JPH04171202A - Steam turbine power generating plant - Google Patents
Steam turbine power generating plantInfo
- Publication number
- JPH04171202A JPH04171202A JP29884190A JP29884190A JPH04171202A JP H04171202 A JPH04171202 A JP H04171202A JP 29884190 A JP29884190 A JP 29884190A JP 29884190 A JP29884190 A JP 29884190A JP H04171202 A JPH04171202 A JP H04171202A
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- Prior art keywords
- turbine
- pressure turbine
- steam
- super
- ultra
- Prior art date
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Abstract
Description
【発明の詳細な説明】
[発明の目的]
(産業上の利用分野)
本発明は、蒸気タービン発電プラントに係り、特に、主
蒸気の温度、圧力を上昇させた超高温高圧タービンを用
いた発電プラントに関する。[Detailed Description of the Invention] [Object of the Invention] (Industrial Application Field) The present invention relates to a steam turbine power generation plant, and in particular to a power generation plant using an ultra-high temperature and high pressure turbine in which the temperature and pressure of main steam are increased. Regarding plants.
(従来の技術)
従来の蒸気タービン発電プラントにおける蒸気条件は、
主蒸気圧力246kg/cof g 、主蒸気温度53
8℃、再熱蒸気温度566℃が一般的であるが、この蒸
気圧力、温度をさらに上昇させることにより、発電プラ
ントの熱効率を大幅に改善することができる。この原理
を最も単純な蒸気タービン発電システムであるランキン
サイクルを用いて説明する。(Prior art) Steam conditions in a conventional steam turbine power plant are as follows:
Main steam pressure 246 kg/cof g, main steam temperature 53
8° C. and reheat steam temperature of 566° C. are common, but by further increasing the steam pressure and temperature, the thermal efficiency of the power plant can be significantly improved. This principle will be explained using the Rankine cycle, which is the simplest steam turbine power generation system.
第6図は、ランキンサイクルの温度・エントロピ線図(
T−3線図)を示す。同図において、従来のプラントは
、線A’ BEF’ A’で、温度、圧力を上昇させた
超高温高圧プラントが線ABEFAで示されている。従
来のプラント有効仕事は面積A’ BEF’で、熱損失
は面積BCDEで表される。従って、熱効率は、面積A
’ BEF’ /面積A’ CDF’ となる。超高温
高圧プラントでは、有効仕事が面積AA’ FF’だけ
増加するため、面積AA’ FF’ /面積ACDF分
だけプラント熱効率は上昇する。Figure 6 shows the temperature/entropy diagram of the Rankine cycle (
T-3 diagram) is shown. In the figure, a conventional plant is shown by the line A'BEF'A', and an ultra-high temperature and high pressure plant in which the temperature and pressure are increased is shown by the line ABEFA. Conventional plant effective work is expressed by area A'BEF' and heat loss is expressed by area BCDE. Therefore, the thermal efficiency is the area A
'BEF'/area A'CDF'. In an ultra-high-temperature, high-pressure plant, the effective work increases by the area AA'FF', so the plant thermal efficiency increases by the area AA'FF'/area ACDF.
例えば、主蒸気圧力316kg/aig 、蒸気温度5
66/ 566/ 566℃の二段再熱蒸気タービンの
場合(第8図に示す)、従来のプラントより約4%の熱
効率向上が期待できる。For example, main steam pressure 316 kg/aig, steam temperature 5
In the case of a two-stage reheat steam turbine at 66/566/566°C (as shown in Figure 8), an approximately 4% increase in thermal efficiency can be expected over conventional plants.
第7図は、主蒸気温度と熱効率向上値との関係を示す。FIG. 7 shows the relationship between main steam temperature and thermal efficiency improvement value.
同図において、aは従来のプラントを示し、b−dは超
高温高圧プラントを示している。In the figure, a indicates a conventional plant, and b-d indicate an ultra-high temperature and high pressure plant.
一方、タービンのロータ、ケーシングの材料についてみ
ると、b、cのレベルまでは現在使用されているフェラ
イト系の鋼材を高温用に改良した材料で対応できるが、
dのレベルまではオーステナイト系の材料が必要となる
。第8図は、b、cのレベルの代表的な蒸気タービンプ
ラントを示す。On the other hand, when looking at materials for turbine rotors and casings, levels B and C can be handled using materials improved from the currently used ferritic steel materials for high temperatures.
