge area of the platform that projects into the annular channel with respect to the rectilinear connection of the two reference points is located in a front area of the platform in the axial direction of the stator device.

11. The stator device according to claim 9 , wherein the edge area of the platform that projects into the annular channel extends into the annular channel by at least 0.3% of an extension of the annular channel with respect to a rectilinear connection of the reference points in the radial direction of the stator device in the area of the edge area of the platform.

12. The stator device according to claim 9 , wherein the edge area of the platform that projects into the annular channel is rounded in a front or rear area in the axial direction of the stator device, wherein the edge area of the platform that projects into the annular channel includes a projection, and wherein the platform has a larger extension in the axial direction of the stator device in an area that is facing towards the annular channel than in an area that is facing away from the annular channel, wherein the projection overlaps the housing appliance that adjoins the platform in the axial direction of the stator device at least in certain areas.

13. The stator device according to claim 9 , wherein the edge area of the platform that projects into the annular channel with respect to the rectilinear connection of the two reference points is located in a rear area of the platform in the axial direction of the stator device.

14. The stator device according to claim 9 , wherein the edge area of the platform that projects into the annular channel extends into the annular channel by at least 0.8% of an extension of the annular channel with respect to a rectilinear connection of the reference points in the radial direction of the stator device in the area of the edge area of the platform.

15. The stator device according to claim 1 , wherein the platform is arranged in an inner edge area of the blade with respect to the radial direction of the stator device.

16. A blade wheel device with a stator device according to claim 1 and a rotor device, wherein the suction appliance is connected to a conduit area via which working fluid can be supplied to the rotor device during operation of the blade wheel device.

17. The blade wheel device according to claim 16 , wherein the conduit area has at least one nozzle via which the working fluid can be supplied to the rotor device during operation of the blade wheel device.

18. The stator device according to claim 1 , wherein the suction appliance is connected to the flow area in an area that is facing towards the suction side of the blade.

19. The stator device according to claim 1 , wherein the suction appliance extends in the circumferential direction of the each of the plurality of guide vanes across an angular range that is larger than 30°.

20. The stator device according to claim 1 , wherein the platform is arranged in an outer edge area of the blade with respect to the radial direction of the stator device.

Assignees

• Rolls Royce Deutschland Ltd & Co Kg

Inventors

• Grothe Patrick

Classifications

• F01D5/12

  Blades ({specially adapted for radial flow machines or engines F01D5/04}; blade roots F01D5/30; rotors with blades adjustable in operation F01D7/00; stator blades F01D9/02) · CPC title

• F01D17/162 Primary

  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

• F02C6/08

  the gas being bled from the gas-turbine compressor · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F01D9/041

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