JPS61135940A - Exhaust gas damper - Google Patents

Exhaust gas damper

Info

Publication number
JPS61135940A
JPS61135940A JP25563284A JP25563284A JPS61135940A JP S61135940 A JPS61135940 A JP S61135940A JP 25563284 A JP25563284 A JP 25563284A JP 25563284 A JP25563284 A JP 25563284A JP S61135940 A JPS61135940 A JP S61135940A
Authority
JP
Japan
Prior art keywords
exhaust gas
damper
gas
gas turbine
exhaust
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
Application number
JP25563284A
Other languages
Japanese (ja)
Inventor
Katsutoshi Higuma
樋熊 勝敏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP25563284A priority Critical patent/JPS61135940A/en
Publication of JPS61135940A publication Critical patent/JPS61135940A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30Exhaust heads, chambers, or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

PURPOSE:To prevent a reversal flow and an abnormal pressure increase when exhaust gas ducts are merged by providing a damper to the exhaust gas ducts that lead the burnt gas discharged from a gas turbine system to a smoke stack. CONSTITUTION:A compound cycle plant has a gas turbine system 10, a waste heat recovering boiler 20, a steam turbine system 40 and denitrification system 31. In such an arrangement, an exhaust gas damper 27 is disposed in an exhaust gas duct 25 from the waste heat recovering boiler 20 to a smoke stack 24. As an abnormal pressure increase in the exhaust gas duct can take place by the compressed air due to the racing gas turbine if a damper at the waste heat recovering boiler outlet is rapidly closed while the gas turbine is being tripped, the abnormal pressure increase is prevented by the rate of speed of the damper closure at the waste heat recovering boiler outlet and the action of the afore-said exhaust gas damper 27. Further, the burnt gas from the working gas turbine is prevented from reversing itself into the stopped gas turbine system.

Description

【発明の詳細な説明】 〔発明の利用分野〕 本発明は、ガスタービン装置から排出される燃焼ガスを
排熱回収ボイラより煙突まで導く排ガスダクトにおける
排ガスダンパーに係り、特に、逆流防止と異状昇圧を防
止できる排ガスダクトにおける排ガスダンパーに関する
[Detailed Description of the Invention] [Field of Application of the Invention] The present invention relates to an exhaust gas damper in an exhaust gas duct that guides combustion gas discharged from a gas turbine device from an exhaust heat recovery boiler to a chimney, and particularly relates to an exhaust gas damper for preventing backflow and for preventing abnormal pressure rise. This invention relates to an exhaust gas damper in an exhaust gas duct that can prevent

〔発明の背景〕[Background of the invention]

第5図及び第6図は従来のガスタービン装置10とその
燃焼ガスを熱源として蒸気を発生する排熱回収ボイラ2
0と、この発生蒸気を駆動蒸気とする蒸気タービン装置
40とを備えた場合の複合サイクルプラントを示してい
る。
Figures 5 and 6 show a conventional gas turbine device 10 and an exhaust heat recovery boiler 2 that generates steam using its combustion gas as a heat source.
This shows a combined cycle plant including a steam turbine 40 and a steam turbine device 40 that uses the generated steam as driving steam.

ここで排ガスダクト25は煙突24人口部で合流され煙
突に導かれる。又、二本の排ガスダクトが合流され一本
のダクトになっているため、一台が運転し、一台が停止
している場合には、運転中の排ガスが停止中の排ガスダ
クト25を通υ、排熱回収ボイラ20及びガスタービン
装置10へ逆流するという問題がある。
Here, the exhaust gas ducts 25 are merged at the chimney 24 and guided to the chimney. In addition, since two exhaust gas ducts are merged into one duct, when one unit is operating and the other is stopped, the exhaust gas from the operating unit passes through the stopped exhaust gas duct 25. υ, there is a problem of backflow to the exhaust heat recovery boiler 20 and the gas turbine device 10.

〔発明の目的〕[Purpose of the invention]

本発明の目的はガスタービン二台各々の排ガスダクトを
一本に合流させた場合、運転中の燃焼ガスの逆流と、ガ
スタービン停止時、空転による圧縮空気による異状昇圧
を防止できる排ガスダンパーを提供することにある。
An object of the present invention is to provide an exhaust gas damper that can prevent backflow of combustion gas during operation and abnormal pressure rise due to compressed air due to idle rotation when the gas turbine is stopped, when the exhaust gas ducts of two gas turbines are merged into one. It's about doing.