Up to the level d, austenitic materials are required. FIG. 8 shows a typical steam turbine plant at levels b and c.
同図において、ボイラ1で発生された超高温高圧の蒸気
は、超高圧タービン2aで仕事した後、再びボイラ1に
入り 566℃に加温され高圧タービン3に導かれる。In the figure, ultra-high temperature and high pressure steam generated in a boiler 1 works in an ultra-high pressure turbine 2a, then enters the boiler 1 again, is heated to 566° C., and is led to a high pressure turbine 3.
高圧タービン3を出た蒸気は、再度ボイラ1で加温され
た後、中圧タービン4゜低圧タービン5で仕事をし、復
水器7で凝縮して水になる。この水は、給水ポンプ8で
加圧され、ボイラ1へ導かれる、各タービンで蒸気が行
った仕事は、ロータの回転エネルギーとなり、発電機6
で電気エネルギーに変換される。The steam leaving the high-pressure turbine 3 is heated again in the boiler 1, then works in the intermediate-pressure turbine 4° and the low-pressure turbine 5, and is condensed in the condenser 7 to become water. This water is pressurized by the feed water pump 8 and guided to the boiler 1. The work done by the steam in each turbine becomes the rotational energy of the rotor, which generates the generator 6.
is converted into electrical energy.
ところが、第7図のdのレベル(主蒸気温度650℃)
になると、ロータ、ケーシング等の高温強度を確保する
ため、タービンの主要部の材料にクロム、ニッケル等を
多量に含入したオーステナイト系ステンレス鋼やニッケ
ル基の超合金を用いる必要が生じる。これらオーステナ
イト系の材料は、高価なため温度、圧力ともに高い超々
高圧部のみに用いるべく第9図に示すように超々高圧タ
ービン9aが別に設置されている。However, at level d in Figure 7 (main steam temperature 650°C)
In order to ensure the high-temperature strength of the rotor, casing, etc., it becomes necessary to use austenitic stainless steel or nickel-based superalloy containing large amounts of chromium, nickel, etc. as the material for the main parts of the turbine. Since these austenitic materials are expensive, an ultra-super-high pressure turbine 9a is separately installed as shown in FIG. 9 in order to use them only in the ultra-super-high pressure section where both temperature and pressure are high.
この場合、超々高圧タービン9aから低圧タービン5ま
でを一本の軸でつなぐのは、タービンの全長が長くなり
軸の熱伸びや建屋の大きさの関係で好ましくなく、低圧
タービン5を同図に示すように別軸とするのが一般的で
ある。In this case, it is not preferable to connect the ultra-super high pressure turbine 9a to the low pressure turbine 5 with a single shaft because the total length of the turbine becomes long and the thermal expansion of the shaft and the size of the building are undesirable. It is common to use separate axes as shown.
(発明が解決しようとする課題)
しかしながら、主蒸気温度650℃級の蒸気タービン発
電プラントで用いられるオーステナイト系材料は、フェ
ライト鋼に比べて高温強度は優れてはいるが、熱伸びが
大きく、熱伝導率が悪い等の特性を有している。(Problem to be solved by the invention) However, although austenitic materials used in steam turbine power plants with main steam temperatures of 650°C class have superior high-temperature strength compared to ferritic steel, they have large thermal elongation and It has characteristics such as poor conductivity.
通常、蒸気タービンの起動時には、回転部であるロータ
側か静止部であるケーシング側より先に温まり、停止時
には逆にロータ側かケーシング側より早く冷たくなる。Normally, when a steam turbine is started, the rotor side (the rotating part) or the casing side (the stationary part) warms up first, and when the steam turbine is stopped, the rotor side or the casing side cools down faster.
そこで、ロータ、ケーシング間の熱伸びの差が大きいと
、タービン各部の軸方向の間隙を大きくする必要が生じ
、蒸気漏洩によるタービン内部効率低下の要因となり、
回転部と静止部との接触による事故の発生する危険性が
ある。Therefore, if the difference in thermal elongation between the rotor and the casing is large, it becomes necessary to increase the axial clearance between each part of the turbine, which causes steam leakage and a reduction in turbine internal efficiency.
