Steam turbine sealing mechanism

Description

Field

[0001] The present invention relates to a steam turbine.

Background

[0002] One known steam turbine includes a casing for containing a turbine rotor and a gland packing for sealing the gap between the casing and the turbine rotor, as disclosed in, for example, Japanese patent application laid open number 2003-13704. In this steam turbine, the gland packing includes two separate parts, and the first half and second half of the gland packing are connected with bolts with the joint surface of the first half of the gland packing and the joint surface of the second half mating with each other. In addition, the casing and the gland packing are connected with bolts with the joint surface of the casing and the joint surface of the gland packing mating with each other. Seal steam (gland steam) is supplied to the first half of the gland packing, and heat insulation members are disposed in the second half of the gland packing. In this manner, leakage of the steam from the gap between the casing and the gland packing when the casing is thermally deformed is prevented.

[0003] US 5,031,921 discloses a steam turbine gland seal arrangement for use in a steam turbine which has at least one casing and a shaft extending through the casing so that steam may be admitted into the casing for operating on blades attached to the shaft for effecting rotation thereof. An inner gland and an outer gland are provided at one end of the shaft where the shaft exits the casing. Each of these glands supports seals in close proximity with the shaft for preventing steam from escaping the casing. The inner gland is supported within an aperture in the casing where the shaft exits, and the outer gland is attached to an outer surface of the casing surrounding the aperture. The arrangement further includes an annular seal plate which circumscribes the turbine shaft and has an inner radial portion attached to an outer surface of the inner gland. An outer radial portion of the annular seal plate is cantilevered from the inner attached portion. The outer radial portion contacts an axially inner surface of the outer gland when this gland is attached to the casing. The outer gland exerts a deflecting pressure on the annular seal plate to provide a positive seal between the inner gland and the outer gland.

[0004] JP H06 26303 A discloses a steam turbine having a turbine axle provided on the low pressure side with a collar larger than the outer diameter of its coupling flange. A cover for closing the opened end face of an outer casing is formed into a disc shape having the outer diameter equal to the outer diameter of the opened end face of the outer casing and the inner diameter fitted to the collar of the turbine axle. Gland packing of opposed labyrinth structure is then provided between the collar and the inner diameter side of the cover and connected to the opened end face of the outer casing by a bolt so as to improve sealing performance and to facilitate assembly and disassembly.

Summary

Technical Problem

[0005] When the difference in temperature between the casing and the gland packing becomes large and the difference in the amount of thermal deformation thereby becomes large, sufficient pressure (contact pressure) may not be ensured on, for example, the mating surface at which the joint surface of the first half of the gland packing and the joint surface of the second half mate with each other. Therefore, the steam may leak from the gap between the first half and second half of the gland packing.

[0006] It is an object of the present invention to provide a steam turbine in which leakage of steam can be prevented.

Solution to Problem

[0007] According to the present invention, there is provided a steam turbine comprising: a turbine rotor including a shaft member and a plurality of seals connected to the shaft member, the shaft member extending in an axial direction; a turbine casing disposed around the turbine rotor with a turbine casing space formed between the turbine casing and the turbine rotor; and a gland casing connected to an axial end of the turbine casing and including an outer gland axially disposed so as to close an opening at an axial end of the turbine casing space from the outside, and an inner gland axially disposed so as to provide a gland space between the inner gland and the outer gland, wherein the outer gland and the inner gland each include a first annular section having a first joint surface and a second annular section having a second joint surface joined to the first joint surface, the first annular section being disposed around a part of the turbine rotor, the second annular section being disposed around another part of the turbine rotor, and wherein a gland steam is supplied into the gland space and said plurality of seals is provided between the shaft member and the inner gland and between the shaft member and the outer gland, and wherein the inner gland includes an annular protrusion extending in an axial direction from the inner gland toward the outer gland; the steam turbine further comprising: a heat insulation space defined by a radially inner surface of the turbine casing, a radially inner surface of the outer gland, the inner gland including a radially outer facing surface of the protrusion, and a sealing mechanism, wherein the sealing mechanism is disposed between the radially inner surface of the outer gland and the radially outer facing surface of the protrusion to prevent the gland steam in the gland space from flowing into the heat insulation space.

[0008] In the present invention, the heat insulation space in which steam flow is inhibited is formed in the boundary region between the first end portion of the turbine casing and the second end portion of the gland member adjacent to the first end portion of the turbine casing. This prevents the difference in temperature between the turbine casing and the gland member from increasing in the boundary region (a joint portion, a connection portion) between the turbine casing and the gland member. Therefore, the difference in the amount of thermal deformation between the turbine casing and the gland member is prevented from increasing in the vicinity of the boundary region. Leakage of steam from the mating surface at which the first joint surface of the first section of the gland member mates with the second joint surface of the second section is thereby prevented.

[0009] In the steam turbine according to an embodiment of the present invention, the heat insulation space is formed so as to surround the shaft. In this case, the difference in temperature between the turbine casing and the gland member is prevented from increasing.

[0010] In the steam turbine according to another embodiment of the present invention, the heat insulation space is a hermetically sealed space. In this case, the steam flow is sufficiently inhibited in the heat insulation space, and a high heat insulation effect can be obtained.

