JPS62359B2 - - Google Patents
Info
- Publication number
- JPS62359B2 JPS62359B2 JP6313577A JP6313577A JPS62359B2 JP S62359 B2 JPS62359 B2 JP S62359B2 JP 6313577 A JP6313577 A JP 6313577A JP 6313577 A JP6313577 A JP 6313577A JP S62359 B2 JPS62359 B2 JP S62359B2
- Authority
- JP
- Japan
- Prior art keywords
- compressor
- control
- valve
- surge
- blow
- 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.)
- Expired
Links
- 238000000034 method Methods 0.000 claims description 10
- 230000005540 biological transmission Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000746 purification Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 238000007664 blowing Methods 0.000 description 1
- 239000013642 negative control Substances 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0284—Conjoint control of two or more different functions
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Description
【発明の詳細な説明】
この発明は大型ターボ圧縮機の流量及び圧力を
連続的に測定し、サージ現象を避けるために、前
記測定値と基準値とを比較してその制御差値に基
いて、吹出弁を調節する送風圧縮機、特に溶鉱炉
用送風圧縮機の制御方法に関する。DETAILED DESCRIPTION OF THE INVENTION This invention continuously measures the flow rate and pressure of a large turbo compressor, compares the measured value with a reference value, and controls based on the difference value in order to avoid surge phenomena. , relates to a method of controlling a blow compressor for adjusting a blow-off valve, particularly a blow compressor for a blast furnace.
このような制御方法が適用される溶鉱炉の送風
系の1例が第1図に示されており、同図におい
て、送風圧縮機1はこれに結合された送風系内に
所定の圧力で所定の流量の給気を生ずる。圧縮機
1のすぐ下流に吹出弁2が配置され、この吹出弁
2は必要な場合に給気の一部分を大気に排出する
ように作用する。この吹出弁2の次に不還弁3お
よび制御弁4が設けられ、その下流には再生器5
が配設され、図面ではこのような再生器を1つだ
け示してある。次いで給気はリング主管6に流入
し、これから吹上げられて羽口結合部から溶鉱炉
7に入る。次いで溶鉱炉中で発生したのどガスが
のど8から浄化システム9に入り、そこからのど
ガスシステム10に流入する。現今では溶鉱炉7
の背圧はこの浄化システムを経由して極めて頻繁
に制御されている。のどガス系内に存在する圧力
は他の場所においても同様に制御され、したがつ
てこののどガス系は一定圧力の巨大な蓄積器を形
成している。 An example of a blowing system of a blast furnace to which such a control method is applied is shown in FIG. Produces a flow rate of air supply. Immediately downstream of the compressor 1, a blow-off valve 2 is arranged, which serves to discharge a portion of the charge air to the atmosphere if necessary. A non-return valve 3 and a control valve 4 are provided next to the blow-off valve 2, and a regenerator 5 is downstream thereof.
is provided, and only one such regenerator is shown in the drawing. The supply air then flows into the ring main pipe 6, from which it is blown up and enters the blast furnace 7 through the tuyere connection. The throat gas generated in the blast furnace then enters a purification system 9 through the throat 8 and from there into a throat gas system 10 . Currently, blast furnace 7
back pressure is very often controlled via this purification system. The pressure present in the throat gas system is controlled elsewhere as well, so that this throat gas system forms a huge reservoir of constant pressure.
第2図には溶鉱炉7の低抗の特性曲線と組合わ
された圧縮機1の特性曲線群を示し、この図にお
いて流量QAは横軸に、また吐出圧力PEは縦軸に
示されており、Aは吹出弁2の全開時の抵抗曲
線、B,B′はガイドベーン特性が0%及び100%
の際における圧縮機1の動作点曲線、Cは吹出曲
線、Dは安全曲線、Eはサージ限度曲線をそれぞ
れ示し、吹出曲線Cより右下方の領域は許容領
域、左上方は非許容領域となつている。正常運転
時にはこの圧縮機1は吹出弁2を全開して始動さ
れ、それにより動作点BP1が得られる。吹出弁
2が閉じられると、圧縮機1の動作点は、ガイド
ベーン特性が0%の曲線Bに沿つて、溶鉱炉7の
抵抗特性曲線HO1と交わる動作点BP2まで移動
する。そしてガイドベーンが開かれると、圧縮機
1の動作点はガイドベーン特性が100%の曲線
B′が抵抗曲線HO1と交わるBP3にまで移動す
る。 FIG. 2 shows a group of characteristic curves of the compressor 1 combined with the characteristic curve of the low resistance of the blast furnace 7, in which the flow rate QA is shown on the horizontal axis and the discharge pressure PE is shown on the vertical axis. A is the resistance curve when the blow-off valve 2 is fully open, B and B' are the guide vane characteristics of 0% and 100%.
