JPH05902U - Low-pressure cabin of steam turbine - Google Patents
Low-pressure cabin of steam turbineInfo
- Publication number
- JPH05902U JPH05902U JP5667291U JP5667291U JPH05902U JP H05902 U JPH05902 U JP H05902U JP 5667291 U JP5667291 U JP 5667291U JP 5667291 U JP5667291 U JP 5667291U JP H05902 U JPH05902 U JP H05902U
- Authority
- JP
- Japan
- Prior art keywords
- pressure partition
- partition wall
- pressure
- plate structure
- reinforcing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000005192 partition Methods 0.000 claims abstract description 48
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 29
- 238000003466 welding Methods 0.000 claims abstract description 4
- 238000000605 extraction Methods 0.000 description 5
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910001208 Crucible steel Inorganic materials 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
(57)【要約】
【目的】 内車室の熱変形を小さくして、内部の蒸気リ
ークを減少する。
【構成】 蒸気入口1において複数段の静翼6aを支持
する板構造の翼環5aと板構造の第1の圧力隔壁4aと
を溶接により一体化する。第2,第3の圧力隔壁4b,
4c間に取付ける補強リブ9を分離する。第1,第2の
圧力隔壁4a,4b間には、補強リブではなくて、パイ
プ等の補強棒15を設ける。第1,第2,第3の圧力隔
壁4a,4b,4cをそれぞれ内車室3と一体に設け
る。
(57) [Abstract] [Purpose] To reduce the thermal deformation of the inner passenger compartment and reduce the internal steam leak. [Structure] A blade ring 5a having a plate structure for supporting a plurality of stages of stationary blades 6a at a steam inlet 1 and a first pressure partition wall 4a having a plate structure are integrated by welding. Second and third pressure partition walls 4b,
The reinforcing ribs 9 attached between the 4c are separated. A reinforcing rod 15 such as a pipe is provided between the first and second pressure partition walls 4a and 4b instead of a reinforcing rib. The first, second and third pressure partition walls 4a, 4b and 4c are provided integrally with the inner casing 3, respectively.
Description
【0001】[0001]
本考案は、蒸気タービンの低圧車室に関し、更に詳細にはその翼環と圧力隔壁 の構造に関する。 BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a low pressure casing of a steam turbine, and more particularly to the structure of its blade ring and pressure partition.
【0002】[0002]
図2は従来より使用されている蒸気タービン低圧車室の上半部の一例を示し、 蒸気入口1より低圧車室に入った蒸気流2は、内車室3により第1の圧力隔壁4 aを介して支持される翼環5aに嵌め込まれた複数段の静翼6a、該第1の圧力 隔壁4aと一体に形成された第2の圧力隔壁4aと一体化した板構造の翼環5b で支持された複数段の静翼6b、内車室3と一体に形成された第3の圧力隔壁4 cと一体化した板構造の翼環5cで支持された静翼6c、及び内車室3で支持さ れた静翼6dを経て動翼7に噴出し、ロータ8を回転させる。また、補強リブ9 が圧力隔壁4aと4b、4bと4cとの間及び内車室3と圧力隔壁4cとの間に それぞれ設けられている。なお、10は外車室、11は第1抽気室、12は第2 抽気室、13は補強材である。 FIG. 2 shows an example of the upper half of a steam turbine low-pressure casing that has been conventionally used. The steam flow 2 entering the low-pressure casing from the steam inlet 1 is caused to flow into the first pressure partition wall 4 a by the inner casing 3. A plurality of stages of stationary blades 6a fitted into a blade ring 5a supported via a blade ring 5b having a plate structure integrated with a second pressure partition wall 4a integrally formed with the first pressure partition wall 4a. A plurality of stationary vanes 6b supported, a stationary vane 6c supported by a blade ring 5c having a plate structure integrated with a third pressure partition wall 4c integrally formed with the inner casing 3, and the inner casing 3 It is jetted to the moving blade 7 through the stationary blade 6d supported by and the rotor 8 is rotated. Reinforcing ribs 9 are provided between the pressure partition walls 4a and 4b, 4b and 4c and between the inner casing 3 and the pressure partition wall 4c, respectively. In addition, 10 is an outer car room, 11 is a 1st extraction chamber, 12 is a 2nd extraction chamber, and 13 is a reinforcing material.