[0011] In the steam turbine according to yet another embodiment of the present invention, the turbine casing includes: a first turbine casing section disposed around a part of the turbine rotor and a second turbine casing section disposed around another part of the turbine rotor, the first and second turbine casing sections being connected to each other to form the turbine casing. When the turbine casing, as well as the gland member, is separable, maintenance, for example, is facilitated.

Advantageous Effects of Invention

[0012] According to the present invention, leakage of steam can be prevented.

Brief Description of Drawings

[0013] 

FIG. 1 is a schematic configuration diagram illustrating an example of a steam turbine according to an embodiment.

FIG. 2 is a side cross-sectional view illustrating the vicinity of a boundary region between a turbine casing and a gland member according to the embodiment.

FIG. 3 is a front view illustrating an example of a casing according to the embodiment.

FIG. 4 is a perspective view illustrating an example of the gland member according to the embodiment.

FIG. 5 is a diagram illustrating an example of a sealing mechanism according to the embodiment.

FIG. 6 is a diagram illustrating an example of a steam turbine according to a comparative example.

FIG. 7 is a diagram illustrating the distribution of temperature in a turbine casing and a gland member in the comparative example.

FIG. 8 is a diagram illustrating the distribution of temperature in the turbine casing and the gland member according to the embodiment.

Description of Embodiments

[0014] Embodiments of the present invention will next be described with reference to the drawings, but the present invention is not limited thereto. The requirements in the respective embodiments described below may be appropriately combined. Some components may not be used. The components in the following embodiments include those which can be easily replaced by persons skilled in the art and also include those substantially equivalent to these components.

[0015] In the following description, an XYZ orthogonal coordinate system is set, and the positional relations between components will be described with reference to the XYZ orthogonal coordinate system. One direction in a prescribed plane is defined as an X axis direction. A direction orthogonal to the X axis direction in the prescribed plane is defined as a Y axis direction, and a direction orthogonal to (i.e., a direction normal to) the X axis direction and to the Y axis direction is defined as a Z axis direction. The directions of rotation (inclination) about the X, Y, and Z axes are defined as θX, θY, and θZ directions, respectively. The X axis is perpendicular to a YZ plane. The Y axis is perpendicular to an XZ plane. The Z axis is perpendicular to an XY plane. The XY plane includes the X axis and the Y axis. The XZ plane includes the X axis and the Z axis. The YZ plane includes the Y axis and the Z axis.

[0016] FIG. 1 is a schematic configuration diagram illustrating an example of a steam turbine 1 according to this embodiment. In FIG. 1, the steam turbine 1 includes a low-pressure turbine casing 100 and a high-pressure turbine casing 200. The high-pressure turbine casing 200 includes a casing 3 disposed around a turbine rotor 2. In this embodiment, the shaft (rotating shaft) of the turbine rotor 2 is parallel to the X axis.

[0017] The casing 3 includes: a turbine casing 4 disposed around the turbine rotor 2 and having a turbine casing space SP formed between the turbine casing 4 and the turbine rotor 2; and gland casings 5 disposed around the turbine rotor 2 and connected to the turbine casing 4 so as to close openings 24 at the ends of the turbine casing space SP. The openings 24 and the gland casings 5 are disposed at respective opposite ends, with respect to X axis direction, of the turbine casing 4.

[0018] FIG. 2 is an enlarged diagram showing part of FIG. 1 and is a side cross-sectional view illustrating the vicinity of a boundary region between the turbine casing 4 and one of the gland casings 5. FIG. 2 is a cross-sectional view showing the vicinity of the gland casing 5 disposed on the +X side of the center of the turbine casing space SP. FIG. 3 is a front view illustrating an example of the casing 3 of the steam turbine 1.

[0019] As shown in FIGS. 1, 2, and 3, the turbine rotor 2 includes a rotatable shaft member 21 and a plurality of seals 22 connected to the shaft member 21. As shown in FIG. 1, the turbine rotor 2 is rotatably supported by bearings 32. The bearings 32 are disposed outside of the turbine casing 4. The bearings 32 are supported by bearing stands provided on a base 35 formed from, for example, concrete.

[0020] The turbine casing 4 is disposed around the turbine rotor 2. The turbine casing 4 has the openings 24 which connect the outer space of the turbine casing 4 to the turbine casing space SP, i.e., the inner space of the turbine casing 4, and in which at least part of the turbine rotor 2 is disposed. The openings 24 are formed on the opposite sides, with respect to the X axis direction, of the turbine casing 4 and disposed at the opposite ends of the turbine casing space SP. The central portion, with respect to the X axis direction, of the turbine rotor 2 is disposed inside of the turbine casing 4, and the opposite ends of the turbine rotor 2 are disposed outside of the turbine casing 4. A steam supply port is provided in an upper portion of the turbine casing 4. Steam (main steam) is supplied to the turbine casing space SP of the turbine casing 4 through the steam supply port.

[0021] The turbine casing 4 is separated into an upper turbine casing 4A and a lower turbine casing 4B. The upper turbine casing 4A is disposed around a part of the turbine rotor 2, and the lower turbine casing 4B is disposed around another part of the turbine rotor 2. The upper turbine casing 4A has a joint surface Pa1. The lower turbine casing 4B has a joint surface Pb1 joined to the joint surface Pa1. Each of the joint surface Pa1 and the joint surface Pb1 is parallel to the XY plane.

