Fluid-flow machine—blade with hybrid profile configuration

• US 9,394,794 B2
• Filed: 12/08/2011
• Issued: 07/19/2016
• Est. Priority Date: 12/08/2010
• Status: Active Grant

• Current Assignee: Rolls-Royce Deutschland Limited & Company KG (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce Deutschland Limited & Company KG (Rolls-Royce Holdings Plc)
• Inventors: Guemmer, Volker
• Primary Examiner(s): YOUNGER, SEAN JERRARD
• Application Number:
  US13/314,274
• Publication Number:
  US 20120148396A1
• Time in Patent Office: 1,685 Days
• Field of Search: 415/191, 416/91, 416/227.A, 416/227.R, 416/231.B, 416/231.R
• US Class Current: 1/1
• CPC Class Codes: F01D 5/145 Means for influencing boundary layers or secondary circulations for compressors F04D29/68
• CPC Class Codes: F01D 5/146 of blades with tandem configuration, split blades or slotted blades
• CPC Class Codes: F04D 29/324 Blades
• CPC Class Codes: F04D 29/384 characterised by form
• CPC Class Codes: F04D 29/544 Blade shapes
• CPC Class Codes: F04D 29/682 by fluid extraction
• CPC Class Codes: F04D 29/684 by fluid injection
• CPC Class Codes: F05D 2240/301 Cross-sectional characteristics
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A blade for use in a fluid-flow machine, where at least one of the meridional flow line profile sections MSLi and MSLo is provided at a distance of max. 35% of the main flow path width from the respective inner and outer main flow path boundaries. The blade has in at least parts of a central area a multi-profile configuration such that at least two partial profiles (7, 9, 10) arranged one behind the other in the flow direction are provided, of which each has substantially the shape of a blade profile, where a passage (8) is provided between each two partial profiles and is passed through by fluid from the blade pressure side to the blade suction side.

Claims

1. A blade of a rotor or stator row with hybrid profile configuration for use in a fluid-flow machine,

the blade being configured for positioning in a main flow path confined by an inner and an outer main flow path boundary and having a main flow path width W, where the blade is split in a direction of its blade height into an inner boundary area IRB (defined between the inner main flow path boundary HBi and a nearby inner meridional flow line profile section MSLi), an outer boundary area ARB (defined between the outer main flow path boundary HBo and a nearby outer meridional flow line profile section MSLo) and a central area ZB (defined between the inner meridional flow line profile section MSLi and the outer meridional flow line profile section MSLo), the blade also including a plurality of further meridional flow profile sections,

wherein at least one of the meridional flow line profile sections MSLi and MSLo is provided at a distance of max. 35% of the main flow path width from its associated main flow path boundary,

wherein the blade has in at least parts of the central area a multi-profile configuration such that at least two partial profiles arranged one behind the other in the flow direction are provided, of which each has substantially a blade profile shape,

wherein at least one passage is provided between each of the at least two partial profiles and is passed through by fluid from a blade pressure side to a blade suction side,

wherein the at least one passage has, along the blade height, a variable passage width d,

wherein a local value of the variable passage width d is measured by a smallest distance that can be determined by inscribing a circle between contours of the at least two partial profiles on a same radius from an axis of the fluid-flow machine,

wherein the variable passage width d along the blade height has a maximum value in at least one of the inner and outer boundary areas IRB and ARB,

wherein in at least one of the inner and outer boundary areas IRB and ARB, a changeover from the multi-profile configuration to a single-profile configuration is provided when viewing a blade profile section geometry in a direction of the main flow path boundary adjoining the respective boundary area (IRB or ARB) and the at least one passage ends at the point of changeover confined by a flank surface FF,

wherein the flank surface FF includes an edge SSFFK on the blade suction side,

wherein the flank surface FF includes an edge DSFFK on the blade pressure side and a distance greater than zero is provided between the pressure-side flank surface edge DSFFK and the nearest main flow path boundary,

wherein at least one of the boundary areas IRB and ARB is provided at a fixed blade end provided with a shroud or blade root;

wherein the multi-profile configuration includes an arrangement with at least two partial profiles,

wherein a meridional distance Am between a trailing edge of a partial profile and a leading edge of an adjacently arranged downstream partial profile is defined,