【0003】[0003]
以上述べた従来の蒸気タービンの低圧車室の構造は、しかし、次のような問題 点があった。 However, the structure of the low-pressure casing of the conventional steam turbine described above, however, has the following problems.
【0004】 (1) 蒸気入口1部の蒸気流2は、仕事を終えて内車室3から出る蒸気流14に 比べて高温なので、加熱された圧力隔壁4a〜4cの熱膨張により内車室3の全 体が変形し、そのため、内部の蒸気リークが増加して、性能低下が生じる。すな わち、蒸気入口1において複数段の静翼6aを支持する翼環5aと第1の圧力隔 壁4aとの嵌合部Aでは、軸方向変位(波打ち変形)が生じ、該嵌合部Aに隙間 が生じて蒸気2′がリークする。また、静翼6a〜6cが溶接されている箇所で は、半径方向変位(オーバル変形)が問題となる。つまり、静翼6a〜6dとロ ータ8との間および動翼7と静翼6a〜6dとの間の隙間が不均一となり、蒸気 リークが増大したり、あるいはフィン接触トラブルを発生したりする。(1) Since the steam flow 2 at the steam inlet 1 is higher in temperature than the steam flow 14 exiting from the inner casing 3 after finishing work, thermal expansion of the heated pressure partition walls 4a to 4c causes the inner casing to expand. The whole of No. 3 is deformed, so that the steam leak inside increases and the performance deteriorates. That is, at the fitting portion A between the blade ring 5a that supports the plurality of stages of stationary blades 6a at the steam inlet 1 and the first pressure partition wall 4a, axial displacement (waviness deformation) occurs, and the fitting A gap is created in the portion A and the steam 2'leaks. Further, radial displacement (oval deformation) becomes a problem at the places where the stationary blades 6a to 6c are welded. That is, the gaps between the stationary blades 6a to 6d and the rotor 8 and between the moving blade 7 and the stationary blades 6a to 6d become non-uniform, resulting in increased steam leakage or fin contact trouble. To do.
【0005】 (2) 第1、第2の圧力隔壁4a、4bと内車室3との接合部Bおよび各圧力隔 壁4a〜4cと補強リブ9との接合部に高応力が生じ、強度が低下する。(2) High stress is generated at the joint B between the first and second pressure partition walls 4a and 4b and the inner casing 3 and at the joints between the respective pressure partition walls 4a to 4c and the reinforcing ribs 9, and the strength is increased. Is reduced.
【0006】 (3) 蒸気入口1において複数段の静翼6aを支持する翼環5aは、厚板材の機 械加工材又は鋳鋼品であり、コストがかかる。(3) The blade ring 5a that supports the plurality of stages of the stationary blades 6a at the steam inlet 1 is a machined material of a thick plate material or a cast steel product and is costly.
【0007】 本考案は、このような従来技術の課題を解決するためになされたもので、内車 室の熱変形を小さくして内部の蒸気リークを減少し、また部品数を少なくしてコ ストを安くするようにした蒸気タービンの低圧車室を提供することを目的とする 。The present invention has been made in order to solve the problems of the prior art as described above, and reduces thermal deformation of the inner casing to reduce internal steam leakage, and reduces the number of parts to reduce The purpose is to provide a low-pressure passenger compartment of a steam turbine that has a low strike.