The operating point curve of the compressor 1 at the time of ing. During normal operation, the compressor 1 is started with the blow-off valve 2 fully open, thereby obtaining the operating point BP1. When the blow-off valve 2 is closed, the operating point of the compressor 1 moves along the curve B where the guide vane characteristic is 0% to the operating point BP2 where it intersects the resistance characteristic curve HO1 of the blast furnace 7. When the guide vanes are opened, the operating point of compressor 1 is the curve where the guide vane characteristics are 100%.
B' moves to BP3 where it intersects the resistance curve HO1.
溶鉱炉7の低抗が特性曲線HO1から特性曲線
HO2に示すような高い抵抗値となると、圧縮機
1の動作点は特性曲線B′に沿つて吹出曲線Cと交
る動作点BP4に移動する。そしてここで吹出弁
2が開き始めて、たとえ圧縮機1が圧力を維持し
ても、溶鉱炉7に不要な給気は大気に排出される
こととなる。 The low resistance of blast furnace 7 changes from the characteristic curve HO1 to the characteristic curve.
When a high resistance value as shown by HO2 is reached, the operating point of the compressor 1 moves along the characteristic curve B' to an operating point BP4 that intersects the blowout curve C. Then, the blow-off valve 2 starts to open, and even if the compressor 1 maintains the pressure, the unnecessary supply air to the blast furnace 7 will be discharged to the atmosphere.
このように吹出曲線Cに到達したとき吹出弁2
の確実な開口を行うために、従来から第3図に示
すような電気回路を用いた制御器による制御方法
が行われている。 In this way, when the blowout curve C is reached, the blowoff valve 2
In order to ensure reliable opening, a control method using a controller using an electric circuit as shown in FIG. 3 has conventionally been used.
この制御器において、圧縮機1の流量QA及び
圧力PEの測定値は電気信号に変換され、即ち圧
力PEの測定値は関数発生器30によつて変換さ
れる。信号の差値が通例の方式で比較器32で形
成され、この差値が制御差値としてサージ限度制
御器34に加えられ、次いでこの制御器34は吹
出弁2を制御するための信号yを提供する。なお
11は電磁制御弁を示す。 In this controller, the measured values of the flow rate QA and the pressure PE of the compressor 1 are converted into electrical signals, ie the measured values of the pressure PE are converted by a function generator 30. A signal difference value is formed in the customary manner in a comparator 32 and this difference value is applied as a control difference value to a surge limit controller 34, which then outputs a signal y for controlling the blow-off valve 2. provide. Note that 11 indicates an electromagnetic control valve.
ところでこのような制御方法においては、制御
が手動でなされ、また大圧力変動を伴う状態で
は、圧縮機のサージ現象が発生するという欠点が
ある。たまに起るサージ現象は従来許し得るもの
と考えられてきたが、最近では避けなければなら
ないものと考えられている。 However, such a control method has the disadvantage that the control is performed manually and that a surge phenomenon occurs in the compressor under conditions involving large pressure fluctuations. Although the occasional surge phenomenon was previously considered to be something that could be tolerated, it has recently been considered something that must be avoided.
最近の研究では約25MW程度の性能をもつ大型
送風圧縮機の場合には、サージ現象が起る都度、
羽根に弾性限界を超える大きさの応力がかかつ
て、羽根の損傷が起ることが判明した。現在の炉
用送風圧縮機は効率の観点から、各圧縮機が単一
の溶鉱炉に供給するように設計され、特に混乱又
は破壊時に大圧給変動が起り、従つてサージ現象
の発生を防ぐことは困難である。 Recent research shows that in the case of large blower compressors with a performance of about 25 MW, whenever a surge phenomenon occurs,
It has been found that damage to the blades occurs when the blades are subjected to a stress that exceeds their elastic limit. Current blast compressors for furnaces are designed from an efficiency point of view so that each compressor feeds a single blast furnace, especially in the event of a disruption or breakage, which can result in large pressure supply fluctuations and thus prevent the occurrence of surge phenomena. It is difficult.
