IP Library › Granted Patent US 11,739,648
Granted Patent B2
US 11,739,648 · App. 17/531,207 · Granted Aug 29, 2023

Steam turbine rotor blade and manufacturing method and remodeling method of steam turbine rotor blade

Inventors: Yasuhiro Sasao (Tokyo, JP); Soichiro Tabata (Tokyo, JP); Ryo Takata (Tokyo, JP); Takeshi Kudo (Tokyo, JP)
Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
F01D5/22F05D2230/10F05D2260/602
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Quick Facts
Patent No.
US 11,739,648
App. No.
17/531,207
Granted
Aug 29, 2023
Kind
B2
Abstract

Water droplets that are moved on blade surfaces of a rotor blade are effectively guided toward the blade trailing edge while influence on the strength of the rotor blade is suppressed. A steam turbine rotor blade having a tie-boss for joining to adjacent blades at an intermediate position in the blade length direction is provided. The steam turbine rotor blade includes an airfoil part in which a blade surface is partly hollow as viewed in a section obtained by cutting by an orthogonal plane to a rotation center line of a turbine and a recessed blade surface that is this hollow partial blade surface passes through the blade root side of the tie-boss at least in a region on the pressure side and extends in a strip shape in the blade chord length direction.

Claims (16)

1. A steam turbine rotor blade having a tie-boss for joining to adjacent blades at an intermediate position in a blade length direction, the steam turbine rotor blade comprising:

an airfoil part in which a blade surface is partly hollow as viewed in a section obtained by cutting the airfoil part with an orthogonal plane to a rotation center line of a turbine and wherein a recessed blade surface forms the hollow partial blade surface and is positioned radially below the tie-boss at least in a region on a pressure side, and wherein the recessed blade surface extends in a strip shape in a blade chord length direction,

wherein

a starting end of the recessed blade surface that extends in the strip shape is located in a suction side surface and a terminal end of the recessed blade surface is located in a pressure side surface,

the recessed blade surface is continuous from the starting end to the terminal end via a blade leading edge and extends such that a distance from a blade root monotonically increases from the starting end to the terminal end, and

on a suction side of the rotor blade, the recessed blade surface is inclined outward in a radial direction toward the leading edge of the rotor blade, and on a pressure side of the rotor blade, the recessed blade surface is inclined outward in the radial direction toward a blade trailing edge.

2. The steam turbine rotor blade according to claim 1 , wherein the recessed blade surface has a curved shape as viewed in the section obtained by cutting the airfoil part with the orthogonal plane to the rotation center line.

3. The steam turbine rotor blade according to claim 1 , wherein

2<L/D<100 is satisfied when an opening length of the recessed blade surface is defined as L and a depth of the recessed blade surface is defined as D and an aspect ratio of the recessed blade surface is defined as L/D in the section obtained by cutting the airfoil part with the orthogonal plane to the rotation center line.

4. The steam turbine rotor blade according to claim 1 , wherein

a maximum value of an angle formed by normal lines normal to a blade surface and passing through two points on the blade surface close to each other across an edge in the recessed blade surface is in a range of 1 degree to 60 degrees in the section obtained by cutting the airfoil part with the orthogonal plane to the rotation center line.

5. The steam turbine rotor blade according to claim 1 , wherein

the airfoil part is carved out by mechanical processing and a depth of the recessed blade surface is equal to or smaller than a machining allowance in the mechanical processing.

6. A manufacturing method of the steam turbine rotor blade according to claim 1 having the tie-boss for joining to adjacent blades at the intermediate position in the blade length direction, the manufacturing method comprising:

carving out the steam turbine rotor blade having the recessed blade surface of by mechanical processing; and

carrying out shot peening for the airfoil part.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 19, 2021
From: SASAO, YASUHIRO; TABATA, SOICHIRO; TAKATA, RYO; KUDO, TAKESHI
To: MITSUBISHI HEAVY INDUSTRIES, LTD.
Reel/Frame 058168/0682 →
Priority Claims (1)
JP 2020-195377 · Nov 25, 2020 · national
Continuity (1)
Related Publication 20220162949A1 · May 26, 2022