Blade coupling structure and turbine system having the same

Patent metadata

Field	Value
Publication number	US-11293291-B2
Application number	US-202117155065-A
Country	US
Kind code	B2
Filing date	Jan 21, 2021
Priority date	Jan 31, 2020
Publication date	Apr 5, 2022
Grant date	Apr 5, 2022

Abstract

A blade coupling structure and a turbine system having the same securely couple a blade to a rotor disk. The blade coupling structure includes a root elastic member disposed between a root end of a blade root of the blade and an inner end of a coupling slot formed in the rotor disk; and a wedge member having a wedge body fitted between the root elastic member and the inner end of the coupling slot. The wedge member and the root elastic member press each other and press the root end so that the blade root is fixedly coupled to the coupling slot. A flat portion of the wedge member contacts the root elastic member, and an inclined portion of the wedge member facilitates the fitting of the wedge body. A wedge passage is formed in non-contact regions of the wedge body and passes a cooling fluid to the blade.

First claim

What is claimed is:

1. A blade coupling structure comprising:
a rotor disk having an outer peripheral surface in which a coupling slot is formed;
a blade having a blade root mounted in the coupling slot of the rotor disk;
a root elastic member disposed between an inner end of the coupling slot and a root end of the blade root; and
a wedge member disposed between the root elastic member and the inner end of the coupling slot,
wherein the wedge member and the root elastic member press each other and press the root end so that the blade root is fixedly coupled to the coupling slot,
wherein the wedge member comprises a wedge body fitted between the root elastic member and the inner end of the coupling slot, the wedge body including a radially inner side having a shape corresponding to the inner end of the coupling slot and radially outer side that is formed opposite to the radially inner side and faces the root elastic member;
wherein the radially outer side of the wedge member includes a flat portion in contact with the root elastic member,
wherein the wedge member further comprises a wedge passage formed in the wedge body so that a cooling fluid passes through the wedge passage in an axial direction of the rotor disk, and
wherein the wedge passage has a cross-sectional area that increases in a direction of flow of the cooling fluid to diffuse the cooling fluid.

2. The blade coupling structure according to claim 1 , wherein the wedge member further comprises an inclined portion formed at an axial end of the flat portion to facilitate the wedge body being fitted between the root elastic member and the inner end of the coupling slot.

3. The blade coupling structure according to claim 1 , wherein the wedge passage is formed in a region of the wedge body in which the root elastic member is not in contact with the flat portion.

4. The blade coupling structure according to claim 1 , wherein the root elastic member comprises:
a pair of edge contact portions respectively formed on circumferentially opposite sides of the root elastic member and respectively pressed in a radially outward direction by contact with circumferentially opposite sides of the flat portion;
a center contact portion formed on the center of the root elastic member and pressed in the radially outward direction by contact with the center of the flat portion; and
a pair of end contact portions formed between the center contact portion and either of the respective edge contact portions and configured to contact the root end of the blade root in order to press the root end of the blade root in the radially outward direction.

5. The blade coupling structure according to claim 1 , wherein the root elastic member comprises:
a center contact portion formed on the center of the root elastic member and pressed in the radially outward direction by contact with the center of the flat portion;
a pair of edge contact portions respectively formed on circumferentially opposite sides of the center contact portion; and
a pair of end contact portions respectively formed between either of the respective edge contact portions and a circumferential end of the root elastic member and configured to contact the root end of the blade root in order to press the root end of the blade root in the radially outward direction.

6. The blade coupling structure according to claim 1 , wherein the root elastic member comprises:
a pair of center contact portions disposed adjacent to each other;
a pair of edge contact portions formed on circumferentially opposite sides of the pair of center contact portions; and
a plurality of end contact portions including one end contact portion formed between the pair of center contact portions,
wherein the plurality of end contact portions further includes two other end contact portions, one of the two other end contact portions formed between one of the pair of center contact portions and one of the pair of edge contact portions, the other of the two other end contact portions formed between the other of the pair of center contact portions and the other of the pair of edge contact portions.

7. A blade coupling structure comprising:
a rotor disk having an outer peripheral surface in which a coupling slot is formed;
a blade having a blade root mounted in the coupling slot of the rotor disk;
a root elastic member disposed between an inner end of the coupling slot and a root end of the blade root; and
a wedge member disposed between the root elastic member and the inner end of the coupling slot,
wherein the wedge member and the root elastic member press each other and press the root end so that the blade root is fixedly coupled to the coupling slot,
wherein the wedge member comprises a wedge body fitted between the root elastic member and the inner end of the coupling slot, the wedge body including a radially inner side having a shape corresponding to the inner end of the coupling slot and a radially outer side that is formed opposite to the radially inner side and faces the root elastic member;
wherein the radially outer side of the wedge member includes a flat portion in contact with the root elastic member,
wherein the wedge member further comprises a wedge passage formed in the wedge body so that a cooling fluid passes through the wedge passage in an axial direction of the rotor disk, and
wherein the wedge passage has a cross-sectional area that decreases in a direction of flow of the cooling fluid to increase a flow rate of the cooling fluid.

8. A turbine system comprising:
a casing;
a compression section disposed in the casing and configured to compress air; a combustor connected to the compressor section and configured to produce combustion gas by burning a mixture of fuel and the compressed air; and
a turbine section disposed in the casing and configured to generate power using the combustion gas,
wherein at least one of the compression section and the turbine section comprises:
a rotor disk having an outer peripheral surface in which a coupling slot is formed;
a blade having a blade root mounted in the coupling slot of the rotor disk;
a root elastic member disposed between an inner end of the coupling slot and a root end of the blade root; and
a wedge member disposed between the root elastic member and the inner end of the coupling slot,
wherein the wedge member and the root elastic member press each other and press the root end so that the blade root is fixedly coupled to the coupling slot,
wherein the wedge member comprises a wedge body fitted between the root elastic member and the inner end of the coupling slot, the wedge body including a radially inner side having a shape corresponding to the inner end of the coupling slot and a radially outer side that is formed opposite to the radially inner side and faces the root elastic member,
wherein the radially outer side of the wedge member includes a flat portion in contact with the root elastic member,
wherein the wedge member further comprises a wedge passage formed in the wedge body so that a cooling fluid passes through the wedge passage in an axial direction of the rotor disk, and
wherein the wedge passage has a cross-sectional area that increases in a direction of flow of the cooling fluid to diffuse the cooling fluid.

9. The turbine system according to claim 8 , wherein the wedge member further comprises an inclined portion formed at an axial end of the flat portion to facilitate the wedge body being fitted between the root elastic member and the inner end of the coupling slot.

10. The turbine system according to claim 8 , wherein the wedge passage has a cross-sectional area that decreases in a direction of flow of the cooling fluid to increase

Assignees

• Doosan Heavy Ind & Construction Co Ltd

Inventors

• Bae Jinho

Classifications

• F01D5/081

  Cooling fluid being directed on the side of the rotor disc or at the roots of the blades (F01D5/087 takes precedence) · CPC title

• F01D5/3007 Primary

  of axial insertion type · CPC title

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F01D5/147

  Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18) · CPC title

• F01D5/3092

  Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers (F01D5/288 takes precedence) · CPC title