[0022] The upper turbine casing 4A includes an upper flange 41 including the joint surface Pa1. The lower turbine casing 4B includes a lower flange 42 including the joint surface Pb1. With the joint surface Pa1 and the joint surface Pb1 mating with each other, the upper turbine casing 4A and the lower turbine casing 4B are fastened with bolts and thereby connected to each other, whereby the turbine casing 4 is formed. The openings 24 are formed between the upper turbine casing 4A and the lower turbine casing 4B.

[0023] As shown in FIG. 2, each of the gland casings 5 includes: an outer gland (gland member) 51 disposed so as to close the opening 24 at an end of the turbine casing space SP from the outside; and an inner gland (inner member) 52 disposed at a position closer to the center, with respect to the X axis direction, of the turbine casing space SP than the outer gland 51 so as to close the opening 24 at the end of the turbine casing space SP. The outer gland 51 and the inner gland 52 are disposed around the turbine rotor 2.

[0024] As shown in FIG. 2, the turbine casing 4 has a joint surface Pb2 joined to a joint surface Pa2 of the outer gland 51. The joint surface Pb2 of the turbine casing 4 is an attachment surface to which the outer gland 51 is attached. The joint surface Pb2 of the turbine casing 4 is an annular surface disposed around the opening 24 and facing outward with respect to the center of the turbine casing space SP. Each of the joint surface Pa2 and the joint surface Pb2 is parallel to the YZ plane perpendicular to the shaft of the turbine rotor 2. A mating surface P2 at which the joint surface Pa2 and the joint surface Pb2 mate with each other is perpendicular to a mating surface P1 at which the joint surface Pa1 and the joint surface Pb1 mate with each other.

[0025] FIG. 4 is a perspective view of one of the outer glands 51. Each outer gland 51 is disposed so as to cover a gap between the turbine casing 4 and the turbine rotor 2 disposed in the opening 24 of the turbine casing 4 and prevents leakage of steam from the opening 24. In this embodiment, gland steam (seal steam) is supplied to a gland space GS between the outer gland 51 and the inner gland 52 through supply ports 81 provided in the outer gland 51. At least part of the gland steam supplied to the gland space GS is discharged from discharge ports 82 provided in the outer gland 51.

[0026] As shown in FIGS. 3 and 4, each outer gland 51 has an annular shape in the YZ plane. At least part of the outer gland 51 is connected to the turbine casing 4. With the joint surface Pa2 of the turbine casing 4 and the joint surface Pb2 of the outer gland 51 mating with each other, the outer gland 51 and the turbine casing 4 are fastened with bolts 37, and the outer gland 51 is thereby connected to the turbine casing 4.

[0027] Each outer gland 51 is separated into an upper outer gland 51A and a lower outer gland 51B. The upper outer gland 51A is disposed around a part of the turbine rotor 2, and the lower outer gland 51B is disposed around another part of the turbine rotor 2. The upper outer gland 51A has a joint surface Pa3. The lower outer gland 51B has a joint surface Pb3 joined to the joint surface Pa3. The joint surface Pa3 and the joint surface Pb3 are parallel to the XY plane. In this embodiment, the mating surface P1 at which the joint surface Pa1 and the joint surface Pb1 mate with each other and a mating surface P3 at which the joint surface Pa3 and the joint surface Pb3 mate with each other are disposed in the same plane.

[0028] The upper outer gland 51A includes an upper flange 27 including the joint surface Pa3. The lower outer gland 51B includes a lower flange 28 including the joint surface Pb3. With the joint surface Pa3 and the joint surface Pb3 mating with each other, the upper outer gland 51A and the lower outer gland 51B are fastened with bolts 38 and thereby connected to each other, whereby the outer gland 51 is formed.

[0029] Each inner gland 52 is disposed so as to cover a gap between the turbine casing 4 and the turbine rotor 2 disposed in the opening 24 of the turbine casing 4 and prevents leakage of steam from the opening 24. At least part of the inner gland 52 is connected to the turbine casing 4. The inner gland 52 has an annular shape in the YZ plane. As is the outer gland 51, the inner gland 52 may be separated into an upper inner gland and a lower inner gland. The inner gland 52 may be formed by connecting the upper inner gland and the lower inner gland with, for example, bolts. The inner gland 52 may not be separated.

[0030] As shown in FIG. 2, the inner gland 52 has a connection section 53 connected to the inner surface of the turbine casing 4. In this embodiment, a recess 54 is formed on the inner surface of the turbine casing 4. The connection section 53 includes a protrusion fitted into the recess 54. The inner gland 52 includes a protrusion 55 extending toward the outer side of the center, with respect to the X axis direction, of the turbine casing space SP. The protrusion 55 is disposed so as to surround the shaft of the turbine rotor 2.

