Turbine exhaust structure of particular design

Abstract

A turbine exhaust structure for an intermediate-pressure exhaust end of a high-and-intermediate-pressure (HIP) module.

Claims

1. A turbine exhaust structure, comprising: a casing divided into a first element having an arcuate shape and a second element coupled to the first element, with a central aperture formed between the first element and the second element, the central aperture extending from a first face of the casing to a second face of the casing opposing the first face, wherein the first element and the second element are configured to receive turbine exhaust, wherein a flow of the turbine exhaust in the first element is undivided from a flow of the turbine exhaust in the second element to form an unseparated turbine exhaust passage; wherein the second element comprises at least one outlet having a rectangular cross section configured to receive the flow of turbine exhaust from the first element and the flow of turbine exhaust from the second element, wherein the at least one outlet combines the flow of turbine exhaust from the first element with the flow of turbine exhaust from the second element and directs a combined flow of turbine exhaust in a downward direction extending outward from a side of the second element; at least one exhaust pipe having a circular cross section correspondingly coupled to the at least one outlet of the second element of the casing, wherein the at least one exhaust pipe is configured to receive only the combined flow of turbine exhaust from the second element, wherein the at least one exhaust pipe directs the downward directed combined flow of turbine exhaust received from the at least one outlet in a direction extending outward from the at least one outlet, and at least one connecting pipe configured to correspondingly connect the at least one outlet of the second element to the at least one exhaust pipe, the at least one connecting pipe having a first end with a rectangular cross section coupled to the rectangular cross section of the at least one outlet and a second end with a circular cross section coupled to the circular cross section of the at least one exhaust pipe, wherein the at least one connecting pipe directs the combined flow of turbine exhaust received from the at least one outlet in the same downward direction towards the at least one exhaust pipe, wherein the at least one exhaust pipe guides the combined flow of turbine exhaust received from the at least one connecting pipe in a direction extending laterally outward from the at least one outlet and the least one connecting pipe, wherein the turbine exhaust structure is an intermediate-pressure exhaust end.

2. The turbine exhaust structure according to claim 1, wherein the first element is connected to the second element along a horizontal joint plane.

3. The turbine exhaust structure according to claim 1, wherein the first element is an upper element, and the second element is a lower element.

4. The turbine exhaust structure according to claim 1, wherein a section of the first face of the central aperture is larger than a section of the second opposite face of the central aperture.

5. The turbine exhaust structure according to claim 1, wherein the at least one connecting pipe comprises a plurality of connecting pipes, and wherein the second element comprises at least two outlets, each outlet connected to a respective connecting pipe of the plurality of connecting pipes.

6. The turbine exhaust structure according to claim 1, wherein the second element is welded to the at least one connecting pipe.

7. The turbine exhaust structure according to claim 1, wherein a dimension of the turbine exhaust structure varies from 6 to 12 meters.

8. The turbine exhaust structure according to claim 1, wherein a dimension of the turbine exhaust structure varies from 9 to 10 meters.

9. The turbine exhaust structure according to claim 1, wherein a dimension of the turbine exhaust structure varies from 2 to 6 meters.

10. The turbine exhaust structure according to claim 1, wherein a dimension of the turbine exhaust structure varies from 3 to 4 meters.

11. The turbine exhaust structure according to claim 1, wherein no pipe is connected to the first element.

12. The turbine exhaust structure of claim 1, further comprising: a plurality of spaced outer reinforcements on the first element and the second element, each of the spaced outer reinforcements extending radially from the central aperture about both the first face of the casing and the second face of the casing.