There is a risk of an accident occurring due to contact between the rotating part and the stationary part.
また、熱伝導率が悪いと、タービン起動時にロータ、ケ
ーシング等の蒸気通路部側のみ熱くなり、内外面での温
度差が大きくなるため、蒸気通路部側に大きな熱応力が
生じる。そのため、タービンのウオーミングに長時間を
要し、急速な起動・停止ができない。In addition, if the thermal conductivity is poor, only the steam passage side of the rotor, casing, etc. becomes hot when the turbine is started, and the temperature difference between the inner and outer surfaces increases, resulting in large thermal stress on the steam passage side. Therefore, it takes a long time to warm up the turbine, and rapid startup and shutdown are not possible.
さらに、超々高圧タービンを通過する蒸気は、圧力が高
いため、体積流量が小さく、従ってタービン翼長も短く
なり、タービン内部効率も低い値となる。Furthermore, since the pressure of the steam passing through the ultra-super high pressure turbine is high, the volumetric flow rate is small, so the turbine blade length is also short, and the turbine internal efficiency is also low.
そこで、本発明の目的は、オーステナイト系材料を用い
たタービン発電プラントにおいて、熱伸びや熱応力に起
因する不具合を除去し、高効率。Therefore, the purpose of the present invention is to eliminate defects caused by thermal elongation and thermal stress in turbine power generation plants using austenitic materials, and to achieve high efficiency.
高信頼性、高運用性を備えた蒸気タービン発電プラント
を提供することにある。Our objective is to provide a steam turbine power generation plant with high reliability and high operability.
[発明の構成コ
(課題を解決するための手段)
本発明は、ボイラから蒸気タービンに最初に供給される
主蒸気の温度、圧力が在来より高いレベルにあり、且つ
前記タービンが複数の蒸気タービンを直列に接続した蒸
気タービン群または複数の蒸気タービンを直列に接続し
た蒸気タービン群を並列して構成されている蒸気タービ
ン発電プラントにおいて、主蒸気が最初に導入される蒸
気タービンのみを別軸とし、単独に発電機を駆動するよ
うにしたものである。[Structure of the Invention (Means for Solving the Problems) The present invention provides a system in which the temperature and pressure of main steam initially supplied from a boiler to a steam turbine are at higher levels than conventional ones, and the turbine is connected to a plurality of steam turbines. In a steam turbine power plant that consists of a steam turbine group in which turbines are connected in series or a steam turbine group in which multiple steam turbines are connected in series in parallel, only the steam turbine into which main steam is first introduced is separated from the shaft. It is designed to independently drive a generator.
(作 用)
ボイラで発生した在来レベルより高い温度、圧力の主蒸
気が最初に導入される蒸気タービンは、他の蒸気タービ
ン群とは別軸で単独に発電機を駆動するようにしている
ので、運転条件を他の蒸気タービン群に影響されること
なく選択でき、使用材料に対応した構成が容易になり内
部効率の向上、遠心応力、熱伸びの影響、高温部におけ
る熱応力等を低減することができる。(Function) The steam turbine into which the main steam generated in the boiler at a temperature and pressure higher than conventional levels is first introduced is designed to drive a generator independently on a separate shaft from the other steam turbines. As a result, operating conditions can be selected without being influenced by other steam turbine groups, making it easy to configure configurations compatible with the materials used, improving internal efficiency, and reducing centrifugal stress, effects of thermal elongation, thermal stress in high-temperature parts, etc. can do.
(実施例)
以下、本発明の一実施例を図面を参照して説明する。第
1図は、本発明の一実施例を示す構成図である。(Example) Hereinafter, an example of the present invention will be described with reference to the drawings. FIG. 1 is a configuration diagram showing an embodiment of the present invention.