【0008】[0008]
上記の課題を解決するために、本考案は、蒸気タービンの低圧車室における蒸 気入口において複数段の静翼を支持する板構造の翼環と板構造の第1の圧力隔壁 とを溶接により一体化するとともに、該第1の圧力隔壁とこれに隣接する板構造 の第2の圧力隔壁との間及び該第2の圧力隔壁とこれに隣接する板構造の第3の 圧力隔壁との間の一方に取り付けられる補強リブを分離し、かつ他方には補強リ ブに代えて補強棒を設け、前記第1,第2及び第3の圧力隔壁をそれぞれ内車室 と一体に設けたものである。 In order to solve the above-mentioned problems, the present invention is to weld a blade ring of a plate structure supporting a plurality of stages of stationary blades at a steam inlet in a low pressure casing of a steam turbine and a first pressure partition wall of the plate structure by welding. Between the first pressure partition wall and the second pressure partition wall of the plate structure adjacent to the first pressure partition wall, and between the second pressure partition wall and the third pressure partition wall of the plate structure adjacent to the first pressure partition wall. A reinforcing rib attached to one of the above is separated, and a reinforcing rod is provided to the other in place of the reinforcing rib, and the first, second and third pressure partition walls are respectively provided integrally with the inner casing. is there.
【0009】[0009]
上記の手段によれば、高温の蒸気流によって最初に加熱される第1の圧力隔壁 と翼環、静翼とを一体化し、かつ第1、第2及び第3のいずれかの圧力隔壁間の 設けられる補強リブを分離するとともに、他の圧力隔壁間は熱変形拘束をやわら げる補強棒で接合しているので、熱膨張による内車室の変形が小さくなり、内部 の蒸気リークが減少する。 According to the above means, the first pressure partition, which is first heated by the high-temperature steam flow, is integrated with the blade ring and the stationary blade, and the pressure partition between any one of the first, second, and third pressure partitions is integrated. Since the reinforcing ribs provided are separated and the other pressure bulkheads are joined by reinforcing rods that relieve the thermal deformation constraint, the deformation of the inner casing due to thermal expansion is reduced and the internal steam leak is reduced. To do.
【0010】 また、該補強棒は補強リブに比べてその接合部の応力が小さいので、疲労強度 が向上する。そして、第1の圧力隔壁と翼環、複数段の静翼とを一体化している ので、部品数が減少する。Further, since the stress of the joining portion of the reinforcing rod is smaller than that of the reinforcing rib, the fatigue strength is improved. Further, since the first pressure partition wall, the blade ring, and the plurality of stages of stationary blades are integrated, the number of parts is reduced.
【0011】[0011]
以下、図1を参照して本考案の一実施例について詳細に説明する。なお、図1 において、図2に示したものと同一の部分には同一の符号を付して、重複する説 明は省略する。 Hereinafter, an embodiment of the present invention will be described in detail with reference to FIG. Note that, in FIG. 1, the same parts as those shown in FIG. 2 are denoted by the same reference numerals, and overlapping description will be omitted.
【0012】 図1に示すように、本実施例によれば、蒸気入口1において複数段の静翼6a を支持する翼環5aは板構造とされ、この翼環5aと同じく板構造の第1の圧力 隔壁4aとが溶接により一体化されている。As shown in FIG. 1, according to the present embodiment, the blade ring 5a that supports the plurality of stages of stationary blades 6a at the steam inlet 1 has a plate structure. The partition wall 4a is integrated by welding.
【0013】 また、第2抽気室12における第2の圧力隔壁4bと第3の圧力隔壁4cとの 間に取り付けられる補強リブ9は分離されていて、それぞれ第2、第3の圧力隔 壁4b、4cに取り付けられている。そして、第1抽気室11における第1の圧 力隔壁4aと第2の圧力隔壁4bとの間には、補強リブ9に代えて、パイプ等の 補強棒15が複数本設けられている。Further, the reinforcing ribs 9 attached between the second pressure partition wall 4b and the third pressure partition wall 4c in the second bleed chamber 12 are separated, and the second and third pressure partition walls 4b are separated from each other. , 4c. A plurality of reinforcing rods 15 such as pipes are provided in place of the reinforcing ribs 9 between the first pressure partition wall 4a and the second pressure partition wall 4b in the first extraction chamber 11.