13. A steam turbine, comprising: a combined high-and-intermediate pressure (HIP) casing having a high pressure casing; and an intermediate pressure turbine exhaust end structure coupled to the HIP casing, the intermediate pressure turbine exhaust structure end structure including: a casing divided into a first element having an arcuate shape and a second element coupled to the first element, with a central aperture formed between the first element and the second element, the central aperture extending from a first face of the casing to a second face of the casing opposing the first face, wherein the first element and the second element are configured to receive turbine exhaust, wherein a flow of the turbine exhaust in the first element is undivided from a flow of the turbine exhaust in the second element to form an unseparated turbine exhaust passage; wherein the second element comprises at least one outlet having a rectangular cross section configured to receive the flow of turbine exhaust from the first element and the flow of turbine exhaust from the second element, wherein the at least one outlet combines the flow of turbine exhaust from the first element with the flow of turbine exhaust from the second element and directs a combined flow of turbine exhaust in a downward direction extending outward from a side of the second element; at least one exhaust pipe having a circular cross section correspondingly coupled to the at least one outlet of the second element of the casing, wherein the at least one exhaust pipe is configured to receive only the combined flow of turbine exhaust from the second element, wherein the at least one exhaust pipe directs the downward directed combined flow of turbine exhaust received from the at least one outlet in a direction extending outward from the at least one outlet, and at least one connecting pipe configured to correspondingly connect the at least one outlet of the second element to the at least one exhaust pipe, the at least one connecting pipe having a first end with a rectangular cross section coupled to the rectangular cross section of the at least one outlet and a second end with a circular cross section coupled to the circular cross section of the at least one exhaust pipe, wherein the at least one connecting pipe directs the combined flow of turbine exhaust received from the at least one outlet in the same downward direction towards the at least one exhaust pipe, wherein the at least one exhaust pipe guides the combined flow of turbine exhaust received from the at least one connecting pipe in a direction extending laterally outward from the at least one outlet and the least one connecting pipe.

14. The steam turbine according to claim 13, wherein the first face of the casing of the intermediate pressure turbine exhaust end structure is configured to connect with the HIP casing.

15. A turbine exhaust structure, comprising: a casing divided into a first element having an arcuate shape and a second element coupled to the first element, with a central aperture formed between the first element and the second element, the central aperture extending from a first face of the casing to a second face of the casing opposing the first face, wherein the first element and the second element are configured to receive turbine exhaust, wherein a flow of the turbine exhaust in the first element is undivided from a flow of the turbine exhaust in the second element to form an unseparated turbine exhaust passage; wherein the second element comprises a first outlet and a second outlet, each outlet having a rectangular cross section configured to receive the flow of turbine exhaust from the first element and the flow of turbine exhaust from the second element, wherein each of the first outlet and the second outlet combines the flow of turbine exhaust from the first element with the flow of turbine exhaust from the second element and directs a combined flow of turbine exhaust in a downward direction extending outward from a side of the second element, wherein the first outlet and the second outlet are located on opposing sides of the second element; a first exhaust pipe and a second exhaust pipe correspondingly coupled with the first outlet and the second outlet of the second element of the casing, the first exhaust pipe and the second exhaust pipe each having a circular cross section, wherein the first exhaust pipe and the second exhaust pipe are each configured to receive only the combined flow of turbine exhaust from the second element, wherein each of the first and second exhaust pipes directs the downward directed combined flow of turbine exhaust received from the correspondingly coupled first outlet and second outlet in a direction extending outward from the correspondingly coupled first outlet and second outlet, and a first connecting pipe and a second connecting pipe correspondingly connecting the first and the second outlets of the second element to the first and second exhaust pipes, the first connecting pipe and the second connecting pipe each having a first end with a rectangular cross section correspondingly coupled to the rectangular cross sections of the first and the second outlets and a second end with a circular cross section correspondingly coupled to the circular cross sections of the first and the second exhaust pipes, wherein each of the first and second connecting pipes directs the combined flow of turbine exhaust received from the correspondingly coupled first outlet and second outlet in the same downward direction towards the correspondingly coupled first exhaust pipe and second exhaust pipe, wherein each of the first exhaust pipe and second exhaust pipe guides the combined flow of turbine exhaust received from the correspondingly coupled first connecting pipe and second connecting pipe in a direction extending laterally outward from the correspondingly coupled first outlet and second outlet and the correspondingly coupled first connecting pipe and second connecting pipe, wherein the turbine exhaust structure is an intermediate-pressure exhaust end.

Description

DRAWINGS

(1) Other features and advantages of the present invention will appear from the following description, given by way of examples and in view of the following drawings in which:

(2) FIG. 1A is an isometric view of a HIP casing used in a known steam turbine;

(3) FIG. 1B is a schematic view of an intermediate-pressure exhaust end used in a known steam turbine;

(4) FIG. 2 is an isometric view of a high-and-intermediate-pressure casing comprising a turbine exhaust structure according to one embodiment of the invention;

(5) FIG. 3 is a vertical flange connection side isometric view of a turbine exhaust structure according to an embodiment of the invention; and

(6) FIG. 4 is a rear pedestal side isometric view of a turbine exhaust structure according to an embodiment of the invention.