〔発明の概要〕[Summary of the invention]

本発明の特徴は、ガスタービン装置から排出される燃焼
ガスを排熱回収ボイラより煙突まで導く排ガスダクト中
の排ガスダンパーにおいて、運転中の燃焼ガスが停止中
のガスタービン装置に逆流するのを防止し、ガスタービ
ントリップ時のガスタービン空転による圧縮空気による
異状昇圧を防止できる構造としたことにある。
A feature of the present invention is that the exhaust gas damper in the exhaust gas duct that guides the combustion gas discharged from the gas turbine device from the exhaust heat recovery boiler to the chimney prevents the combustion gas during operation from flowing back into the stopped gas turbine device. However, it has a structure that can prevent abnormal pressure rise due to compressed air due to gas turbine idling during a gas turbine trip.

〔発明の実施例〕[Embodiments of the invention]

本発明を適用した排ガスダクトにおける排ガスダンパー
を備えた複合サイクルプラントの実施例を説明する。
An embodiment of a combined cycle plant equipped with an exhaust gas damper in an exhaust gas duct to which the present invention is applied will be described.

第1図において、複合サイクルプラントは、ガスタービ
ン装置10と、そのガスタービン装置から排出される燃
焼ガスを熱源として蒸気を発生する排熱回収ボイラ20
と、その排熱回収ボイラで発生した蒸気を駆動蒸気とす
る蒸気タービン装置40とガスタービン装置から排出さ
れる燃焼ガスのN Ox成分を除去する脱硝装置31と
を備えている。そして、ガスタービン装置10は導入空
気4を加圧する圧縮機11と、加圧空気を燃料系統5か
ら供給された燃料と共に燃焼する燃焼器14と、燃焼に
より生じた燃焼ガスにより駆動されるタービン12と、
負荷をとる発電機13を備えている。また、排熱回収ボ
イラ20はガスタービン装置から導かれる燃焼ガス流の
上流から下流に沿って過熱器21、蒸発器22、節炭器
23及び煙突24をもっていて、過熱器21で生じた蒸
気を蒸気配管2を通じて蒸気タービン装置40に導き、
置40からは給水配管1を通じて節炭器23に導かれる
。更に、この排熱回収ボイラ装置20の蒸発器22と過
熱器21との間には脱硝装置30が設置される。本実施
例では第2図において、排熱回収ボイラ装置20より煙
突24までの排ガスダクト25に組込まれた排ガスダン
パー27を設置することにより、ガスタービントリップ
時、排熱回収ボイラ出口ダンパーを急閉すると、ガスタ
ービンの空転による圧縮空気により排ガスダクトが異状
昇圧となるので、排熱回収ボイラ出口ダンパーの閉まる
速度と、本発明の排ガスダンパー(スイング式ダンパー
)を使用することにより異状昇圧を防止でき、又、排ガ
スダンパー27を設置することにより、一台運転、一台
停止している場合に、運転中の燃焼ガスが停止中のガス
タービン装置(含排熱回収ボイラ)への逆流を防止でき
る。
In FIG. 1, the combined cycle plant includes a gas turbine device 10 and an exhaust heat recovery boiler 20 that generates steam using combustion gas discharged from the gas turbine device as a heat source.
, a steam turbine device 40 that uses steam generated in the exhaust heat recovery boiler as driving steam, and a denitrification device 31 that removes NOx components from combustion gas discharged from the gas turbine device. The gas turbine device 10 includes a compressor 11 that pressurizes the introduced air 4, a combustor 14 that burns the pressurized air together with fuel supplied from the fuel system 5, and a turbine 12 that is driven by the combustion gas generated by combustion. and,
It is equipped with a generator 13 that takes the load. Further, the exhaust heat recovery boiler 20 has a superheater 21, an evaporator 22, a economizer 23, and a chimney 24 along the upstream to downstream of the combustion gas flow led from the gas turbine device, and the steam generated in the superheater 21 is guided to the steam turbine device 40 through the steam piping 2;
From the station 40, the water is led to the energy saver 23 through the water supply pipe 1. Further, a denitration device 30 is installed between the evaporator 22 and the superheater 21 of the exhaust heat recovery boiler device 20. In this embodiment, as shown in FIG. 2, by installing an exhaust gas damper 27 built into the exhaust gas duct 25 from the exhaust heat recovery boiler device 20 to the chimney 24, the exhaust heat recovery boiler outlet damper is quickly closed when the gas turbine trips. Then, the pressure in the exhaust gas duct will rise abnormally due to the compressed air generated by the idle rotation of the gas turbine, so this abnormal pressure rise can be prevented by adjusting the closing speed of the exhaust heat recovery boiler outlet damper and using the exhaust gas damper (swing type damper) of the present invention. In addition, by installing the exhaust gas damper 27, when one unit is in operation and one unit is stopped, it is possible to prevent the combustion gas in operation from flowing back to the gas turbine device (exhaust heat recovery boiler) that is stopped. .