従つてこの発明の目的は、前記従来の制御方法
のもたらす欠点を排除し、ターボ圧縮機、特に大
型ターボ圧縮機におけるサージ現象を防止するこ
とのできる制御方法を提供するにある。 SUMMARY OF THE INVENTION Accordingly, an object of the present invention is to provide a control method capable of eliminating the drawbacks of the conventional control methods and preventing surge phenomena in turbo compressors, particularly large turbo compressors.
この発明によれば、上記の目的は圧力及び流量
の実測量と基準値との制御差値を非線形的に増大
する方法により、制御差値が負となつて圧縮機の
動作点が吹出曲線を越えて非許容領域内に移動す
れば、制御差値が増加するような方法で達成され
ることとなる。 According to the present invention, the above object is achieved by nonlinearly increasing the control difference value between the measured quantities of pressure and flow rate and the reference value, so that the control difference value becomes negative and the operating point of the compressor changes to the blowout curve. Moving beyond this and into the unacceptable region will be achieved in such a way that the control difference value increases.
第4図ないし第6図にこの発明の実施例が示さ
れ、以下これを参照しつつこの発明を詳細に述べ
る。なお第3図のものと同一部分については同一
の符号を付した。 Embodiments of the present invention are shown in FIGS. 4 to 6, and the present invention will be described in detail below with reference to these. Note that the same parts as those in FIG. 3 are given the same reference numerals.
第4図から判るように非線形伝達要素40がサ
ージ限度制御器34の入力側に接続される。比較
器32において形成される制御差値XDが許容領
域内にある場合は正を、また非許容領域内にある
場合は負をあらわすようになつている。すなわち
サージ限度制御器34に対する制御差値が正の場
合は、圧縮機1の動作点が吹出曲線Cの右下側に
おける許容領域にあり、制御差値が場合には吹出
曲線の左上側の非許容領域にあることを意味す
る。 As can be seen in FIG. 4, a nonlinear transfer element 40 is connected to the input side of the surge limit controller 34. When the control difference value XD formed by the comparator 32 is within the permissible region, it represents a positive value, and when within the non-permissible region, it represents a negative value. That is, when the control difference value for the surge limit controller 34 is positive, the operating point of the compressor 1 is in the allowable region on the lower right side of the blowout curve C; This means that it is within the permissible range.
非線形伝達要素40の利得特性は、少くとも2
つの傾斜増加型の直線で形成される。非許容領域
内に入るために特性曲線が中断し、この場合ノイ
ズ信号によつて起る小さい負制御差値は、あらか
じめ定めた大きさのものでない限り消去される。
大きくて非許容領域における制御差値は、例えば
入力対出力の比が1:5となるような高い利得が
えられるようにし、これによつてサージ限度制御
器34の干渉を増大させ、この結果吹出弁2を急
速に開かせて圧縮機1の動作点を許容領域に戻す
こととなる。 The gain characteristic of the nonlinear transfer element 40 is at least 2
It is formed by two straight lines with increasing slope. The characteristic curve is interrupted due to entering the non-permissible region, in which case small negative control difference values caused by noise signals are eliminated unless they are of a predetermined magnitude.
A control difference value in the large, non-acceptable region allows a high gain to be obtained, for example an input to output ratio of 1:5, thereby increasing the interference of the surge limit controller 34, resulting in The blow-off valve 2 is rapidly opened to return the operating point of the compressor 1 to the permissible range.
さらに比較器32に形成された制御差値XD
は、限度制御器42で第2図の安全曲線Dにおけ
る限度値と比較され、図から判るようにこの安全
曲線Dはサージ限度曲線Eと吹出曲線Cとの中間
にあつて吹出曲線Cとの距離の方が大きく、この
距離は不適当な制御動作によつてもたらされる制
御システムの故障の場合にのみ到達するような距
離となつている。もし制御差値XDが前記限度値
を超えると、吹出弁2は全開される。 Furthermore, the control difference value XD formed in the comparator 32
is compared with the limit value at the safety curve D in FIG. The distance is greater and is such that it is reached only in the event of a failure of the control system caused by improper control action. If the control difference value XD exceeds the limit value, the blow-off valve 2 is fully opened.
始動段階において、一方では正常な運転状態が
出来る限り速かに達せられ、他方では通常のサー
ジ限度制御器34の使用によつて引起され、サー
ジ作用を生じさせるおそれのある高度の行過ぎ状
態が、可能な限り除去されなければならない。 During the start-up phase, on the one hand, normal operating conditions are reached as quickly as possible, and on the other hand, high overshoot conditions, which can be triggered by the use of the normal surge limit controller 34 and which can give rise to surge effects, are ensured. , shall be removed as much as possible.
