Information
-
Patent Grant
-
6786698
-
Patent Number
6,786,698
-
Date Filed
Thursday, December 19, 200222 years ago
-
Date Issued
Tuesday, September 7, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 416 189
- 416 191
- 416 193 A
-
International Classifications
-
Abstract
A turbine bucket is disclosed which includes a dovetail for mounting the bucket within the turbine, a parallelogram-shaped platform connected to the dovetail, a parallelogram-shaped shroud, and an airfoil connected between the platform and the shroud. The platform includes an inner flowpath surface at which a first end of the airfoil intersects with the platform the inner flowpath surface being parallelogram-shaped and formed from a first inclined plane and a second inclined plane that meet at a first common boundary and form a first ridge or valley, boundary bisecting the inner flowpath surface, the shroud including an outer flowpath surface at which the second end of the airfoil intersects the shroud, the outer flowpath surface being parallelogram-shaped and formed from a third inclined plane and a fourth inclined plane that meet at a second common boundary and form a second ridge or valley, second common boundary bisecting the outer flowpath surface.
Description
The present invention relates to steam turbine buckets, and in particular, to an improved steam turbine bucket flowpath design that eliminates flowpath steps between adjacent buckets.
BACKGROUND OF THE INVENTION
In a steam turbine (not shown), the turbine buckets are typically installed adjacent to one another circumferentially around a turbine wheel (also not shown).
FIG. 1
a
shows a stage
10
that includes a plurality of prior art buckets
12
as they would be mounted adjacent to one another around a portion of a turbine wheel. Each bucket
12
includes a dovetail
14
for mounting the buckets around the turbine wheel. To the outside of each dovetail
14
is a parallelogram-shaped platform
16
from which protrudes an airfoil
18
. Each airfoil
18
includes a pressure side
20
that is partially concave in shape and a suction side
22
that is convex in shape. To the outside of each airfoil
18
is a parallelogram-shaped shroud
24
.
Each bucket
12
's platform
16
includes a flat inner flowpath surface
26
at which one end
28
of the corresponding airfoil
18
intersects with platform
16
. Similarly, each bucket
12
's shroud
24
includes a second flat outer flowpath surface
30
(
FIG. 1
c
) at which the other end
32
of the corresponding airfoil
18
intersects with shroud
24
.
Adjacent buckets, such as buckets
12
a
and
12
b
shown in
FIG. 1
b
, form an inner flowpath
34
, which is established by adjacent inner flowpath surfaces
26
a
and
26
b
of adjacent platforms
16
a
and
16
b
, by way of example. Adjacent buckets also form an outer flowpath
36
, which is established by adjacent outer flowpath surfaces
30
a
and
30
b
of adjacent shrouds
24
a
and
24
b
of buckets
12
a
and
12
b
, again by way of example.
When buckets
12
are installed circumferentially around a turbine wheel, their airfoils
18
are each skewed with respect to the centerline (not shown) of the turbine. As they follow the circumference of the turbine wheel, airfoils
18
are staggered with respect to the centerline of the turbine. Each bucket
12
's platform
16
is then angled with respect to the centerline of the turbine to follow the stagger angle of the airfoils
18
around the turbine wheel. As such, as shown in
FIG. 1
b
, flowpath steps
38
in flowpath
34
are created between the platforms
16
of adjacent buckets, such as platforms
16
a
and
16
b
of buckets
12
a
and
12
b
, shown by way of example in
FIG. 1
b.
Similarly, each bucket
12
's shroud
24
is angled with respect to the centerline of the turbine to, again, follow the stagger angle of the airfoils
18
around the turbine wheel. Here again, as shown in
FIG. 1
c
, flowpath steps
40
are created in an outer flowpath
36
between the shrouds
24
of adjacent buckets, such as shrouds
24
a
and
24
b
of buckets
12
a
and
12
b
, again by way of example.
FIGS. 1
b
and
1
c
depict typical distinct steps in the flowpaths of prior art steam turbine buckets. These circumferential steps in a turbine's flowpath reduce the aerodynamic performance of the turbine. Advantageously, however, these prior art buckets can be manufactured using 3-axis milling machines that are not too expensive to buy or operate. In addition, manufacturing shops typically have 3-axis machines.