同図において、1はボイラ、2aは超高圧タービン、3
は高圧タービン、4は中圧タービン、5は低圧タービン
、9bは超々高圧タービンを示す。In the figure, 1 is a boiler, 2a is an ultra-high pressure turbine, and 3
4 is a high-pressure turbine, 4 is an intermediate-pressure turbine, 5 is a low-pressure turbine, and 9b is an extremely high-pressure turbine.
この超々高圧タービン9bには発電機6aを直結し、超
高圧タービン2aから低圧タービン5までは軸を連結し
、この軸に発電機6bを直結する。A generator 6a is directly connected to this ultra-super high pressure turbine 9b, a shaft is connected from the ultra high pressure turbine 2a to the low pressure turbine 5, and the generator 6b is directly connected to this shaft.
ボイラ1で発生した蒸気は、超々高圧タービン9bから
超高圧タービン2aへ流れ、ボイラ1で再熱され高圧タ
ービン3へ導かれる。高圧タービン3を出た蒸気は、ボ
イラ1で再熱され中圧タービン4へ導かれ、この中圧タ
ービン4から低圧タービン5へ流れ、復水器7で凝縮し
て水になる。Steam generated in the boiler 1 flows from the ultra-high pressure turbine 9b to the ultra-high pressure turbine 2a, is reheated by the boiler 1, and is guided to the high-pressure turbine 3. Steam leaving the high-pressure turbine 3 is reheated in the boiler 1 and guided to the intermediate-pressure turbine 4, flows from the intermediate-pressure turbine 4 to the low-pressure turbine 5, and is condensed in the condenser 7 to become water.
この水は、給水ポンプ8で加圧され、ボイラ1に給水さ
れる。This water is pressurized by a water supply pump 8 and supplied to the boiler 1.
しかして、超々高圧タービン9bは、高温強変に対応す
るためオーステナイト系材料を用い、超高圧タービン2
a等の約1/2の回転速度で運転し発生動力を発電機6
aで電気エネルギーに変換する。なお、超高圧タービン
2aや高圧タービン3は、圧力、温度が比較的低いので
フェライト鋼を用いる。Therefore, the ultra-high-pressure turbine 9b uses an austenitic material in order to cope with high temperature and severe changes, and the ultra-high-pressure turbine 2
Operates at approximately 1/2 rotation speed of a etc. and generates power to generator 6.
Convert it to electrical energy at a. Note that ferritic steel is used for the ultra-high pressure turbine 2a and the high pressure turbine 3 because their pressure and temperature are relatively low.
上記したように超々高圧タービン9bは、超高圧タービ
ン2a等の1/2の回転速度で運転されるが、タービン
内部における蒸気の軸流速度がタービンの回転速度に比
例するように翼を設計されているので、蒸気の軸流速度
を回転速度に合せて遅くするためには、翼長を約2倍に
する必要がある。As mentioned above, the ultra-high pressure turbine 9b is operated at half the rotation speed of the ultra-high pressure turbine 2a, etc., but the blades are designed so that the axial velocity of steam inside the turbine is proportional to the rotation speed of the turbine. Therefore, in order to reduce the axial velocity of steam to match the rotational speed, the blade length must be approximately doubled.
ここで、タービンの翼長と段落効率との関係を第2図に
示す。同図から明らかなように翼長5(1mm以下にな
ると段落効率が急激に低下する。これは、タービン蒸気
通路部の壁面近傍では、第3図に示すように二次流れl
Oが影響を及ぼす範囲lが翼長しにかかわらず略一定し
ているから、翼長しが短くなると相対的に二次流れ10
の範囲が大きくなるためと考えられる。Here, the relationship between the blade length of the turbine and the stage efficiency is shown in FIG. As is clear from the same figure, when the blade length becomes 5 (1 mm or less), the stage efficiency decreases rapidly.This is because the secondary flow l
Since the range l affected by O is approximately constant regardless of the blade length, the secondary flow 10 is relatively constant as the blade length becomes shorter.
This is thought to be because the range of
従って、超々高圧タービン9bの翼長が従来の20〜3
0mmから約2倍の約50mmへと長くなれば、タービ
ン内部効率も上昇する。Therefore, the blade length of the ultra-super high pressure turbine 9b is 20 to 3
If the length increases from 0 mm to about 50 mm, which is about twice the length, the turbine internal efficiency will also increase.