このための実施例が第5図に示されており、制
御可能な積分器50を含む始動回路が用いられ、
この回路は次の様に作動する。 An embodiment for this is shown in FIG. 5, in which a starting circuit including a controllable integrator 50 is used,
This circuit operates as follows.
圧縮機1の始動中に吹出弁2は制御によつて開
かれている。この制御指令が続いている間、積分
器50にはある大きさの可変因子が設定され、こ
の大きさは制御器の開口指令の発生を確実に行う
ことができる大きさである。この積分器50の出
力電圧は許容制御差値に対して反対の極性をもつ
ている。このようにして非許容制御差値がサージ
限度制御器34にシミユレートされ、この制御器
はこれに対応して応答する。圧縮機1の始動が完
了すると吹出弁2はじよじよに閉じられ、これは
圧縮機1の動作点が吹出線Cに達するまで実施さ
れる。積分器50はクリアされ、それに含まれた
内容は調節可能な速度比率で放出され、その出力
信号は最初の値からゼロになる。このようにして
真の制御差値は、サージ機度制御器34内で効果
を発揮するから、この制御器は圧縮機1の動作点
が吹出線Cに達する程度まで吹出弁2をじよじよ
に閉じる。積分器50のクリア速度を適切に選択
することによつて、始動階段において圧縮機1の
動作点は吹出線Cを越えないことが保証される。 During startup of the compressor 1, the blow-off valve 2 is opened under control. While this control command continues, a variable factor of a certain magnitude is set in the integrator 50, and this magnitude is large enough to ensure generation of the opening command of the controller. The output voltage of this integrator 50 has a polarity opposite to the allowable control difference value. In this way, unacceptable control difference values are simulated to the surge limit controller 34, which responds accordingly. When the start-up of the compressor 1 is completed, the blow-off valve 2 is gradually closed until the operating point of the compressor 1 reaches the blow-off line C. The integrator 50 is cleared and its contained contents are discharged at an adjustable rate, and its output signal goes from its initial value to zero. In this way, the true control difference value takes effect in the surge intensity controller 34, which gradually controls the blowoff valve 2 to such an extent that the operating point of the compressor 1 reaches the blowout line C. close. By appropriately selecting the clearing speed of the integrator 50, it is ensured that the operating point of the compressor 1 does not exceed the blowout line C during the start-up step.
前記第3図示の制御方法において、サージ限度
制御器34は連続電気信号及び出力信号の形の手
動制御指令を発することが知られ、この出力信号
は吹出弁2を調節する調整駆動装置を制御するの
に役立つ。この場合吹出弁2はさらに手動で開口
されてもよいが、サージ限度制御器34によつて
指令された以上には閉じられないことが保証され
る。しかしこのシステムは開から閉への手動制御
信号が極端に急速に変化すると、第5図に示す始
動回路を伴わない場合に生ずるのと類似した行過
ぎ状態を生じる欠点をもつている。 In the control method shown in said third figure, it is known that the surge limit controller 34 issues a manual control command in the form of a continuous electrical signal and an output signal, which output signal controls the regulating drive regulating the blow-off valve 2. useful for. In this case the blow-off valve 2 may also be opened manually, but it is ensured that it is not closed further than commanded by the surge limit controller 34. However, this system has the disadvantage that extremely rapid changes in the open-to-close manual control signal can result in an overshoot condition similar to that which would occur without the starting circuit shown in FIG.
この現象を避けるために、手動制御信号は、第
6図に示す比較器60においてサージ限度制御器
34の出力信号と比較される。この差値及び比較
器32における制御差値は最少値選択のために回
路62に送られる。この回路62の出力信号は制
御差値の代りにサージ限度制御器34に加えられ
る。このようにして、吹出弁2はさらに進んだ程
度まで手動で開くことができるが、圧縮機1の動
作点が吹出曲線Cを越えるようにまでは閉じられ
ないことを保証する。しかしサージ限度制御器3
4の出力信号は常に吹出弁2の実際の位置に対応
するから上記の行過ぎ状態が起ることはない。 To avoid this phenomenon, the manual control signal is compared with the output signal of the surge limit controller 34 in a comparator 60 shown in FIG. This difference value and the control difference value in comparator 32 are sent to circuit 62 for minimum value selection. The output signal of this circuit 62 is applied to the surge limit controller 34 in place of the control difference value. In this way, the blowoff valve 2 can be manually opened to a further extent, but it is ensured that it is not closed to such an extent that the operating point of the compressor 1 exceeds the blowoff curve C. However, surge limit controller 3
Since the output signal of 4 always corresponds to the actual position of the blow-off valve 2, the above-mentioned overshooting condition never occurs.