wherein the meridional distance Am in at least one part of the main flow path width is provided with negative values and thus adjacent partial profiles overlap in the meridional flow direction and form a duct-like flow passage between them,

wherein the overlap at least in a partial section of the blade increases towards the main flow path boundary of the respective blade end, and the trailing edge HKT1 of a front partial profile extends in the direction of the main flow path boundary of the respective blade end increasingly far downstream of a leading edge VKT2 of a rear partial profile, and

wherein at least one of the following;

a decreasing overlap is provided, starting from a point in the central area ZB of the blade and extending in a direction of at least one blade end up to the point of changeover from the multi-profile configuration to the single-profile configuration;

or the suction-side flank surface edge SSFFK is provided at the main flow path boundary nearest the suction-side flank surface edge SSFFK such that one of the plurality of further meridional flow profile sections of the blade includes a ledge in its suction-side course directly on the main flow path boundary nearest the suction-side flank surface edge SSFFK at a point upstream of or directly at at least one of the trailing edge of the partial profile or a trailing edge of the blade.

2. The blade of claim 1, wherein at least one of the meridional flow line profile sections MSLi and MSLo is provided at a distance of max. 20% of the main flow path width from its associated main flow path boundary.

3. The blade of claim 2, wherein, when viewing the blade along its blade height the changeover from the multi-profile configuration to the single-profile configuration is such that a profile contour of the single profile encloses the partial profiles of the multi-profile configuration and forms at least partially joint contour sections with the partial profiles of the multi-profile configuration and that when viewing the blade along its blade height the changeover from the multi-profile configuration to the single-profile configuration is such that at least one of the trailing edge and a leading edge of the partial profiles of the multi-profile arrangement projects beyond the profile contour of the single profile.

4. The blade of claim 3, wherein at least one of the flank surface edges SSFFK and DSFFK is provided substantially or exactly in one of the plurality of further meridional flow profile sections.

5. The blade of claim 4, wherein the suction-side flank surface edge SSFFK is at least partially provided at the main flow path boundary at or upstream of the trailing edge of the partial profile and that thus a single profile configuration is provided in the respective boundary area (IRB or ARB) only in one of the plurality of further meridional flow profile sections directly at the respective main flow path boundary.

6. The blade of claim 5, wherein at least one of the following applies:

at least one section of one of the flank surface edges DSFFK and SSFFK approaches in the flow direction a main flow path boundary and is thus inclined relative to the meridional flow line profile sections of the blade;

or that a course of the pressure-side flank surface edge DSFFK, when viewed in the flow direction,

a) includes a first section, in which the pressure-side flank surface edge DSFFK is substantially or exactly provided along one of the plurality of further meridional flow profile sections, and

b) includes a second section adjoining the first one in the flow direction, in which the pressure-side flank surface edge DSFFK is inclined relative to the meridional flow direction and thereby approaches the main flow path boundary adjoined by the boundary area IRB or ARB including the pressure-side flank surface edge DSFFK.

7. The blade of claim 6, wherein the flank surface FF is substantially or precisely provided as part of a conical surface whose axis of symmetry is defined by an axis of the fluid-flow machine, and the flank surface FF has an S-shaped course.

8. The blade of claim 7, wherein at least one of the following applies:

the pressure-side flank surface edge DSFFK starts in an immediate vicinity of or directly at at least one of the leading edge of the partial profile or a leading edge of the blade;

or the suction-side flank surface edge SSFFK starts in the immediate vicinity of or directly at the leading edge of at least one of the partial profile or the blade.

9. The blade of claim 8,

wherein a distribution of the passage width d/dmin=fkt (w/W) in the central area ZB assumes a minimum value, and the maximum value of the passage width is greater than the minimum value by at least a factor of 1.5, in accordance with dmax/dmin ≧

1.5.

10. The blade of claim 1, wherein, when viewing the blade along its blade height the changeover from the multi-profile configuration to the single-profile configuration is such that a profile contour of the single profile encloses the partial profiles of the multi-profile arrangement and forms at least partially joint contour sections with the partial profiles of the multi-profile arrangement and that when viewing the blade along its blade height the changeover from the multi-profile configuration to the single-profile configuration is such that at least one of the trailing edge and the leading edge of the partial profiles of the multi-profile arrangement projects beyond the profile contour of the single profile.