[0031] A heat insulation space HS is defined by a first region 61 of the inner surface of the turbine casing 4 and a second region 62 of the outer gland 51 with respect to the X axis direction. The first region 61 of the inner surface of the turbine casing 4 includes a first end portion, with respect to the X axis direction, of the inner surface of the turbine casing 4 (the end portion on the +X side in the example shown in FIG. 2). The second region 62 of the outer gland 51 includes a second end portion of the inner surface of the outer gland 51 that is adjacent to the first end portion of the inner surface of the turbine casing 4 (the second end portion is the end portion of the outer gland 51 on the -X side in the example shown in FIG. 2). The heat insulation space HS is formed between the first region 61 of the turbine casing 4, the second region 62 of the outer gland 51, the inner gland 52, and a sealing mechanism 70. In this embodiment, the inner gland 52 and the sealing mechanism 70 serve as space-forming members that form the heat insulation space HS between the inner gland 52, the sealing mechanism 70, the first region 61, and the second region 62.

[0032] The inner gland 52 includes: a facing surface 56 that is disposed in the protrusion 55 and faces the first region 61 and the second region 62 through a gap; and a side surface 57 that is disposed between the connection section 53 and the facing surface 56 and faces the outer side with respect to the center of the turbine casing space SP. The side surface 57 faces the sealing mechanism 70 through a gap. In this embodiment, each of the first region 61, the second region 62, and the facing surface 56 is substantially parallel to the X axis.

[0033] The sealing mechanism 70 seals the gap between the facing surface 56 and the inner surface of the outer gland 51. In this embodiment, the heat insulation space HS is formed between the first region 61 of the turbine casing 4, the second region 62 of the outer gland 51, the facing surface 56 of the inner gland 52, the side surface 57 of the inner gland 52, and the sealing mechanism 70.

[0034] The heat insulation space HS is a closed space. In this embodiment, the heat insulation space HS is a hermetically sealed space. The heat insulation space HS is formed so as to surround the shaft of the turbine rotor 2. The gland space GS is disposed so as to be adjacent to the heat insulation space HS. The space-forming members including the inner gland 52 (the protrusion 55) and the sealing mechanism 70 are disposed at the boundary between the heat insulation space HS and the gland space GS. The first region 61 and the second region 62 form the boundary region between the turbine casing 4 and the outer gland 51. The heat insulation space HS is disposed between the gland space GS and the first and second regions 61 and 62.

[0035] In the heat insulation space HS, the flow of steam is inhibited. In this embodiment, the flow of steam (the velocity of the airflow) in the heat insulation space HS is smaller (lower) than the flow of steam (the velocity of the airflow) in the gland space GS. Gland steam is supplied from the outside of the gland space GS to the gland space GS through the supply ports 81. No steam (such as gland steam) is supplied from the outside of the heat insulation space HS to the heat insulation space HS. The sealing mechanism 70 is disposed between the heat insulation space HS and the gland space GS to thereby prevent the gland steam in the gland space GS from flowing into the heat insulation space HS. Specifically, in this embodiment, the amount of steam flowing into the heat insulation space HS from the outside per unit time is smaller than the amount of steam (gland steam) flowing into the gland space GS from the outside per unit time.

[0036] The dimension Wa of the heat insulation space HS in the radial direction of the shaft of the turbine rotor 2 is smaller than the distance W1 between the outer surface of the shaft member 21 and the first region 61 and the distance W2 between the outer surface of the shaft member 21 and the second region 62. The heat insulation space HS is a very small space formed in the boundary region between the turbine casing 4 and the outer gland 51.

[0037] FIG. 5 is a diagram illustrating an example of the sealing mechanism 70 according to this embodiment. The sealing mechanism 70 includes a secured member 71 secured to the inner surface of the outer gland 51 and having an inner space, an elastic member 72, such as a flat spring, disposed in the inner space of the secured member 71, and a sealing member 73, at least part of which is disposed in the inner space of the secured member 71. The secured member 71 has an opening 74 that connects the inner space of the secured member 71 to its outer space. At least part of the sealing member 73 is disposed in the opening 74. A part of the sealing member 73 is disposed in the inner space of the secured member 71, and another part of the sealing member 73 is disposed in the outer space of the secured member 71 through the opening 74. In the inner space of the secured member 71, the elastic member 72 is disposed between the outer gland 51 and the sealing member 73. The elastic member 72 generates a force (urging force) that causes the sealing member 73 to be pressed against the inner gland 52 (the protrusion 55). Sufficient contact between the sealing member 73 and the inner gland 52 is thereby obtained. Therefore, the outflow of gas in the heat insulation space HS and the flow of steam in the gland space GS into the heat insulation space HS are prevented.

