JPS5979005A - Axial-flow turbine having widthwise-flow type speed governing step attached with variable nozzle - Google Patents
Axial-flow turbine having widthwise-flow type speed governing step attached with variable nozzleInfo
- Publication number
- JPS5979005A JPS5979005A JP18821782A JP18821782A JPS5979005A JP S5979005 A JPS5979005 A JP S5979005A JP 18821782 A JP18821782 A JP 18821782A JP 18821782 A JP18821782 A JP 18821782A JP S5979005 A JPS5979005 A JP S5979005A
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- nozzle
- variable nozzle
- widthwise
- flow
- 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.)
- Pending
Links
- 238000000034 method Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 238000010248 power generation Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 241000473391 Archosargus rhomboidalis Species 0.000 description 1
- 238000001467 acupuncture Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000002918 waste heat Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
【発明の詳細な説明】
本発明は、軸流タービンに関し、可変ノズル付輻流式調
速段を有する軸流タービンを提供するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an axial flow turbine, and provides an axial flow turbine having a radial flow governor stage with a variable nozzle.
発電用及び動力用に数多く使用されている蒸気タービン
、ガスタービン、ガスエキスパンダー類においては、一
般に、作動条件の圧力比及び流量が大きいことがら、多
段の軸流式を採用している。2. Description of the Related Art Steam turbines, gas turbines, and gas expanders that are widely used for power generation and motive power generally adopt a multistage axial flow type because the operating conditions include large pressure ratios and large flow rates.
また、これら軸流タービンの負荷制御にはノズル締切に
よる蒸気量制御を採用しており、このノズル締切には第
1図に示すようなプラグ式の弁を使用し、かつ弁の流量
特性?向上させるために一般に多弁方式となっている。In addition, steam flow control by nozzle shutoff is adopted for load control of these axial flow turbines, and a plug-type valve as shown in Fig. 1 is used for this nozzle shutoff. In order to improve this, a multi-verbal system is generally used.
なお、第1図において、1はプラグ式の制御弁、2はノ
ズル、3はロータ、4はノズル室、5はノズル室仕切板
、6は揚程棒、7は蒸気入口乞示す。In FIG. 1, 1 is a plug-type control valve, 2 is a nozzle, 3 is a rotor, 4 is a nozzle chamber, 5 is a nozzle chamber partition plate, 6 is a lift rod, and 7 is a steam inlet.
しかして、このような多弁式のノズル締切制御方式にお
いては、弁の圧損は無視できないものであり、弁の圧損
は、タービン第一段ノズル入口圧力を低下させ、タービ
ンでの有効熱落差が減少することを意味する。これは、
弁の開き始め、特に弁数の少ない場合に大きな影響を及
ぼし、第2図及び第3図はそれぞれ弁数4弁における弁
開度と弁圧損との関係及び弁開度と有効熱落差との関係
を示している。However, in such a multi-valve nozzle shutoff control system, the valve pressure loss cannot be ignored, and the valve pressure loss decreases the turbine first stage nozzle inlet pressure, reducing the effective heat drop in the turbine. It means to do. this is,
This has a big effect when the valve starts to open, especially when the number of valves is small. Figures 2 and 3 show the relationship between the valve opening and the valve pressure loss and the relationship between the valve opening and the effective heat drop when the number of valves is four, respectively. It shows a relationship.
一方、近年は、省エネルギーへの動向が高まり、数多く
の排熱回収発電設備が計画・運転されているが、このよ
うな発電設備は熱源側(排熱量)を制御できないために
、タービンの制御は負荷制御でなく入口圧制御を採用し
ている。タービンの負荷は排熱量まかせとなり、操業度
が不振な時期とか、またはプロセスによっては毎日排熱
量が変化したすして、低負荷運転になることが多く、弁
圧損の大きいポイントで運転している。このような排熱
回収タービンは、比較的出力が小さいことから、コスト
減も考慮し、高速タービンであることが多く、したがっ
て高速であることから、比較的段数も少ないため、特に
弁圧損の影響乞受けやすく、低負荷での性能向上が重要
なポイントとなっている。On the other hand, in recent years, there has been a growing trend toward energy conservation, and a large number of waste heat recovery power generation facilities are being planned and operated.However, since the heat source side (exhaust heat amount) of such power generation facilities cannot be controlled, turbine control is difficult. Adopts inlet pressure control instead of load control. The load on the turbine is determined by the amount of exhaust heat, and the turbine is often operated at a low load during periods of low operating efficiency or when the amount of exhaust heat changes daily depending on the process, and the turbine is operated at a point where valve pressure loss is large. Since such exhaust heat recovery turbines have a relatively small output, they are often high-speed turbines in consideration of cost reduction, and therefore, due to their high speed, the number of stages is relatively small, so they are particularly sensitive to the effects of valve pressure drop. The important point is to improve performance at low loads and to make it easy to accept.