【0014】 このような本実施例の構成によれば、高温の蒸気流2によって最初に加熱され る第1の圧力隔壁4aと翼環5a、静翼6aとを一体化し、かつ第2、第3の圧 力隔壁4b、4c間に設けられる補強リブ9を分離するとともに、第1、第2の 圧力隔壁4a、4b間は熱変形拘束をやわらげる補強棒15で接合しているので 、熱膨張による内車室3の変形が小さくなり、内部の蒸気リークが減少する。According to such a configuration of this embodiment, the first pressure partition wall 4a, which is first heated by the high-temperature steam flow 2, the blade ring 5a, and the stationary blade 6a are integrated, and the second and second blades are integrated. The reinforcing ribs 9 provided between the three pressure partition walls 4b and 4c are separated, and the first and second pressure partition walls 4a and 4b are joined by the reinforcing rod 15 that softens the thermal deformation restraint. As a result, the deformation of the inner casing 3 is reduced, and the steam leak inside is reduced.
【0015】 また、補強棒15は補強リブ9に比べてその接合部の応力が小さいので、疲労 強度が向上する。そして、第1の圧力隔壁4aと、翼環5a、複数段の静翼6a とを一体化しているので、部品数が減少する。Further, the reinforcing bar 15 has a smaller stress at the joint portion than the reinforcing rib 9, so that the fatigue strength is improved. Further, since the first pressure partition wall 4a, the blade ring 5a, and the plurality of stages of stationary blades 6a are integrated, the number of parts is reduced.
【0016】 なお、変形例として、第1、第2の圧力隔壁4a、4b間に補強リブ9を分離 して設け、第2、第3の圧力隔壁4b、4c間に補強棒15を設けても、実質的 に同様な作用効果が得られる。As a modified example, reinforcing ribs 9 are provided separately between the first and second pressure partition walls 4a and 4b, and a reinforcing rod 15 is provided between the second and third pressure partition walls 4b and 4c. Also, substantially the same effect can be obtained.
【0017】[0017]
以上述べたように、本考案によれば、蒸気タービンの低圧車室における高温領 域を一体化し、圧力隔壁間に取り付けられる補強リブを分離し、さらに、熱変形 拘束をやわらげる補強棒を設ける構成としたので、内車室の熱変形が小さくなり 、内部の蒸気リークが減少する。その結果、タービン性能が向上する。 As described above, according to the present invention, the high-temperature region in the low-pressure casing of the steam turbine is integrated, the reinforcing ribs mounted between the pressure bulkheads are separated, and the reinforcing rod for softening the thermal deformation restraint is provided. As a result, the thermal deformation of the inner compartment is reduced, and the steam leak inside is reduced. As a result, turbine performance is improved.
【0018】 また、圧力隔壁間を接合する補強棒の接合部の応力が小さくなり、疲労強度が 向上する。そして、第1の圧力隔壁と、翼環、複数段の静翼とを一体化したので 、部品数が減少するとともに、静翼保持部が板構造であるため重量が低減し、コ ストが減少する。Further, the stress of the joint portion of the reinforcing rod for joining the pressure partition walls is reduced, and the fatigue strength is improved. Further, since the first pressure partition wall, the blade ring, and the plurality of stages of stationary vanes are integrated, the number of parts is reduced, and since the stationary vane holding portion has a plate structure, the weight is reduced and the cost is reduced. To do.
【図1】本考案の一実施例に係る蒸気タービンの低圧車
室を示す、車室上半部の断面図である。FIG. 1 is a cross-sectional view of an upper half of a passenger compartment showing a low-pressure passenger compartment of a steam turbine according to an embodiment of the present invention.
【図2】従来の蒸気タービンの低圧車室を示す、車室上
半部の断面図である。FIG. 2 is a cross-sectional view of the upper half of the passenger compartment showing a low-pressure passenger compartment of a conventional steam turbine.