DETAILED DESCRIPTION

(7) Reference is first made to FIG. 2 which discloses a HIP casing 31 according to an embodiment of the invention. The high-and-intermediate-pressure casing 31 comprises a turbine exhaust structure 30, which is an intermediate-pressure exhaust end 30, and a combined high-pressure/intermediate-pressure casing 32, said casing 32 being connected to the turbine exhaust structure 30 thanks to a vertical flange connection 33.

(8) It is worth noting that the combined high-pressure/intermediate-pressure casing 32 is identical to the combined high-pressure/intermediate-pressure casing 12 represented on FIG. 1A. In an embodiment, the intermediate-pressure exhaust end 30 is configured to be connected to the different modules used in a known steam turbine. In other words, the interfaces of the intermediate-pressure exhaust end 30 are configured in such a way that the design of the other components, i.e., those constituting a known steam turbine and intended to be associated to an intermediate-pressure exhaust end 30, does not need to be modified.

(9) For example, the vertical flange connection 33 is identical to the one used in an intermediate-pressure exhaust end of the prior art like the vertical flange connection 13.

(10) As illustrated on FIGS. 3 and 4, the intermediate-pressure exhaust end 30 comprises a casing 34 divided into a first element 35 and a second element 36, which is connected to the first element. The intermediate-pressure exhaust end 30 also comprises two connecting pipes 37, 38 which are configured to be connected to a second pipe 39 and 40. The second pipe 39, 40 is an elbow pipe.

(11) The second element 36 comprises two outlets 41, 42 (not shown) of rectangular cross section. The connecting pipe 37, 38 is provided with a first end 371, 381, having a first section, and a second end 372, 382, having a second section. Moreover, the second element 36 is connected to the connecting pipe 37, 38 via a welded connection.

(12) The outlet 41, 42 is connected to the first end 371, 381 and the second end 372, 382 is configured to be connected to the second pipe 39, 40.

(13) As illustrated on FIGS. 3 and 4, the first element 35 is an upper element 35. The second element 36 is a lower element 36.

(14) It is to be noted that the casing 34 has a central aperture 43 which extends from a first face 341, shown on FIG. 3, to a second opposite face 342 of the casing 34, shown on FIG. 4. A first face central aperture 431 has a first section and a second face central aperture 432 has a second section. The first section of the first face central aperture 431 is larger than the second section of the second face central aperture 432.

(15) Moreover, the upper element 35 is connected to the lower element 36 along a horizontal joint plan by a plurality of studs and nuts 44 via two supports 45 and 46 on the second opposite face 342, as shown on FIG. 4.

(16) The casing 34 comprises a plurality of outer reinforcements 47 on both the upper element 35 and the lower element 36. The outer reinforcements 47 of the lower element 36 extend radially from both the first face central aperture 431 and the second face central aperture 432. The outer reinforcements 47 of the upper element 35 extend radially from the first face central aperture 431 to the second face central aperture 432 and vice versa. The casing 34 also comprises a plurality of inner reinforcements 48 (not shown) located inside said casing 34.

(17) In addition, the first face central aperture 431 of the casing 34 is configured to be connected with the combined high-pressure/intermediate-pressure casing 32 due to the vertical flange connection 33 and a plurality of studs and nuts 49, which are around the first face central aperture 431, and a sealing weld.

(18) As shown on FIGS. 2, 3 and 4, no pipe is connected to the upper element 35.

(19) Thus, such configuration makes the maintenance operations much easier as compared to the one of the intermediate-pressure casing 11 with the four outlets 16, 17, 18 and 19. Indeed, no pipe needs to be dismantled nor retightened. Specifically, the opening and closing of the HIP casing 31 is easier.

(20) Furthermore, the turbine exhaust end according to the present invention is very cost-efficient because it allows avoiding the use of Y-shaped pipes which are very difficult to manufacture, thereby reducing quantities of materials to be used. Indeed, it is estimated that the turbine exhaust end according to the present invention allows sparing around 15 tons of materials. Moreover, the turbine exhaust end according to the present invention is also very cost-efficient because said turbine exhaust end is a fabricated structure whereas the one described in FIG. 1A is a foundry structure.

(21) The interfaces of the intermediate-pressure exhaust end 30 are configured in such a way that the design of the other components constituting a known steam turbine, for example the diaphragms, does not need to be modified.