Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Concave surface
Reexamination Certificate
2001-10-12
2003-06-17
Look, Edward K. (Department: 3745)
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Concave surface
C416SDIG002, C416SDIG005
Reexamination Certificate
active
06579066
ABSTRACT:
FIELD OF THE INVENTION
The present invention relates to a turbine bucket which is provided at the low pressure last stage of a steam turbine.
BACKGROUND ART
A turbine bucket is generally provided for a purpose of properly converting energy contained in thermal fluid into rotation energy. When designing the turbine bucket, it is necessary that the turbine bucket has a strength of withstanding a loading force and a centrifugal force by the thermal fluid and has to satisfy a mechanical characteristic with regard to vibration characteristic which prevents stimuli at the time of rated rotation. Further, in order to converting the thermal fluid energy into the rotation energy it is necessary to satisfy aerodynamic characteristic of reduced energy loss. Accordingly, in order to satisfy both the mechanical characteristic and the aerodynamic characteristic at the same time, it is necessary to overcome mutually contradicting structural requirements.
When there is a problem with regard to strength because of stress concentration at a contain position on a turbine bucket, even if a blade profile having a stream line reflecting fluid flow performance, it is necessary to thicken the blade cross section to increase the blade rigidity. Further, if the vibration characteristic of the blade profile shows stimuli at the time of the rated rotation which has to be avoided, it is also necessary to modify the blade profile. In particular, with regard to a turbine bucket for a steam turbine, if a higher efficiency of the blade performance is seeked, rigidity of individual blades is reduced, therefore, in order to increase rigidity of the blade structure as a whole, a blade connecting structure is employed in which adjacent blades are connected by such as shrouds and tie wires. Since such blade connecting structure disturbs the fluid flow in view of flow performance, the structure is not necessarily optimum as a turbine bucket as a whole.
In order to overcome these problems, it is necessary to determine the blade profile with only one solution for every limiting condition such as a blade length so as to fully satisfy reliability based on the mechanical characteristic as well as the aerodynamic characteristic. For example, U.S. Pat. No. 5,267,834 discloses a structure in which a blade profile satisfying strength, vibration and performance properly when the blade length is about 660 mm is determined, and a cover piece is provided at tips of the blades and a sleeve is provided at intermediate portions of the blades and the adjacent blades are connected by a member connecting the adjacent blades at two positions in the radial direction.
In the above referred to U.S. Pat. No. 5,267,834, it is indicated that for the blade profile and the blade structure when the blade length is about 660 mm through the provision of the blade connecting member at two positions in the radial direction the rigidity of the blade structure as a whole is enhanced. However, the provision of such blade connecting member at two positions in the intermediate portions of the blades disturbs working fluid flow at substantially the intermediate portions between the blades and extremely reduces fluid flow performance representing aerodynamic characteristic at the intermediate portions.
The present invention is carried out in view of the above problems and an object of the present invention is to provide a turbine bucket in which adjacent blades are connected without using the connecting member at the intermediate portions of the blades.
DISCLOSURE OF THE INVENTION
In order to achieve the object of the present invention, a turbine bucket of the present invention is formed in such a manner that the blade sectional configuration is twisted from a blade root portion to a blade tip side, and when assuming two axial directions in a blade section of the bucket on horizontal plane and taking one axial direction as X axis and the other axial direction perpendicular to X axis as Y axis, the blade sections at predetermined heights from the blade root portion of the turbine bucket are formed in a range of ±0.3 mm from respective points defining blade section configurations as shown respectively in chart 1, chart 4, chart 7, chart 10, chart 13, chart 16 and chart 18.
In order to achieve the object of the present invention, a turbine bucket of the present invention is formed in such a manner that the blade sectional configuration is twisted from a blade root portion to a blade tip side, and when assuming two axial directions in a blade section of the bucket on horizontal plane and taking one axial direction as X axis and the other axial direction perpendicular to X axis as Y axis, the blade sections at predetermined heights from the blade root portion of the turbine bucket are formed in a range of ±0.3 mm from respective points defining blade section configurations as shown respectively in chart 19, chart 22, chart 24, chart 9, chart 12, chart 15 and chart 18.
As has been explained above, according to the present invention an advantage can be obtained that a turbine bucket can be provided in which adjacent blades are connected each other without using a connecting member at the blade intermediate portion.
Further, the present invention provides, even with no connecting member at the blade intermediate portion, a turbine bucket which has a mechanical strength withstanding such as large centrifugal force and steam loading force, a vibration characteristic avoiding stimuli at the time of rated rotation and fluid flow performance converting steam energy to rotation every properly with reduced loss.
REFERENCES:
patent: 4900230 (1990-02-01), Patel
patent: 5088894 (1992-02-01), Patel
patent: 5267834 (1993-12-01), Dinh et al.
patent: 5286168 (1994-02-01), Smith
patent: 5286169 (1994-02-01), Dinh et al.
patent: 5299915 (1994-04-01), Dinh et al.
patent: 5393200 (1995-02-01), Dinh et al.
patent: 5445498 (1995-08-01), Williams et al.
patent: 5480285 (1996-01-01), Patel et al.
patent: 4-5402 (1992-01-01), None
Ikeuchi Kazuo
Katayose Masumi
Namura Kiyoshi
Saito Eiji
Shikano Yoshio
Kershteyn Igor
Look Edward K.
Mattingly Stanger & Malur, P.C.
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