[0038] The heat insulation space HS described with reference to FIG. 2 etc. is formed on a first side (+X side), with respect to the X axis direction, of the turbine casing space SP. As shown in FIG. 1, another gland casing 5 including the outer gland 51 and the inner gland 52 is disposed on a second side (-X side), with respect to the X axis direction, of the turbine casing space SP, and another heat insulation space HS is formed. In the gland casing 5 disposed on the second side (-X side) of the turbine casing space SP, the heat insulation space HS is defined by the first region 61 of the inner surface of the turbine casing 4 and the second region 62 of the outer gland 51. The first region 61 of the inner surface of the turbine casing 4 includes a second end portion, with respect to the X axis direction, of the inner surface of the turbine casing 4 (the end portion on the -X side). The second region 62 of the outer gland 51 includes a first end portion of the inner surface of the outer gland 51 that is adjacent to the second end portion of the inner surface of the turbine casing 4 (the first end portion of the outer gland 51 is the end portion on the +X side). The first region 61 and the second region 62 form a boundary region between the turbine casing 4 and the outer gland 51 on the second side (-X side) of the turbine casing space SP with respect to the X axis direction. The heat insulation space HS is formed between the first region 61 of the turbine casing 4, the second region 62 of the outer gland 51, the inner gland 52, and the sealing mechanism 70, the inner gland 52 and the sealing mechanism 70 being disposed on the second side (-X side) of the turbine casing space SP with respect to the X axis direction.

[0039] Next, the operation of the steam turbine 1 according to this embodiment will be described. High-temperature high-pressure steam (main steam) is supplied to the turbine casing space SP through a steam supply port 23. The steam supplied to the turbine casing space SP rotates the turbine rotor 2. In addition, gland steam is supplied to the gland spaces GS through the supply ports 81.

[0040] Since the main steam is supplied to the turbine casing space SP and the gland steam is supplied to the gland spaces GS, the difference in temperature between the turbine casing 4 and each of the outer glands 51 may become large. When the difference in temperature between the turbine casing 4 and an outer gland 51 becomes large with the turbine casing 4 connected to the outer gland 51, the difference in the amount of thermal deformation between the turbine casing 4 and the outer gland 51 may become large. In this case, sufficient pressure (contact pressure) may not be ensured on the mating surface P3 at which the joint surface Pa3 of the upper outer gland 51A mates with the joint surface Pb3 of the lower outer gland 51B. For example, even when the temperature of the turbine casing 4 becomes high and the amount of thermal deformation of the turbine casing 4 becomes large, the temperature of the outer gland 51 may not become as high as the temperature of the turbine casing 4, and the amount of thermal deformation of the outer gland 51 may be small. In this case, a force may act on the outer gland 51 as the turbine casing 4 is thermally deformed. For example, a force may act on at least one of the upper outer gland 51A and the lower outer gland 51B such that the joint surface Pa3 and the joint surface Pb3 are separated from each other. Therefore, steam (gland steam) may leak from the gap between the joint surface Pa3 of the upper outer gland 51A and the joint surface Pb3 of the lower outer gland 51B.

[0041] In this embodiment, the heat insulation spaces HS disposed in the boundary regions between the turbine casing 4 and the outer glands 51 from increasing in the vicinities of the boundary regions between the turbine casing 4 and the outer glands 51.

[0042] FIG. 6 is a diagram illustrating an example of a steam turbine 1J according to a comparative example. The steam turbine 1J according to the comparative example has no heat insulation space HS.

[0043] FIG. 7 is a schematic diagram illustrating the distribution of temperature in the turbine casing 4 and an outer gland 51 in the steam turbine 1J according to the comparative example when main steam is supplied to the turbine casing space SP and gland steam is supplied to the gland spaces GS. FIG. 7 shows the temperature distribution in a cross section parallel to the XY plane and near the boundary region between the turbine casing 4 and the outer gland 51. As shown in FIG. 7, in the steam turbine 1J according to the comparative example, it can be seen that the difference in temperature between the turbine casing 4 and the outer gland 51 is large in the vicinity of the boundary region between the turbine casing 4 and the outer gland 51.

[0044] FIG. 8 is a diagram illustrating the distribution of temperature in the turbine casing 4 and the outer gland 51 in the steam turbine 1 according to the embodiment when main steam is supplied to the turbine casing space SP of the steam turbine 1 and gland steam is supplied to the gland spaces GS. FIG. 8 shows the temperature distribution in a cross section parallel to the XY plane and near the boundary region between the turbine casing 4 and the outer gland 51. As shown in FIG. 8, in the steam turbine 1 according to this embodiment, since the heat insulation space HS for inhibiting the flow of steam is disposed in the boundary region between the turbine casing 4 and the outer gland 51, the difference in temperature between the turbine casing 4 and the outer gland 51 is prevented from increasing in the vicinity of the boundary region between the turbine casing 4 and the outer gland 51.

[0045] Leakage of the steam from the mating surfaces P3 in the steam turbine 1 according to this embodiment is smaller than leakage of the steam from the mating surfaces P3 in the steam turbine 1J according to the comparative example.

[0046] This may be because the gland steam supplied to the gland spaces GS is not supplied to the boundary regions between the turbine casing 4 and the outer glands 51 (the first regions 61 and the second regions 62) and therefore the difference in temperature between the turbine casing 4 and the outer glands 51 is prevented from increasing. Specifically, when the gland steam in the gland spaces GS flows near the boundary regions between the turbine casing 4 and the outer glands 51, an increase in the temperature of the outer glands 51 that is caused by the gland steam in the gland spaces GS may be prevented. More specifically, when the gland steam flows so as to come into contact with the first regions 61 and the second regions 62, the gland steam may cause a phenomenon in which the temperature of the outer glands 51 near the boundary regions is not as high as the temperature of the turbine casing 4.