It should be noted that steam turbine buckets without flowpath steps can be made. Such buckets have inner and outer flowpath surfaces that are “surfaces of revolution” about the centerline of the turbine. However, these buckets can be made only with 5-axis milling machines that are much more expensive to buy and operate than 3-axis machines. Thus, it would be very desirable for a manufacturer of steam turbines to have the ability to make buckets with 3-axis milling machines and that do not form flowpath steps when mounted together around a turbine wheel.
BRIEF DESCRIPTION OF THE INVENTION
In an exemplary embodiment of the invention, a turbine bucket comprises a platform, a shroud, and an airfoil connected between the platform and the shroud, the platform including an inner flowpath surface at which the airfoil is connected to the platform, the inner flowpath surface being formed from a first inclined plane and a second inclined plane that meet at a first common boundary and form a first ridge or valley, the shroud including an outer flowpath surface at which the airfoil is connected to the shroud, the outer flowpath surface being formed from a third inclined plane and a inclined plane that meet at a second common boundary and form a second ridge or valley.
In another exemplary embodiment of the invention, a turbine bucket comprises a dovetail for mounting the bucket within the turbine, a platform connected to the dovetail, a shroud, and an airfoil connected between the platform and the shroud, the platform including an inner flowpath surface at which the airfoil is connected to the platform, the inner flowpath surface being formed from a first inclined plane and a second inclined plane that meet at a first common boundary and form a first ridge or valley, the shroud including an outer flowpath surface at which the airfoil is connected to the shroud, the outer flowpath surface being formed from a third inclined plane and a inclined plane that meet at a second common boundary and form a second ridge or valley, an inner flowpath being formed without steps by inner flowpath surface when it is positioned adjacent to a second inner flowpath surface of a second platform of a second bucket positioned adjacent to the bucket, and an outer flowpath being formed without steps by outer flowpath surface when it is positioned adjacent to a second outer flowpath surface adjacent of a second shroud of the second bucket positioned adjacent to the bucket.
In yet another exemplary embodiment of the invention, a turbine bucket comprises a dovetail for mounting the bucket within the turbine, a parallelogram-shaped platform connected to the dovetail, a parallelogram-shaped shroud, and an airfoil connected at a first end to the platform and at a second end to the shroud, the platform including an inner flowpath surface at which the first end of the airfoil intersects the platform, the inner flowpath surface being parallelogram-shaped and formed from a first triangular-shaped inclined plane and a second triangular-shaped inclined plane that meet at a first common boundary and form a first ridge or valley, the first common boundary bisecting the inner flowpath surface, the shroud including an outer flowpath surface at which the second end of the airfoil intersects the shroud, the outer flowpath surface being parallelogram-shaped and formed from a third triangular-shaped inclined plane and a fourth triangular-shaped inclined plane that meet at a second common boundary and form a second ridge or valley, the second common boundary bisecting the outer flowpath surface.
In a further exemplary embodiment of the invention, a stage of turbine buckets includes at least two buckets, each bucket comprises a dovetail for mounting the bucket within the turbine, a parallelogram-shaped platform connected to the dovetail, a parallelogram-shaped shroud, and an airfoil connected at a first end to the platform and at a second end to the shroud, the platform including an inner flowpath surface at which the first end of the airfoil intersects the platform, the inner flowpath surface being parallelogram-shaped and formed from a first triangular-shaped inclined plane and a second triangular-shaped inclined plane that meet at a first common boundary and form a first ridge or valley, the first common boundary bisecting the inner flowpath surface, the shroud including an outer flowpath surface at which the second end of the airfoil intersects the shroud, the outer flowpath surface being parallelogram-shaped and formed from a third triangular-shaped inclined plane and a fourth triangular-shaped inclined plane that meet at a second common boundary and form a second ridge or valley, the second common boundary bisecting the outer flowpath surface, an inner flowpath being formed without steps by adjacent inner flowpath surfaces when two of the plurality of platforms are positioned adjacent to one another, and an outer flowpath being formed without steps by adjacent outer flowpath surfaces when the two platforms are positioned adjacent to one another.
In yet a further exemplary embodiment of the invention, a turbine bucket flowpath comprises a first flowpath surface formed on a first platform or shroud of a first bucket, the flowpath surface being formed from a first inclined plane and a second inclined plane that meet at a first common boundary and form a first ridge or valley, the first common boundary bisecting the flowpath surface, and a second flowpath surface formed on a second platform or shroud of a second bucket, the second flowpath surface being formed from a third inclined plane and a fourth inclined plane that meet at a second common boundary and form a second ridge or valley, the second common boundary bisecting the second flowpath surface, the flowpath being formed by the second inclined plane of the bucket and the third inclined plane of the second bucket adjacent to the bucket, the second and third planes sharing a common flush edge at the interface between them.