本発明は、このような事情に鑑みなされたもので、ター
ビン入口における弁圧損を減少し、多段軸流タービンの
低負荷運転・タービン入口圧制御運転時の効率向上、エ
ネルギー節減を図ることを目的とする。The present invention was made in view of the above circumstances, and aims to improve efficiency and save energy during low-load operation and turbine inlet pressure control operation of a multistage axial flow turbine by reducing valve pressure loss at the turbine inlet. shall be.
本発明は、多段軸流タービンの入ロ流量制鍼賀ノズル方
式を採用し、かつこの可変ノズル?装備しやすくするた
めに調速段の形式として輻流式(ラジアル・・(ン・フ
ロ一式)を採用したこと乞特徴とする。The present invention adopts a multi-stage axial flow turbine inlet flow rate control acupuncture nozzle system, and also uses this variable nozzle. In order to make it easier to install, a special feature is the adoption of a radial type (radial type) as the type of governor stage.
以下図面を参照して、本発明の一実施例について詳述す
る。An embodiment of the present invention will be described in detail below with reference to the drawings.
第4図は本発明による軸流タービンの基本構造の一例を
示し、ロータ11は蒸気入口側のインペラー(輻流段)
12とブレード14が植設さ]tた数段のディスク(軸
流段)13とから成る。FIG. 4 shows an example of the basic structure of an axial flow turbine according to the present invention, in which the rotor 11 is an impeller (stream stage) on the steam inlet side.
12 and several stages of disks (axial stages) 13 in which blades 14 are installed.
しかして、蒸気は、主止め弁を通った後、渦巻状のノズ
ル室15へ入って来る。その後、蒸気は、可変ノズル1
6を通り、タービン軸に対して直角な方向よりインペラ
ー12に流入し、そのインペラー出口ではタービン軸方
向へと流れ、ノズル17、ブレード14を通過し、排気
口18へと至る。Thus, the steam enters the spiral nozzle chamber 15 after passing through the main stop valve. After that, the steam is transferred to the variable nozzle 1
6 and flows into the impeller 12 from a direction perpendicular to the turbine axis, and at the impeller outlet flows in the direction of the turbine axis, passes through the nozzle 17 and the blade 14, and reaches the exhaust port 18.
なお、インペラー12及び可変ノズル16以外は、従来
の軸流タービンとほぼ同一の構造となっている。Note that the structure other than the impeller 12 and variable nozzle 16 is almost the same as that of a conventional axial flow turbine.
第5図は、可変ノズルの基本機構を示す。この機構は、
従来から、輻流タービン(第4図のインペラー12)に
数多く用いられているものであり、可変ノズル16は連
結棒21を介して回転リング22に取り付けられている
。この回転リング22が左右に回転することにより、可
変ノズル16は連結棒取り付は点を中心として左右に回
転し、ノズル16の開度を調整し、ノズル前の蒸気圧力
を一定に保ちながら、ノズル開度に応じた蒸気量を流入
させる。回転リング22の回転は、サーボ油筒23の動
きが連動レバー24.揚程棒25を介して伝達されるこ
とにより行なわれる。FIG. 5 shows the basic mechanism of the variable nozzle. This mechanism is
Conventionally, the variable nozzle 16 has been used in many radial flow turbines (impeller 12 in FIG. 4), and the variable nozzle 16 is attached to a rotating ring 22 via a connecting rod 21. By rotating this rotating ring 22 left and right, the variable nozzle 16 rotates left and right around the point at which the connecting rod is attached, adjusting the opening degree of the nozzle 16 and keeping the steam pressure in front of the nozzle constant. The amount of steam flows in according to the nozzle opening degree. The rotation of the rotating ring 22 is caused by the movement of the servo oil cylinder 23 via the interlocking lever 24. This is done by being transmitted via the lift rod 25.
第6図は、従来の弁制御方式による固定ノズルと、本発
明による可変ノズルとの部分負荷特性の一例を比較して
示す。この例は、単弁を用いた固定ノズルとの比較であ
るため、性能の差は欠き(,50%の流量で、出力は半
分程の差がでている。FIG. 6 shows a comparative example of the partial load characteristics of a fixed nozzle using a conventional valve control method and a variable nozzle according to the present invention. This example is a comparison with a fixed nozzle using a single valve, so there is no difference in performance (at 50% flow rate, the output is about half the difference).
上述したように、本発明は、軸流段乞有するロータのタ
ービン入口側に輻流段を設け、この輻流段に入口流量を
制御する可変ノズルを設けたものであるから、次のよう
な効果が得られる。As described above, the present invention provides a radial flow stage on the turbine inlet side of a rotor having an axial flow stage, and this radial flow stage is provided with a variable nozzle for controlling the inlet flow rate. Effects can be obtained.