[0047] In this embodiment, the heat insulation spaces HS prevent the gland steam in the gland spaces GS from flowing in the vicinities of the boundary regions between the turbine casing 4 and the outer glands 51. In other words, since the first regions 61 and the second regions 62 forming the boundary regions between the turbine casing 4 and the outer glands 51 are protected by the heat insulation spaces HS, the gland steam in the gland spaces GS is prevented from flowing in contact with the first regions 61 and the second regions 62. Therefore, the occurrence of the phenomenon in which the temperature of the outer glands 51 is prevented from increasing in the vicinities of the boundary regions is suppressed. The heat of the turbine casing 4 is transferred to the outer glands 51 through the mating surfaces P3 etc., and the temperature of the outer glands 51 thereby increases. This may prevent the difference in temperature between the turbine casing 4 and the outer glands 51 from increasing in the vicinities of the boundary regions.

[0048] Since the difference in temperature between the turbine casing 4 and the outer glands 51 is prevented from increasing in the vicinities of the boundary regions between the turbine casing 4 and the outer glands 51, a force that causes separation of the joint surfaces Pa3 from the joint surfaces Pb3 when the turbine casing 4 is thermally deformed is prevented from acting on the outer glands 51. Specifically, the difference in temperature between the turbine casing 4 and the outer glands 51 is small. Therefore, when the turbine casing 4 is thermally deformed, the outer glands 51 are also thermally deformed with the amount of thermal deformation of the outer glands 51 being substantially the same as the amount of thermal deformation of the turbine casing 4. This prevents a force causing separation of the joint surfaces Pa3 from the joint surfaces Pb3 from acting on the outer glands 51. Therefore, leakage of the steam (gland steam) from gaps between the joint surfaces Pa3 of the upper outer glands 51A and the joint surfaces Pb3 of the lower outer glands 51B is prevented.

[0049] As described above, in this embodiment, the heat insulation spaces HS in which the flow of steam is inhibited are formed in the boundary regions between the turbine casing 4 and the outer glands 51, so that the difference in temperature between the turbine casing 4 and the outer glands 51 is prevented from increasing in the boundary regions (joint portions, connection portions) between the turbine casing 4 and the outer glands 51. Therefore, the difference in the amount of thermal deformation between the turbine casing 4 and the outer gland 51 is prevented from increasing in the vicinities of the boundary regions. This can prevent leakage of the steam from the mating surfaces P3 at which the joint surfaces Pa3 of the upper outer glands 51A of the outer glands 51 mate with the joint surfaces Pb3 of the lower outer glands 51B.

[0050] In this embodiment, the outer gland 51 can be separated at the joint surface P3, into the upper outer gland 51A and the lower outer gland 51B, and this can facilitate, for example, maintenance of the steam turbine 1.

[0051] In this embodiment, the heat insulation spaces HS are formed so as to surround the shaft of the turbine rotor 2. This can prevent the difference in temperature between the turbine casing 4 and the outer glands 51 from increasing in the vicinities of the boundary regions between the turbine casing 4 and the outer glands 51.

[0052] In this embodiment, the dimension Wa of the heat insulation spaces HS in the radial direction of the shaft of the turbine rotor 2 is smaller than the distance W1 from the outer surface of the shaft member 21 to the first regions 61 and is also smaller than the distance W2 from the outer surface of the shaft member 21 to the second regions 62. Therefore, while the gland spaces GS to which the gland steam is supplied are ensured, very small heat insulation spaces HS can be formed in the boundary regions between the turbine casing 4 and the outer glands 51.

[0053] In this embodiment, the heat insulation spaces HS are hermetically, sealed spaces. Therefore, the flow of steam is sufficiently inhibited in the heat insulation spaces HS, and a high heat insulation effect can thereby be obtained.

[0054] In this embodiment, the turbine casing 4 is separated into the upper turbine casing 4A and the lower turbine casing 4B. Since the turbine casing 4, as well as the outer glands 51, is separable, for example, maintenance of the steam turbine 1 can be smoothly performed.

[0055] In this embodiment, a plurality of heat insulation spaces HS may be formed around the shaft of the turbine rotor 2, or a heat insulation space HS may be formed only in the vicinity of each mating surface P3.

[0056] In this embodiment, each heat insulation space HS may be completely sealed hermetically or may not be sealed hermetically. Each heat insulation space HS may be a closed space or a semi-closed space. For example, the sealing mechanism 70 may completely seal the gap between the facing surface 56 and the inner surface of the outer gland 51, or a gap may be formed between the sealing mechanism 70 and one or both of the facing surface 56 and the outer gland 51. Specifically, it is only necessary that the flow of steam be more inhibited in the heat insulation spaces HS than in the gland spaces GS.

[0057] In this embodiment, the facing surfaces 56 are disposed in the protrusions 55 provided in the inner glands 52. However, the facing surfaces 56 may be disposed in, for example, the outer glands 51. For example, each outer gland 51 may include a protrusion protruding toward the center, with respect to the X axis direction, of the turbine casing space SP, and the protrusion may have a facing surface 56. The space-forming members for forming the heat insulation spaces HS between the space-forming members, the first regions 61, and the second regions 62 may be members different from the outer glands 51 and the inner glands 52. For example, members different from the outer glands 51 and the inner glands 52 may be disposed in the gland spaces GS so as to face the first regions 61 and the second regions 62.