In still a further exemplary embodiment of the invention, a inner turbine bucket flowpath comprises a first inner flowpath surface formed on a first parallelogram-shaped platform of a first bucket, the inner flowpath surface being formed from a first triangular-shaped inclined plane and a second triangular-shaped inclined plane that meet at a first common boundary and form a first ridge or valley, the first common boundary bisecting the inner flowpath surface, and a second inner flowpath surface formed on a second parallelogram-shaped platform of a second bucket, the inner flowpath surface being formed from a third triangular-shaped inclined plane and a fourth triangular-shaped inclined plane that meet and form a second ridge, which bisects the inner flowpath surface, the inner flowpath being formed by the second triangular-shaped inclined plane of the bucket and the first triangular-shaped inclined plane of the second bucket adjacent to the bucket, the first and second planes and sharing a common flush edge at the interface between them.
In still another exemplary embodiment of the invention, an outer turbine bucket flowpath comprises a first outer flowpath surface formed on a first parallelogram-shaped shroud of a first bucket, the outer flowpath surface being formed from a first triangular-shaped inclined plane and a second triangular-shaped inclined plane that meet at a first common boundary and form a first ridge or valley, the first common boundary bisecting the inner flowpath surface, and a second outer flowpath surface formed on a second parallelogram-shaped shroud of a second bucket, the outer flowpath surface being formed from a third triangular-shaped inclined plane and a fourth triangular-shaped inclined plane that meet at a second common boundary and form a second ridge or valley, the second common boundary bisecting the inner flowpath surface, the outer flowpath being formed by the second triangular-shaped inclined plane of the bucket and the third triangular-shaped inclined plane of the second bucket adjacent to the bucket, the second and third planes and sharing a common flush edge at the interface between them.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
a
is a perspective view of a stage of prior art buckets mounted adjacent to one another around a portion of a turbine wheel.
FIG. 1
b
is a partially enlarged perspective view of the inner portion of the stage of prior art buckets shown in
FIG. 1
a.
FIG. 1
c
is a partially enlarged perspective view of the outer portion of the stage of prior art buckets shown in
FIG. 1
a.
FIG. 2
a
is a partial perspective view of the inner portion of two buckets with an inner flowpath surface made according to the present invention.
FIG. 2
b
is a partial perspective view of the outer lower portion of two buckets with an outer flowpath surface made according to the present invention.
DETAILED DESCRIPTION OF THE INVENTION
FIGS. 2
a
and
2
b
each show a portion of two buckets
40
made according to the present invention. The buckets
40
are again oriented as they would be when mounted adjacent to one another around a turbine wheel. Each bucket
40
again includes a dovetail
14
like the dovetail
14
of the prior art bucket
12
for mounting the buckets
40
around the turbine wheel. To the outside of each dovetail
14
is a parallelogram-shaped platform
42
from which protrudes an airfoil
18
like the airfoil
18
of the prior art bucket
12
. Each airfoil
18
again includes a pressure side
20
and a suction side
22
like the prior art airfoil
18
. As shown in
FIG. 2
b
, to the outside of each airfoil
18
is a parallelogram-shaped shroud
44
.
Each bucket
40
's platform
42
includes an inner flowpath surface
46
at which one end
28
of the corresponding airfoil
18
intersects with platform
42
. Surface
46
is a parallelogram-shaped surface that is formed from two triangular-shaped inclined planes
48
and
50
that meet at a common boundary
52
, which bisects surface
46
. Inclined planes
48
and
50
form either a ridge
51
or a valley
51
. The angle of inclination between planes
48
and
50
is a function of the airfoil stagger angle.
Similarly, each bucket
40
's shroud
44
includes an outer flowpath surface
54
at which the other end
32
of the corresponding airfoil
18
intersects with shroud
44
. Like surface
46
, surface
54
is also a parallelogram-shaped surface that is also formed from two triangular-shaped inclined planes
56
and
58
that meet at a common boundary
60
, which bisects surface
54
. Here again, inclined planes
56
and
58
form a second ridge
53
or valley
53
, the angle of inclination between planes
56
and
58
is a function of the airfoil stagger angle.