【符号の説明】 1 蒸気入口 2 蒸気流 3 内車室 4a〜4c 圧力隔壁 5a〜5c 翼環 6a〜6d 静翼 7 動翼 8 ロータ 9 補強リブ 10 外車室 11 抽気室 12 抽気室 13 補強材 14 蒸気流 15 補強棒[Explanation of Codes] 1 steam inlet 2 steam flow 3 inner casing 4a-4c pressure partition wall 5a-5c blade ring 6a-6d stationary blade 7 moving blade 8 rotor 9 reinforcing rib 10 outer casing 11 extraction chamber 12 extraction chamber 13 reinforcement 14 Steam flow 15 Reinforcing rod
Claims (1)
板構造の翼環と板構造の第1の圧力隔壁とを溶接により
一体化するとともに、該第1の圧力隔壁とこれに隣接す
る板構造の第2の圧力隔壁との間及び該第2の圧力隔壁
とこれに隣接する板構造の第3の圧力隔壁との間の一方
に取り付けられる補強リブを分離し、かつ他方には補強
リブに代えて補強棒を設け、前記第1,第2及び第3の
圧力隔壁をそれぞれ内車室と一体に設けたことを特徴と
する蒸気タービンの低圧車室。Claims for utility model registration: 1. A blade ring having a plate structure for supporting a plurality of stages of stationary blades at a steam inlet and a first pressure partition wall having a plate structure are integrated by welding, and the first Reinforcing ribs attached to one of the pressure partition wall and the second pressure partition wall of the plate structure adjacent thereto and between the second pressure partition wall and the third pressure partition wall of the plate structure adjacent thereto. A low pressure casing for a steam turbine, characterized in that a reinforcing rod is provided on the other side instead of a reinforcing rib, and the first, second and third pressure partition walls are provided integrally with the inner casing. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5667291U JPH085285Y2 (en) | 1991-06-25 | 1991-06-25 | Low-pressure cabin of steam turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5667291U JPH085285Y2 (en) | 1991-06-25 | 1991-06-25 | Low-pressure cabin of steam turbine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH05902U true JPH05902U (en) | 1993-01-08 |
| JPH085285Y2 JPH085285Y2 (en) | 1996-02-14 |
Family
ID=13033915
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5667291U Expired - Fee Related JPH085285Y2 (en) | 1991-06-25 | 1991-06-25 | Low-pressure cabin of steam turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH085285Y2 (en) |
-
1991
- 1991-06-25 JP JP5667291U patent/JPH085285Y2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH085285Y2 (en) | 1996-02-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2246530B1 (en) | Connection structure of exhaust chamber, support structure of turbine, and gas turbine | |
| JP4033715B2 (en) | Exhaust frame, gas turbine engine, and manufacturing method thereof | |
| US8469661B2 (en) | Fabricated gas turbine vane ring | |
| US20110262277A1 (en) | Gas turbine composite workpiece to be used in gas turbine engine | |
| US20170114669A1 (en) | Structural case for aircraft gas turbine engine | |
| US20060000077A1 (en) | A method of manufacturing a stator component | |
| JP2017040262A (en) | CMC nozzle with split end wall for gas turbine engine | |
| JP4787261B2 (en) | Gas turbine casing enclosing gas turbine components | |
| JP2017122445A5 (en) | ||
| JP2008064092A (en) | Expansion joint for gas turbine | |
| JP4347977B2 (en) | Casing for steam turbine or gas turbine | |
| CN108204255B (en) | Turbine system, exhaust frame for turbine system and strut thereof | |
| JPH05902U (en) | Low-pressure cabin of steam turbine | |
| JP2879795B2 (en) | Axial flow turbine for elastic fluid | |
| CA2935760A1 (en) | Gas turbine engine combustor and method of forming same | |
| JP4396258B2 (en) | Double pipe type exhaust pipe and its manufacturing method | |
| US11118479B2 (en) | Stress mitigating arrangement for working fluid dam in turbine system | |
| JPH051603Y2 (en) | ||
| CN114502827A (en) | Structural and/or acoustic panel comprising a U-shaped sealing flange oriented towards the inside of the panel, and method for manufacturing such a panel | |
| JPH0512536B2 (en) | ||
| JP2007009820A (en) | Turbine casing | |
| JP7513559B2 (en) | Silencer | |
| JPS608404A (en) | Low pressure casing of steam turbine | |
| KR102947394B1 (en) | Exhaust structure for gas turbine device | |
| JP2020153249A (en) | Casing and turbine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 19960806 |
|
| LAPS | Cancellation because of no payment of annual fees |