(1)弁圧損が無いため、部分負荷におげろ性能が向上
する。(1) Since there is no valve pressure loss, partial load performance is improved.
(21蒸気流人出径が異なる輻流段をタービン入口に採
用しているので、流入径が大きい分、多くの熱落差を消
化するため、全段軸流式に比べると、段数を少なくする
ことができる。(21) Since a radial flow stage with different steam flow diameters is used at the turbine inlet, the number of stages is reduced compared to a full stage axial flow type in order to absorb a large amount of heat drop due to the large inlet diameter. be able to.
(3) 背圧タービンのように、比較的熱落差、圧力
比が小さい蒸気条件では、数段の輻流タービンも可能で
あったが、復水タービンのように、熱落差・圧力比が太
き(なると、輻流タービンも多段となり、構造が複雑と
なって採用しにくかった。(3) In steam conditions where the heat drop and pressure ratio are relatively small, such as in a back-pressure turbine, a multiple-stage radial flow turbine was possible; When this happened, the radial flow turbine also became multi-stage, making the structure complex and difficult to adopt.
しかし、本発明のように1、輻流式と軸流式とを合体す
ることにより、両者の長所を引き出し、部分負荷特性を
良好にして高熱落差のタービンを作ることが可能となる
。However, by combining the radial flow type and the axial flow type as in the present invention, it is possible to bring out the advantages of both, improve partial load characteristics, and create a turbine with a high thermal drop.
以上述べたように、本発明によれば、産業上きわめて有
益な可変ノズル付輻流式調速段を有する軸流タービンが
提供される。As described above, according to the present invention, there is provided an axial flow turbine having a variable nozzle-equipped radial flow regulating stage which is extremely useful industrially.
【図面の簡単な説明】
第1図は従来の軸流タービンにおける多弁式ノズル締切
制御方式を示す図、第2図はこのノズル締切制御方式に
おける弁開度と弁圧損との関係を示す図、第3図は同様
に弁開度と有効熱落差との関係を示す図、第4図は本発
明上よる軸流タービンの基本構造の一例を示す図、第5
図はその可変ノズル基本機構を示す、第4図のA矢視図
、第6図は本発明による可変ノズルと従来例による固定
ノズルとの部分負荷特性を比較して示す図である。
11・・ロータ、12・・インペラー、13・拳ディス
ク、14・Φブレード、16・・可変ノズ第1 図
第2図 第39
弁開度 青閏度
第4図
第5図
鯛[Brief Description of the Drawings] Fig. 1 is a diagram showing a multi-valve nozzle shut-off control system in a conventional axial flow turbine, and Fig. 2 is a diagram showing the relationship between valve opening degree and valve pressure loss in this nozzle shut-off control system. 3 is a diagram similarly showing the relationship between the valve opening degree and the effective heat drop, FIG. 4 is a diagram showing an example of the basic structure of the axial flow turbine according to the present invention, and FIG.
The figure shows the basic mechanism of the variable nozzle, taken in the direction of arrow A in FIG. 4, and FIG. 6 is a diagram showing a comparison of the partial load characteristics of the variable nozzle according to the present invention and a conventional fixed nozzle. 11. Rotor, 12. Impeller, 13. Fist disk, 14. Φ blade, 16. Variable nozzle No. 1 Fig. 2 Fig. 39 Valve opening degree Blue leap Fig. 4 Fig. 5 Sea bream
Claims (1)
、この輻流段に入口流量を制御する可変ノズルを設けた
ことを特徴とする軸流タービン。An axial flow turbine characterized in that a radial flow stage is provided on the turbine inlet side of a rotor having an axial flow stage, and a variable nozzle for controlling the inlet flow rate is provided in the radial flow stage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18821782A JPS5979005A (en) | 1982-10-28 | 1982-10-28 | Axial-flow turbine having widthwise-flow type speed governing step attached with variable nozzle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18821782A JPS5979005A (en) | 1982-10-28 | 1982-10-28 | Axial-flow turbine having widthwise-flow type speed governing step attached with variable nozzle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5979005A true JPS5979005A (en) | 1984-05-08 |
Family
ID=16219812
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP18821782A Pending JPS5979005A (en) | 1982-10-28 | 1982-10-28 | Axial-flow turbine having widthwise-flow type speed governing step attached with variable nozzle |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5979005A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02161103A (en) * | 1988-12-13 | 1990-06-21 | Shin Murata | Turbine |
-
1982
- 1982-10-28 JP JP18821782A patent/JPS5979005A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02161103A (en) * | 1988-12-13 | 1990-06-21 | Shin Murata | Turbine |
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