Adjacent buckets, such as buckets
40
a
and
40
b
shown in
FIG. 2
a
, form an inner flowpath
62
, which is established by adjacent surfaces
46
a
and
46
b
of adjacent platforms
42
a
and
42
b
. Adjacent buckets
40
a
and
40
b
also form an outer flowpath
64
, which is established by adjacent surfaces
54
a
and
54
b
of adjacent shrouds
44
a
and
44
b.
The parallelogram shape of the inner flowpath surface
46
a
is divided into two triangular planes
48
a
and
50
a
that meet at a common boundary
52
a
and form a ridge
51
a
or a valley
51
a
. Similarly, the parallelogram shape of the inner flowpath surface
46
b
is also divided into two triangular planes
48
b
and
50
b
that meet at a common boundary
52
b
and form a ridge
51
b
or a valley
51
b
. The improved steam turbine bucket inside flowpath
62
consists of the two planes
50
a
and
48
b
sharing a common flush edge
66
at the interface between the two adjacent buckets
40
a
and
40
b
. This common flush edge
66
eliminates the flowpath steps
38
common in prior art buckets
12
.
The parallelogram shape of the outer flowpath surface
54
a
is also divided into two triangular planes
56
a
and
58
a
that meet at a common boundary
60
a
and form a ridge
53
a
or a valley
53
a
. Similarly, the parallelogram shape of the outer flowpath surface
54
b
is also divided into two triangular planes
56
b
and
58
b
that meet at a common boundary
60
b
and form a ridge
53
b
or a valley
53
b
. The improved steam turbine bucket outer flowpath
64
consists of the two planes
58
a
and
56
b
sharing a common flush edge
68
at the interface between the two adjacent buckets
40
a
and
40
b
. This common flush edge
68
again eliminates the flowpath steps
38
common in prior art buckets
12
.
One advantage of the bucket flowpath surface configuration used in the present invention is the potential of machining such surfaces without the use of 5-axis milling machines, thus making the part manufacturing more robust and cheaper to make.
The improved bucket flowpath surface configuration of the present invention could be used on reaction turbine buckets, as well as all other skewed and integral tip shrouded bucket designs.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
Claims
- 1. A turbine bucket comprising:a platform; a shroud; and an airfoil connected between the platform and the shroud; the platform including an inner flowpath surface at which the airfoil is connected to the platform, the inner flowpath surface being formed from a first inclined plane and a second inclined plane that meet at a first common boundary, wherein an inner flowpath without steps is formed between the inner flowpath surface and a second inner flowpath surface of a second platform of a second bucket of substantially the same construction as the bucket when the bucket is positioned adjacent to the second bucket; the shroud including an outer flowpath surface at which the airfoil is connected to the shroud, the outer flowpath surface being formed from a third inclined plane and a fourth inclined plane that meet at a second common boundary, wherein an outer flowpath without steps is formed between the outer flowpath surface and a second outer flowpath surface of a second shroud of the second bucket when the bucket is positioned adjacent to the second bucket.
- 2. A turbine bucket as recited in claim 1, wherein the inner flowpath surface and the outer flowpath surface are each parallelogram-shaped.
- 3. A turbine bucket as recited in claim 1, wherein the first, second, third, and fourth inclined planes are each triangular-shaped.
- 4. A turbine bucket as recited in claim 1, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first ridge.
- 5. A turbine bucket as recited in claim 1, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first valley.
- 6. A turbine bucket as recited in claim 1, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second ridge.
- 7. A turbine bucket as recited in claim 1, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second valley.
- 8. A turbine bucket comprising:a dovetail for mounting the bucket within the turbine; a platform connected to the dovetail; a shroud; and an airfoil connected between the platform and the shroud; the platform including an inner flowpath surface at which the airfoil is connected to the platform, the inner flowpath surface being formed from a first inclined plane and a second inclined plane that meet at a first common boundary; the shroud including an outer flowpath surface at which the airfoil is connected to the shroud, the outer flowpath surface being formed from a third inclined plane and a fourth inclined plane that meet at a second common boundary, wherein an inner flowpath is formed without steps by the inner flowpath surface when it is positioned adjacent to a second inner flowpath surface of a second platform of a second bucket positioned adjacent to the bucket; and wherein an outer flowpath is formed without steps by the outer flowpath surface when it is positioned adjacent to a second outer flowpath surface adjacent of a second shroud of the second bucket positioned adjacent to the bucket.
- 9. The turbine bucket as recited in claim 8, wherein the inner flowpath surface and the outer flowpath surface are each parallelogram-shaped.