次に、本発明の実施例を第1図、第2図、第3図、及び
第4図を用いて説明する。第1図は排ガスダクトの異状
昇圧防止及び逆流防止を備えた複合サイクルプラントを
示す。
Next, embodiments of the present invention will be described using FIGS. 1, 2, 3, and 4. FIG. 1 shows a combined cycle plant equipped with measures to prevent abnormal pressure rise and backflow in the exhaust gas duct.

第2図はガスタービン装置10から排出される燃焼ガス
を煙突まで導く排ガスダクトの経路を示す。この場合、
ガスタービンがトリップ時、排熱回収ボイラ出口ダンパ
ー26と排ガスダンパー27を設置することにより、排
ガスダクトの異状昇圧防止と、運転中の複数台からの逆
流を防止できる。
FIG. 2 shows a route of an exhaust gas duct that guides combustion gas discharged from the gas turbine device 10 to a chimney. in this case,
By installing the exhaust heat recovery boiler outlet damper 26 and the exhaust gas damper 27 when the gas turbine trips, it is possible to prevent an abnormal pressure increase in the exhaust gas duct and to prevent backflow from multiple units in operation.

第3図は排ガスダクト内に排熱回収ボイラ出口ダンパー
26及び異状昇圧防止、逆流防止のできる排ガスダンパ
ー27を設置した取付図を示す。
FIG. 3 shows an installation diagram in which an exhaust heat recovery boiler outlet damper 26 and an exhaust gas damper 27 capable of preventing abnormal pressure rise and backflow are installed in the exhaust gas duct.

第4図は排ガスダンパーの詳細図を示す。排ガスダクト
25は、断面積が大きいため、そこに使用するダンパー
27が異状昇圧防止を容易にし、逆流防止を容易にする
ため、構造を単純な逆止弁と同じ機能を持たせている。
Figure 4 shows a detailed diagram of the exhaust gas damper. Since the exhaust gas duct 25 has a large cross-sectional area, the damper 27 used therein is designed to have the same function as a simple check valve in order to easily prevent abnormal pressure rise and to easily prevent backflow.

又、断面積が大きいためダンパーの構造を容易にするの
と異状昇圧防止と逆流防止を容易にするため、ダクト内
の仕切シを細かくシ、ダンパーの取付を多段にすること
によりダンパーに対するガス量の当りが少なくダンパー
の開閉が容易となり、異状昇圧防止及び逆流防止ができ
る。即ち、第4図において、ダンパ一本体27aは回転
軸28に、サポート36と共に取付けられておシ、ダン
パ一本体27aの端部はストッパー35の存在により、
一方向にしか開動しないようになっている。そして、3
0はシール材で、29は仕切り、3はガス流れ、9は逆
流ガス流れを示す。
In addition, because the cross-sectional area is large, the structure of the damper is easy, and in order to prevent abnormal pressure rise and backflow, the partitions in the duct are finely divided, and the damper is installed in multiple stages to reduce the amount of gas relative to the damper. The damper can be opened and closed easily with less contact, and abnormal pressure rise and backflow can be prevented. That is, in FIG. 4, the damper main body 27a is attached to the rotating shaft 28 together with the support 36, and the end of the damper main body 27a is fixed by the presence of the stopper 35.
It is designed to only open in one direction. And 3
0 is a sealing material, 29 is a partition, 3 is a gas flow, and 9 is a counterflow gas flow.

なお、上記も含めて本発明では次の変形例が考えられる
In addition, the following modifications can be considered in the present invention including the above.

(1)ガスタービン装置複数合名7・に接続される排出
ガスダクトを合流し、−ヶの構造の排ガスダクトにおい
て、二台運転、一台停止又は、一台運転、二台停止して
いる場合には、運転中の排ガスが、停止中のダクト内に
逆流することが防止できる構造。
(1) When the exhaust gas ducts connected to multiple gas turbine devices are combined and the exhaust gas ducts have a - structure, two units are in operation and one unit is stopped, or one unit is in operation and two units are stopped. The structure prevents exhaust gas from flowing back into the duct when the system is not running.

(2)  ガスタービントリップ時、運転中のガスター
ビン側からの逆流を防止するため、排熱回収ボイラ出口
部のダンパーを閉とするが、閉状態において、ガスター
ビンが急に回転を止めることができないため、空転中に
空気を吸気し、煙突側に排気を続ける際に排気できる構
造。
(2) When the gas turbine trips, the damper at the exhaust heat recovery boiler outlet is closed to prevent backflow from the operating gas turbine, but in the closed state, the gas turbine may suddenly stop rotating. Since this is not possible, the structure allows air to be taken in during idling and exhausted when continuing to exhaust to the chimney side.