また、低い回転速度とした超々高圧タービン9bの遠心
力を、従来の回転速度のものと比較してみる。回転体の
遠心力は、mrω2で表されるが、翼の質量mは長さが
2倍になるので約2倍、回転半径r路間じ、回転角速度
ωが約1/2になる。In addition, the centrifugal force of the ultra-high pressure turbine 9b set at a low rotation speed will be compared with that of a conventional rotation speed. The centrifugal force of the rotating body is expressed as mrω2, and since the blade mass m is twice the length, it is approximately doubled, the rotation radius r, and the rotational angular velocity ω are approximately 1/2.
従って、回転速度を約1/2、翼長を約2倍とした超々
高圧タービン9bは、遠心力が従来の回転速度のものの
約1/2となるので、信頼性が大幅に向上する。Therefore, the ultra-high pressure turbine 9b with a rotational speed of approximately 1/2 and a blade length approximately twice as large has a centrifugal force approximately 1/2 that of a conventional rotational speed, and therefore reliability is greatly improved.
さらに、超々高圧タービン9bは、独立した軸(他のタ
ービンが連結されていない)で設置されているため、熱
伸びの影響が他の高圧タービン3、中圧タービン4、低
圧タービン5に及ぶことがなく、高圧タービン3、中圧
タービン4、低圧タービン5の軸方向間隙を小さくする
ことができ、信頼性の向上、漏洩損失の低減を図ること
ができる。Furthermore, since the ultra-super high pressure turbine 9b is installed with an independent shaft (to which other turbines are not connected), the effects of thermal expansion will not affect the other high pressure turbines 3, intermediate pressure turbines 4, and low pressure turbines 5. Therefore, the axial clearance between the high pressure turbine 3, intermediate pressure turbine 4, and low pressure turbine 5 can be reduced, and reliability can be improved and leakage loss can be reduced.
一方、第4図に示すように主蒸気止め弁11、蒸気加減
弁12と超々高圧タービン9bとの間に弁13を介して
補助蒸気管を接続すると共に、超々高圧タービン9bの
排気弁14の上流側にウオーミング弁15を介して復水
器(図示しない)へ接続する分岐管を接続して設け、タ
ービン停止中に主蒸気止め弁11と排気弁14を閉とす
れば、超々高圧タービン9bのみのウオーミング運転が
可能となる。On the other hand, as shown in FIG. 4, an auxiliary steam pipe is connected between the main steam stop valve 11, the steam control valve 12, and the ultra-super high pressure turbine 9b via a valve 13, and the exhaust valve 14 of the ultra high pressure turbine 9b is If a branch pipe is connected to the condenser (not shown) via the warming valve 15 on the upstream side, and the main steam stop valve 11 and the exhaust valve 14 are closed while the turbine is stopped, the ultra-super high pressure turbine 9b It is possible to perform a warming operation for only
これにより、高い熱応力が発生しゃすい超々高圧タービ
ン9bを常に高温に保持し、タービン起動による熱応力
を低減させることができ、急速な起動停止が可能となり
負荷の変動に対応しやすくなる。As a result, the ultra-high pressure turbine 9b, which tends to generate high thermal stress, can be maintained at a high temperature at all times, and the thermal stress caused by starting the turbine can be reduced, and rapid startup and shutdown becomes possible, making it easier to respond to load fluctuations.
なお、以上説明した実施例は、オーステナイト系材料を
用いる超々高圧タービン9bを別軸としたが、本発明は
これに限定されるものではなく、フェライト系材料を用
いる超高圧タービンを別軸としても同様の効果が得られ
る。In addition, in the embodiment described above, the ultra-high pressure turbine 9b using an austenitic material is set as a separate shaft, but the present invention is not limited to this, and the ultra-high pressure turbine using a ferrite-based material may be set as a separate shaft. A similar effect can be obtained.