11. The blade of claim 10, wherein at least one of the flank surface edges SSFFK and DSFFK is provided substantially or exactly in one of the plurality of further meridional flow profile sections.

12. The blade of claim 11, wherein at least one of the following applies:

the suction-side flank surface edge SSFFK is at least partially closer to the main flow path boundary of the respective boundary area (IRB or ARB) than the pressure-side flank surface edge DSFFK, resulting in a course of the flank surface FF inclined relative to at least one of the circumferential direction u or the meridional direction m and—

in a flow direction—

to the main flow path boundary;

or that the suction-side flank surface edge SSFFK is at least partially provided at the main flow path boundary at or upstream of the trailing edge of the partial profile and that thus a single profile configuration is provided in the respective boundary area (IRB or ARB) only in one of the plurality of further meridional flow profile sections directly at the main flow path boundary.

13. The blade of claim 12, wherein at least one of the following applies:

at least one section of one of the flank surface edges DSFFK and SSFFK approaches in the flow direction a main flow path boundary and is thus inclined relative to the meridional flow line profile sections of the blade;

or that a course of the pressure-side flank surface edge DSFFK, when viewed in the flow direction,

a) includes a first section, in which the pressure-side flank surface edge DSFFK is substantially or exactly provided along one of the plurality of further meridional flow profile sections, and

b) includes a second section adjoining the first one in the flow direction, in which the pressure-side flank surface edge DSFFK is inclined relative to the meridional flow direction and thereby approaches the main flow path boundary adjoined by the boundary area IRB or ARB including the pressure-side flank surface edge DSFFK.

14. The blade of claim 13, wherein the flank surface FF is substantially or precisely provided as part of a conical surface whose axis of symmetry is defined by an axis of the fluid-flow machine, and the flank surface FF has an S-shaped course.

15. The blade of claim 14, wherein at least one of the following applies:

the pressure-side flank surface edge DSFFK starts in the immediate vicinity of or directly at the leading edge of at least one of a partial profile or the blade;

or the suction-side flank surface edge SSFFK starts in the immediate vicinity of or directly at the leading edge of at least one of the partial profile or the blade.

16. The blade of claim 15, wherein a distribution of the passage width d/dmin=fkt (w/W) in the central area ZB assumes a minimum value, and the maximum value of the passage width is greater than the minimum value by at least a factor of 1.5, in accordance with dmax/dmin ≧

1.5.

17. The blade of claim 15,

wherein the suction-side flank surface edge SSFFK is at least partially closer to the main flow path boundary of the respective boundary area (IRB or ARB) than the pressure-side flank surface edge DSFFK, resulting in a course of the flank surface FF inclined relative to at least one of the circumferential direction u or the meridional direction m and—

in a flow direction—

to the main flow path boundary of the respective boundary area,

the flank surface FF mainly facing away from whichever of a radially inner or a radially outer end of the blade that the flank surface FF is located nearest to.

18. The blade of claim 1, wherein a distribution of the passage width d/dmin=fkt (w/W) in the central area ZB assumes a minimum value, and the maximum value of the passage width is greater than the minimum value by at least a factor of 1.5, in accordance with dmax/dmin ≧

1.5.

19. The blade of claim 18,

wherein the suction-side flank surface edge SSFFK is at least partially closer to the main flow path boundary of the respective boundary area (IRB or ARB) than the pressure-side flank surface edge DSFFK, resulting in a course of the flank surface FF inclined relative to at least one of the circumferential direction u or the meridional direction m and—

in a flow direction—

to the main flow path boundary of the respective boundary area,

the flank surface FF mainly facing away from whichever of a radially inner or a radially outer end of the blade that the flank surface FF is located nearest to.

20. The blade of claim 1,

wherein the suction-side flank surface edge SSFFK is at least partially closer to the main flow path boundary of the respective boundary area (IRB or ARB) than the pressure-side flank surface edge DSFFK, resulting in a course of the flank surface FF inclined relative to at least one of the circumferential direction u or the meridional direction m and—

in a flow direction—

to the main flow path boundary, of the respective boundary area

the flank surface FF mainly facing away from whichever of a radially inner or a radially outer end of the blade that the flank surface FF is located nearest to.