(3)ガスタービン装置複数合名々に接続される排出ガ
スダクトを合流し、−ヶの構造の排ガスダクトにおける
、二台運転、一台停止又は、一台運転、二台停止してい
る状態において、停止しているガスタービンを起動する
際に、運転中の排ガスが逆流することなく排ガスダンパ
ーを開にすることを可能とする構造。
(3) When the exhaust gas ducts connected to multiple gas turbine devices are combined and the exhaust gas duct has a structure of -, two units are operating and one unit is stopped, or one unit is operating and two units are stopped, A structure that allows the exhaust gas damper to be opened when starting a stopped gas turbine without causing the exhaust gas during operation to flow back.

(4)  ガスタービン装置複数合名々に接続される排
出ガスダクトを合流し、−ヶの構造の排ガスダクトにお
ける、異状昇圧防止、逆流防止ができるのと、停止中の
ガスタービンを、運転中の複数台のガスタービン排ガス
が逆流することなく起動することを可能とする構造。
(4) By merging the exhaust gas ducts connected to multiple gas turbine devices, it is possible to prevent abnormal pressure rise and reverse flow in the exhaust gas ducts with a structure of 1-2. A structure that allows the gas turbine to start up without backflow of exhaust gas.

〔発明の効果〕〔Effect of the invention〕

本発明によれば、ガスタービン装置から排出される、燃
焼ガスを煙突まで導く排ガスダクトにおいて、逆流防止
、異状昇圧防止ダンパーを設置することにより、ガスタ
ービンからの排ガスダクトを合流させることができる。
According to the present invention, the exhaust gas ducts from the gas turbine can be merged by installing a backflow prevention and abnormal pressure rise prevention damper in the exhaust gas duct that guides the combustion gas discharged from the gas turbine device to the chimney.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図、第2図、第3図及び第4図は本発明を適用した
排ガスダクトにおける逆流防止並びに異状昇圧防止ライ
ンの実施例で、第1図は逆流及び異状昇圧防止ラインを
備えた複合サイクルプラントの系統図、第2図、第3図
及び第4図は異状昇圧防止ライン及び逆流防止ダンパー
の説明図、第5図はガスタービンと蒸気タービンとを組
合せた従来の複合サイクルプラントの系統図、第6図は
その複合サイクルプラントの配置図である。 10・・・ガスタービン装置、20・・・排熱回収ボイ
ラ、25・・・排ガスダクト、26・・・ダンパー、2
7 、278・・・異状昇圧防止及び逆流防止ダンパー
Figures 1, 2, 3, and 4 show examples of backflow prevention and abnormal pressure rise prevention lines in exhaust gas ducts to which the present invention is applied, and Figure 1 shows a composite line equipped with backflow and abnormal pressure rise prevention lines. System diagram of the cycle plant; Figures 2, 3, and 4 are explanatory diagrams of the abnormal pressure rise prevention line and backflow prevention damper; Figure 5 is the system of a conventional combined cycle plant that combines a gas turbine and a steam turbine. Figure 6 is a layout diagram of the combined cycle plant. DESCRIPTION OF SYMBOLS 10... Gas turbine apparatus, 20... Exhaust heat recovery boiler, 25... Exhaust gas duct, 26... Damper, 2
7, 278... Abnormal pressure rise prevention and backflow prevention damper.

Claims (1)

【特許請求の範囲】 1、ガスタービン装置から排出される燃焼ガスを排熱回
収ボイラより煙突まで導く排ガスダクトにおいて、 前記ガスタービン装置のトリップ時に、空転による圧縮
空気が送られ、前記排熱回収ボイラの出口部に取付けた
ダンパーが閉になると、前記排ガスダクト並びに前記排
熱回収ボイラが異状昇圧となるのを防止する構造を設け
たことを特徴とする排ガスダンパー。
[Claims] 1. In an exhaust gas duct that guides combustion gas discharged from a gas turbine device from an exhaust heat recovery boiler to a chimney, compressed air is sent through idle rotation when the gas turbine device trips, and the exhaust heat recovery An exhaust gas damper comprising a structure that prevents the exhaust gas duct and the exhaust heat recovery boiler from becoming abnormally high in pressure when the damper attached to the outlet of the boiler is closed.
JP25563284A 1984-12-05 1984-12-05 Exhaust gas damper Pending JPS61135940A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25563284A JPS61135940A (en) 1984-12-05 1984-12-05 Exhaust gas damper

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25563284A JPS61135940A (en) 1984-12-05 1984-12-05 Exhaust gas damper

Publications (1)

Publication Number Publication Date
JPS61135940A true JPS61135940A (en) 1986-06-23

Family

ID=17281442

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25563284A Pending JPS61135940A (en) 1984-12-05 1984-12-05 Exhaust gas damper

Country Status (1)

Country Link
JP (1) JPS61135940A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5737911A (en) * 1995-01-20 1998-04-14 Hitachi, Ltd. Method of operating combined plant

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5737911A (en) * 1995-01-20 1998-04-14 Hitachi, Ltd. Method of operating combined plant

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