第5図は、この発明にかかる蒸気タービン発電プラント
の他の実施例を示し、フェライト系材料を用いた超高圧
タービン2bが一軸で発電機6aを直結しており、高圧
タービン3、中圧タービン4、低圧タービン5が相互の
軸を連結すると共に発電機6bを直結している。FIG. 5 shows another embodiment of the steam turbine power generation plant according to the present invention, in which an ultra-high pressure turbine 2b made of ferrite material is directly connected to a generator 6a through one shaft, a high pressure turbine 3, an intermediate pressure turbine 4. The low pressure turbines 5 connect their shafts to each other and are directly connected to the generator 6b.
しかして、超高圧タービン2bは、回転速度を高圧ター
ビン3等の回転速度の172とし、翼長を約2倍とする
ことにより、上記した実施例と同様に信頼性の向上、漏
洩損失の低減、超高圧タービン2bの単独ウオーミング
による熱応力の低減を図ることができる。Therefore, the ultra-high-pressure turbine 2b has a rotational speed of 172 times the rotational speed of the high-pressure turbine 3, etc., and has a blade length approximately twice that of the high-pressure turbine 3, thereby improving reliability and reducing leakage loss in the same way as in the above-mentioned embodiments. , it is possible to reduce thermal stress due to independent warming of the ultra-high pressure turbine 2b.
この実施例は、従来の蒸気条件(246kg/c!Ir
g 。This example is based on conventional steam conditions (246 kg/c!Ir
g.
538/ 566℃)の上記タービン発電プラントに、
上記した主蒸気条件に対応できる過熱器および再熱器を
備えたボイラlas超高圧タービン2b。538/566°C) in the above turbine power plant,
A boiler LAS ultra-high pressure turbine 2b equipped with a superheater and a reheater that can meet the main steam conditions described above.
発電機6aを追加設置することにより、熱効率の高い超
高温高圧発電プラントに改造できる特徴を有する。なお
、1bは、従来のボイラを示す。By additionally installing a generator 6a, it has the feature that it can be remodeled into an ultra-high temperature and high pressure power generation plant with high thermal efficiency. Note that 1b indicates a conventional boiler.
[発明の効果コ
以上説明したように本発明によれば、在来レベルより高
い温度、圧力の主蒸気が最初に導入される蒸気タービン
を他の蒸気タービン群とは別軸で単独に発電機を駆動す
るようにしているので、蒸気タービンの内部効率の向上
を図ると共に、高温高圧部の遠心応力を低減し、さらに
熱伸びの影響や高温部における熱応力の低減を可能とし
た蒸気タービン発電プラントを提供することができる。[Effects of the Invention] As explained above, according to the present invention, the steam turbine into which main steam with a temperature and pressure higher than the conventional level is first introduced can be used as an independent generator with a separate shaft from the other steam turbines. This makes it possible to improve the internal efficiency of the steam turbine, reduce centrifugal stress in the high-temperature, high-pressure section, and further reduce the effects of thermal elongation and thermal stress in the high-temperature section. plant can be provided.
第1図は本発明の一実施例を示す構成図、第2図はター
ビンの翼長と段落効率の関係を示す線図、第3図はター
ビン内部の蒸気の流れを示す説明図、第4図は第1図の
一部を示す詳細図、第5図は本発明の他の実施例を示す
構成図、第6図はランキンサイクルの温度とエントロピ
の関係を示す線図第7図は主蒸気温度と熱効率の関係を
示す説明図、第8図は従来の超高温高圧タービン発電プ
ラントの構成図、第9図は第8図と異なる従来の超高温
高圧タービン発電プラントの構成図である。
1、la、lb・・・ボイラ
2a、2b・・・超高圧−タービン
3・・・高圧タービン
4・・・中圧タービン
5・・・低圧タービン
6a、6b・・・発電機
7・・・復水器
8・・・給水ポンプ
9a、9b・・・超々高圧タービン
(7317)代理人 弁理士 則近 憲佑ヌ長(mm)
第 21!1
v
箒 3 図
第 4 図
エントロヒ。
第6rg!J
土直丸ン11i(’C)
第 7 図
第 タ 穆σFig. 1 is a configuration diagram showing an embodiment of the present invention, Fig. 2 is a diagram showing the relationship between the turbine blade length and stage efficiency, Fig. 3 is an explanatory diagram showing the flow of steam inside the turbine, and Fig. 4 is a diagram showing the relationship between the blade length of the turbine and the stage efficiency. Figure 5 is a detailed diagram showing a part of Figure 1, Figure 5 is a configuration diagram showing another embodiment of the present invention, Figure 6 is a diagram showing the relationship between temperature and entropy of the Rankine cycle, and Figure 7 is the main An explanatory diagram showing the relationship between steam temperature and thermal efficiency, FIG. 8 is a configuration diagram of a conventional ultra high temperature high pressure turbine power generation plant, and FIG. 9 is a configuration diagram of a conventional ultra high temperature high pressure turbine power generation plant different from FIG. 8. 