- 10. The turbine bucket as recited in claim 8, wherein the first, second, third, and fourth inclined planes are each triangular-shaped.
- 11. The turbine bucket as recited in claim 10, wherein the inner flowpath is formed by the second triangular-shaped inclined plane of the bucket and a fifth triangular-shaped inclined plane of the second bucket adjacent to the bucket, the second and fifth planes and sharing a first common flush edge at the interface between them, andwherein the outer flowpath is formed by the fourth triangular-shaped inclined plane of the bucket and a sixth triangular-shaped inclined plane of the second bucket, the fourth and sixth planes and sharing a second common flush edge (at the interface between them.
- 12. A turbine bucket as recited in claim 8, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first ridge.
- 13. A turbine bucket as recited in claim 8, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first valley.
- 14. A turbine bucket as recited in claim 8, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second ridge.
- 15. A turbine bucket as recited in claim 8, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second valley.
- 16. A turbine bucket comprising:a dovetail for mounting the bucket within the turbine; a parallelogram-shaped platform connected to the dovetail; a parallelogram-shaped shroud; and an airfoil connected at a first end to the platform and at a second end to the shroud; the platform including an inner flowpath surface at which the first end of the airfoil intersects with the platform, the inner flowpath surface being parallelogram-shaped and formed from a first triangular-shaped inclined plane and a second triangular-shaped inclined plane that meet at a first common boundary, which bisects the inner flowpath surface, wherein an inner flowpath without steps is formed between the inner flowpath surface and a second inner flowpath surface of a second platform of a second bucket of substantially the same construction as the bucket when the bucket is positioned adjacent to the second bucket; the shroud including an outer flowpath surface at which the second end of the airfoil intersects with the shroud, the outer flowpath surface being parallelogram-shaped and formed from a third triangular-shaped inclined plane and a fourth triangular-shaped inclined plane that meet at a second common boundary, which bisects outer flowpath surface, wherein an outer flowpath without steps is formed between the outer flowpath surface and a second outer flowpath surface of a second shroud of the second bucket when the bucket is positioned adjacent to the second bucket.
- 17. The turbine bucket as recited in claim 16, wherein an inner flowpath is formed by the first triangular-shaped inclined plane of the bucket and a fifth triangular-shaped inclined plane of a second bucket adjacent to the bucket, the first and fifth planes sharing a first common flush edge at the interface between them, andwherein an outer flowpath is formed by the third triangular-shaped inclined plane of the bucket and a sixth triangular-shaped inclined plane of the second bucket, the third and sixth planes sharing a second common flush edge at the interface between them.
- 18. A turbine bucket as recited in claim 16, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first ridge.
- 19. A turbine bucket as recited in claim 16, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first valley.
- 20. A turbine bucket as recited in claim 16, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second ridge.
- 21. A turbine bucket as recited in claim 16, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second valley.
- 22. A stage of turbine buckets including at least two buckets, each bucket comprising:a dovetail for mounting the bucket within the turbine; a parallelogram-shaped platform connected to the dovetail; a parallelogram-shaped shroud; and an airfoil connected at a first end to the platform and at a second end to the shroud; the platform including an inner flowpath surface at which the first end of the airfoil intersects with the platform, the inner flowpath surface being parallelogram-shaped and formed from a first triangular-shaped inclined plane and a second triangular-shaped inclined plane that meet at a first common boundary, which bisects the inner flowpath surface; the shroud including an outer flowpath surface at which the second end of the airfoil intersects with the shroud, the outer flowpath surface being parallelogram-shaped and formed from a third triangular-shaped inclined plane and a fourth triangular-shaped inclined plane that meet at a second common boundary, which bisects the outer flowpath surface; wherein an inner flowpath is formed without steps by adjacent inner flowpath surfaces when two of the plurality of platforms are positioned adjacent to one another; and wherein an outer flowpath is formed without steps by adjacent outer flowpath surfaces when the two platforms are positioned adjacent to one another.
- 23. The plurality of turbine buckets of claim 22, wherein the inner flowpath is formed by the second triangular-shaped inclined plane of a first bucket and a fifth triangular-shaped inclined plane of a second bucket adjacent to the first bucket, the second and fifth planes sharing a common flush edge at the interface between the second and fifth planes, andwherein the outer flowpath is formed by the fourth triangular-shaped inclined plane of the first bucket and a sixth triangular-shaped inclined plane of the second bucket, the fourth and sixth planes sharing a common flush edge at the interface between the fourth and sixth planes.