Reference Signs List

[0058] 

1

steam turbine

2

turbine rotor

3

casing

4

turbine casing

4A

upper turbine casing

4B

lower turbine casing

5

gland casing

21

shaft member

22

seal

24

opening

51

outer gland

51A

upper outer gland

51B

lower outer gland

52

inner gland

53

connection section

56

facing surface

61

first region

62

second region

70

sealing mechanism

GS

gland space

HS

heat insulation space

SP

turbine casing space

Claims

1. A steam turbine comprising:

a turbine rotor (2) including a shaft member (21) and a plurality of seals (22) connected to the shaft member (21), the shaft member (21) extending in an axial direction (X axis);

a turbine casing (4) disposed around the turbine rotor (2) with a turbine casing space (SP) formed between the turbine casing (4) and the turbine rotor (2); and

a gland casing (5) connected to an axial end of the turbine casing (4) and including an outer gland (51) axially disposed so as to close an opening (24) at an axial end of the turbine casing space (SP) from the outside, and an inner gland (52) axially disposed so as to provide a gland space (GS) between the inner gland (52) and the outer gland (51),

wherein the outer gland (51) and the inner gland (52) each include a first annular section having a first joint surface (Pa3) and a second annular section having a second joint surface (Pb3) joined to the first joint surface, the first annular section being disposed around a part of the turbine rotor (2), the second annular section being disposed around another part of the turbine rotor (2), and

wherein a gland steam is supplied into the gland space (GS) and said plurality of seals (22) is provided between the shaft member (21) and the inner gland (52) and between the shaft member (21) and the outer gland (51), and

wherein the inner gland (52) includes an annular protrusion (55) extending in an axial direction from the inner gland (52) toward the outer gland (51);

the steam turbine further comprising:

a heat insulation space (HS) defined by a radially inner surface of the turbine casing (4), a radially inner surface of the outer gland (51), the inner gland (52) including a radially outer facing surface (56) of the protrusion (55), and a sealing mechanism (70),

wherein the sealing mechanism (70) is disposed between the radially inner surface of the outer gland (51) and the radially outer facing surface (56) of the protrusion (55) to prevent the gland steam in the gland space (GS) from flowing into the heat insulation space (HS).

2. The steam turbine according to claim 1, wherein the heat insulation space (HS) is formed so as to surround the shaft member (21).

3. The steam turbine according to claim 1 or claim 2, wherein the heat insulation space (HS) is a hermetically sealed space.

4. The steam turbine according to any one of claims 1 to 3, wherein the turbine casing (4) includes: a first turbine casing section (4A) disposed around a part of the turbine rotor and a second turbine casing section (4B) disposed around another part of the turbine rotor, the first and second turbine casing sections being connected to each other to form the turbine casing (4).

Ansprüche

1. Dampfturbine, umfassend:

einen Turbinenrotor (2), der ein Wellenelement (21) und eine Vielzahl von Dichtungen (22) einschließt, die mit dem Wellenelement (21) verbunden sind, wobei sich das Wellenelement (21) in eine axiale Richtung (X-Achse) erstreckt;

ein Turbinengehäuse (4), das um den Turbinenrotor (2) herum mit einem Turbinengehäuseraum (SP) angeordnet ist, der zwischen dem Turbinengehäuse (4) und dem Turbinenrotor (2) gebildet ist; und

ein Stopfbuchsengehäuse (5), das mit einem axialen Ende des Turbinengehäuses (4) verbunden ist und eine äußere Stopfbuchse (51) einschließt, die axial so angeordnet ist, dass sie eine Öffnung (24) an einem axialen Ende des Turbinengehäuseraums (SP) von der Außenseite her verschließt, und eine innere Stopfbuchse (52), die axial so angeordnet ist, dass ein Stopfbuchsenraum (GS) zwischen der inneren Stopfbuchse (52) und der äußeren Stopfbuchse (51) bereitgestellt wird,

wobei die äußere Stopfbuchse (51) und die innere Stopfbuchse (52) jede einen ersten ringförmigen Abschnitt einschließen, der eine erste Fügefläche (Pa3) aufweist, und einen zweiten ringförmigen Abschnitt, der eine zweite Fügefläche (Pb3) aufweist, die mit der ersten Fügefläche aneinandergefügt ist, wobei der erste ringförmige Abschnitt um einen Teil des Turbinenrotors (2) herum angeordnet ist, wobei der zweite ringförmige Abschnitt um einen anderen Teil des Turbinenrotors (2) herum angeordnet ist, und

wobei ein Stopfbuchsendampf in den Stopfbuchsenraum (GS) zugeführt wird und die Vielzahl von Dichtungen (22) zwischen dem Wellenelement (21) und der inneren Stopfbuchse (52) und zwischen dem Wellenelement (21) und der äußeren Stopfbuchse (51) bereitgestellt sind, und

wobei die innere Stopfbuchse (52) einen ringförmigen Vorsprung (55) einschließt, der sich in eine axiale Richtung von der inneren Stopfbuchse (52) in Richtung der äußeren Stopfbuchse (51) erstreckt;