1, la, lb...Boiler 2a, 2b...Ultra high pressure turbine 3...High pressure turbine 4...Intermediate pressure turbine 5...Low pressure turbine 6a, 6b...Generator 7... Condenser 8...Water pumps 9a, 9b...Ultra-super high pressure turbine (7317) Representative Patent attorney Noriyuki Noriyuki Length (mm) No. 21!1 V Broom 3 Fig. 4 Entrohi. 6th rg! J Donaomarun 11i ('C) Fig. 7 Ta Mu σ
Claims (1)
度、圧力が在来より高いレベルにあり、且つ前記タービ
ンが複数の蒸気タービンを直列に接続した蒸気タービン
群または複数の蒸気タービンを直列に接続した蒸気ター
ビン群を並列して構成されている蒸気タービン発電プラ
ントにおいて、前記主蒸気が最初に導入される前記蒸気
タービンのみを別軸とし、単独に発電機を駆動するよう
にしたことを特徴とする蒸気タービン発電プラント。The temperature and pressure of the main steam initially supplied from the boiler to the steam turbine are at higher levels than conventional ones, and the turbine is a steam turbine group in which a plurality of steam turbines are connected in series, or a plurality of steam turbines are connected in series. In a steam turbine power generation plant comprising a group of steam turbines arranged in parallel, only the steam turbine into which the main steam is introduced first has a separate shaft and independently drives a generator. steam turbine power plant.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP29884190A JPH04171202A (en) | 1990-11-06 | 1990-11-06 | Steam turbine power generating plant |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP29884190A JPH04171202A (en) | 1990-11-06 | 1990-11-06 | Steam turbine power generating plant |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04171202A true JPH04171202A (en) | 1992-06-18 |
Family
ID=17864908
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP29884190A Pending JPH04171202A (en) | 1990-11-06 | 1990-11-06 | Steam turbine power generating plant |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH04171202A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08232609A (en) * | 1995-02-27 | 1996-09-10 | Yoshiharu Tachibana | Steam compression reheat regenerative cycle |
| AU2006200810B2 (en) * | 2005-04-28 | 2008-09-04 | Kabushiki Kaisha Toshiba | Steam turbine power plant |
| JP2009511810A (en) * | 2005-10-17 | 2009-03-19 | シーメンス アクチエンゲゼルシヤフト | Steam turbine power plant and method for adding steam turbine power plant |
| US8794913B2 (en) | 2008-08-11 | 2014-08-05 | Mitsubishi Heavy Industries, Ltd. | Steam turbine facility |
-
1990
- 1990-11-06 JP JP29884190A patent/JPH04171202A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08232609A (en) * | 1995-02-27 | 1996-09-10 | Yoshiharu Tachibana | Steam compression reheat regenerative cycle |
| AU2006200810B2 (en) * | 2005-04-28 | 2008-09-04 | Kabushiki Kaisha Toshiba | Steam turbine power plant |
| US7484926B2 (en) | 2005-04-28 | 2009-02-03 | Kabushiki Kaisha Toshiba | Steam turbine power plant |
| JP2009511810A (en) * | 2005-10-17 | 2009-03-19 | シーメンス アクチエンゲゼルシヤフト | Steam turbine power plant and method for adding steam turbine power plant |
| JP4833293B2 (en) * | 2005-10-17 | 2011-12-07 | シーメンス アクチエンゲゼルシヤフト | Steam turbine power plant and method for adding steam turbine power plant |
| US8794913B2 (en) | 2008-08-11 | 2014-08-05 | Mitsubishi Heavy Industries, Ltd. | Steam turbine facility |
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