- 24. A turbine bucket as recited in claim 22, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first ridge.
- 25. A turbine bucket as recited in claim 22, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first valley.
- 26. A turbine bucket as recited in claim 22, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second ridge.
- 27. A turbine bucket as recited in claim 22, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second valley.
- 28. A turbine bucket flowpath comprising:a first flowpath surface formed on one of a first platform or shroud of a first bucket, the flowpath surface being formed from a first inclined plane and a second inclined plane that meet at a first common boundary which bisects the flowpath surface; and a second flowpath surface formed on a corresponding one of a second platform or shroud of a second bucket the second flowpath surface being formed from a third inclined plane and a fourth inclined plane that meet at a second common boundary, which bisects the second flowpath surface; the flowpath being formed by the second inclined plane of the bucket and the third inclined plane of the second bucket adjacent to the bucket, the second and third planes sharing a common flush edge at the interface between them.
- 29. The turbine bucket flowpath as recited in claim 28, wherein the first flowpath surface and the second flowpath surface are each parallelogram-shaped.
- 30. The turbine bucket flowpath as recited in claim 28, wherein the first, second, third, and fourth inclined planes are each triangular-shaped.
- 31. A turbine bucket flowpath as recited in claim 28, wherein each first inclined plane and each second inclined plane meet at the first common boundary and form a first ridge.
- 32. A turbine bucket flowpath as recited in claim 28, wherein the first inclined plane and the second inclined plane meet at the first common boundary and form a first valley.
- 33. A turbine bucket as recited in claim 28, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second ridge.
- 34. A turbine bucket flowpath as recited in claim 28, wherein the third inclined plane and the fourth inclined plane meet at the second common boundary and form a second valley.
- 35. An inner turbine bucket flowpath comprising:a first inner flowpath surface formed on a first parallelogram-shaped platform of a first bucket, the inner flowpath surface being formed from a first triangular-shaped inclined plane and a second triangular-shaped inclined plane that meet at a first common boundary, which bisects the inner flowpath surface; and a second inner flowpath surface formed on a second parallelogram-shaped platform of a second bucket, the inner flowpath surface being formed from a third triangular-shaped inclined plane and a fourth triangular-shaped inclined plane that meet at a second common boundary, which bisects the inner flowpath surface; the inner flowpath being formed by the second triangular-shaped inclined plane of the bucket and the third triangular-shaped inclined plane of the second bucket adjacent to the first bucket, the second and third planes and sharing a common flush edge at the interface between them.
- 36. A turbine bucket flowpath as recited in claim 35, wherein each first and third inclined plane and each second and fourth inclined plane meet, respectively, at the first and second common boundaries and form first and second ridges.
- 37. A turbine bucket flowpath as recited in claim 35, wherein the first and third inclined plane and the second and fourth inclined plane meet, respectively, at the first common boundary and form first and second valleys.
- 38. A turbine bucket as recited in claim 35, wherein the first and third inclined plane and the second and fourth inclined plane meet, respectively, at the second common boundary and form first and second ridges.
- 39. A turbine bucket as recited in claim 35, wherein the first and third inclined plane and the second and fourth inclined plane meet, respectively, at the second common boundary and form first and second valleys.
- 40. An outer turbine bucket flowpath comprising:a first outer flowpath surface formed on a first parallelogram-shaped shroud of a first bucket, the outer flowpath surface being formed from a first triangular-shaped inclined plane and a second triangular-shaped inclined plane that meet and form a first ridge, which bisects the inner flowpath surface; and a second outer flowpath surface formed on a second parallelogram-shaped shroud of a second bucket, the outer flowpath surface being formed from a third triangular-shaped inclined plane and a fourth triangular-shaped inclined plane that meet and form a second ridge, which bisects the inner flowpath surface; the outer flowpath being formed by the second triangular-shaped inclined plane of the bucket and the third triangular-shaped inclined plane of the second bucket adjacent to the bucket, the second and third planes and sharing a common flush edge at the interface between them.
US Referenced Citations (4)
Number |
Name |
Date |
Kind |
2220918 |
Smith |
Nov 1940 |
A |
3490852 |
Carlstrom et al. |
Jan 1970 |
A |
3576377 |
Beanland et al. |
Apr 1971 |
A |
4135857 |
Pannone et al. |
Jan 1979 |
A |