wobei die Dampfturbine weiter umfasst:

einen Wärmeisolierraum (HS), der durch eine radiale Innenfläche des Turbinengehäuses (4) definiert ist, eine radiale Innenfläche der äußeren Stopfbuchse (51), die innere Stopfbuchse (52), die eine radiale, nach außen gewandte Fläche (56) des Vorsprungs (55) einschließt, und einen Dichtungsmechanismus (70),

wobei der Dichtungsmechanismus (70) zwischen der radialen Innenfläche der äußeren Stopfbuchse (51) und der radialen, nach außen gewandten Fläche (56) des Vorsprungs (55) angeordnet ist, um den Stopfbuchsendampf im Stopfbuchsenraum (GS) daran zu hindern, in den Wärmeisolierraum (HS) zu strömen.

2. Dampfturbine nach Anspruch 1, wobei der Wärmeisolierraum (HS) so gebildet ist, dass er das Wellenelement (21) umgibt.

3. Dampfturbine nach Anspruch 1 oder Anspruch 2, wobei der Wärmeisolierraum (HS) ein hermetisch abgedichteter Raum ist.

4. Dampfturbine nach einem der Ansprüche 1 bis 3, wobei das Turbinengehäuse (4) einschließt: einen ersten Turbinengehäuseabschnitt (4A), der um einen Teil des Turbinenrotors herum angeordnet ist, und einen zweiten Turbinengehäuseabschnitt (4B), der um einen anderen Teil des Turbinenrotors herum angeordnet ist, wobei der erste und zweite Turbinengehäuseabschnitt miteinander verbunden sind, um das Turbinengehäuse (4) zu bilden.

Revendications

1. Turbine à vapeur comprenant :

un rotor de turbine (2) incluant un élément formant arbre (21) et une pluralité de joints (22) reliés à l'élément formant arbre (21), l'élément formant arbre (21) s'étendant dans une direction axiale (axe des X) ;

une enveloppe de turbine (4) disposée autour du rotor de turbine (2) avec un espace d'enveloppement de turbine (SP) formé entre l'enveloppe de turbine (4) et le rotor de turbine (2) ; et

une enveloppe de presse-étoupe (5) reliée à une extrémité axiale de l'enveloppe de turbine (4) et incluant un presse-étoupe extérieur (51) disposé de façon axiale afin de fermer une ouverture (24) au niveau d'une extrémité axiale de l'espace d'enveloppement de turbine (SP) à partir de l'extérieur, et un presse-étoupe intérieur (52) disposé de façon axiale afin de fournir un espace de presse-étoupe (GS) entre le presse-étoupe intérieur (52) et le presse-étoupe extérieur (51),

dans lequel le presse-étoupe extérieur (51) et le presse-étoupe intérieur (52) incluent chacun une première section annulaire ayant une première surface de joint (Pa3) et une seconde section annulaire ayant une seconde surface de joint (Pb3) jointe à la première surface de joint, la première section annulaire étant disposée autour d'une partie du rotor de turbine (2), la seconde section annulaire étant disposée autour d'une autre partie du rotor de turbine (2), et

dans laquelle une vapeur de presse-étoupe est fournie dans l'espace de presse-étoupe (GS) et ladite pluralité de joints (22) est prévue entre l'élément formant arbre (21) et le presse-étoupe intérieur (52) et entre l'élément formant arbre (21) et le presse-étoupe extérieur (51), et

dans lequel le presse-étoupe intérieur (52) inclut une protubérance annulaire (55) s'étendant dans une direction axiale à partir du presse-étoupe intérieur (52) vers le presse-étoupe extérieur (51) ;

la turbine à vapeur comprenant en outre :

un espace d'isolation thermique (HS) défini par une surface intérieure de façon radiale de l'enveloppe de turbine (4), une surface intérieure de façon radiale du presse-étoupe extérieur (51), le presse-étoupe intérieur (52) incluant une surface opposée extérieure de façon radiale (56) de la protubérance (55) et un mécanisme d'étanchéité (70),

dans lequel le mécanisme d'étanchéité (70) est disposé entre la surface intérieure de façon radiale du presse-étoupe extérieur (51) et la surface opposée extérieure de façon radiale (56) de la protubérance (55) pour empêcher la vapeur de presse-étoupe dans l'espace de presse-étoupe (GS) de s'écouler dans l'espace d'isolation thermique (HS).

2. Turbine à vapeur selon la revendication 1, dans laquelle l'espace d'isolation thermique (HS) est formé afin d'entourer l'élément formant arbre (21).

3. Turbine à vapeur selon la revendication 1 ou la revendication 2, dans laquelle l'espace d'isolation thermique (HS) est un espace hermétiquement scellé.

4. Turbine à vapeur selon l'une quelconque des revendications 1 à 3, dans laquelle l'enveloppe de turbine (4) inclut : une première section d'enveloppe de turbine (4A) disposée autour d'une partie du rotor de turbine et une seconde section d'enveloppe de turbine (4B) disposée autour d'une autre partie du rotor de turbine, les première et seconde sections d'enveloppe de turbine étant reliées l'une à l'autre pour former l'enveloppe de turbine (4).

Drawing