第1図はこの発明の方法を適用した溶鉱炉用給
気システムのブロツク線図、第2図は同上の溶鉱
炉特性と圧縮機特性との典型的組合せグラフ、第
3図は従来の制御方法に用いられる典型的な電気
回路図、第4,5,6図はこの発明の第1,2,
3実施例の回路図である。
1……圧縮機、2……吹出器、7……溶鉱炉、
30……関数発生器、32……比較器、34……
サージ限度制御器、40……非線形伝達要素、4
2……限度制御器、50……積分器、60……比
較器。
Fig. 1 is a block diagram of a blast furnace supply air system to which the method of the present invention is applied, Fig. 2 is a graph of a typical combination of the above blast furnace characteristics and compressor characteristics, and Fig. 3 is a diagram showing a typical combination of blast furnace characteristics and compressor characteristics used in the conventional control method. The typical electric circuit diagrams shown in Figs. 4, 5, and 6 are the 1st, 2nd,
FIG. 3 is a circuit diagram of a third embodiment. 1...Compressor, 2...Blower, 7...Blast furnace,
30...Function generator, 32...Comparator, 34...
Surge limit controller, 40...Nonlinear transfer element, 4
2... limit controller, 50... integrator, 60... comparator.
Claims (1)
続的に測定し、サージ現象の発生を防ぐために、
前記測定値と基準値との制御差値に基きサージ限
度制御によつて吹出弁を調節するターボ圧縮機の
制御方法において、前記制御差値を非線形伝達要
素により非線形的に増大し、もし制御差値が負と
なつて圧縮機の動作点が吹出線を越えてサージ限
度曲線の方に移行すれば、利得が増大してサージ
限度制御器に伝達されるようになつていることを
特徴とするターボ圧縮機の制御方法。1 Continuously measure the flow rate and pressure of the air supplied by the turbo compressor, and in order to prevent the occurrence of surge phenomena,
In a turbo compressor control method in which a blow-off valve is adjusted by surge limit control based on a control difference value between the measured value and a reference value, the control difference value is nonlinearly increased by a nonlinear transmission element; If the value becomes negative and the operating point of the compressor moves beyond the blowout line toward the surge limit curve, the gain increases and is transmitted to the surge limit controller. How to control a turbo compressor.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19762623899 DE2623899C3 (en) | 1976-05-28 | 1976-05-28 | Method for operating turbo compressors near the surge limit |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS52145803A JPS52145803A (en) | 1977-12-05 |
| JPS62359B2 true JPS62359B2 (en) | 1987-01-07 |
Family
ID=5979196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6313577A Granted JPS52145803A (en) | 1976-05-28 | 1977-05-28 | Controlling method of turboocompressors |
Country Status (7)
| Country | Link |
|---|---|
| JP (1) | JPS52145803A (en) |
| AT (1) | AT350704B (en) |
| CH (1) | CH621855A5 (en) |
| DE (1) | DE2623899C3 (en) |
| FR (1) | FR2352970A1 (en) |
| GB (1) | GB1578936A (en) |
| IT (1) | IT1086338B (en) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2828124C2 (en) * | 1978-06-27 | 1981-11-19 | M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen | Procedure to prevent pumping of turbo compressors |
| DE2852717C2 (en) * | 1978-12-06 | 1982-02-11 | M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen | Process for limiting the final pressure for turbo compressors by means of blow-off control |
| DE3105376C2 (en) * | 1981-02-14 | 1984-08-23 | M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen | Procedure for operating turbo compressors |
| DE3540087A1 (en) * | 1985-11-12 | 1987-05-14 | Gutehoffnungshuette Man | METHOD FOR REGULATING TURBO COMPRESSORS |
| DE3540285A1 (en) * | 1985-11-13 | 1987-05-14 | Gutehoffnungshuette Man | METHOD AND DEVICE FOR REGULATING TURBO COMPRESSORS |
| JPS63235698A (en) * | 1987-03-25 | 1988-09-30 | Sumitomo Metal Ind Ltd | Control method for blower |
| DE3805119A1 (en) * | 1988-02-18 | 1989-08-31 | Gutehoffnungshuette Man | METHOD AND DEVICE FOR REGULATING TURBO COMPRESSORS |
| DE3809070A1 (en) * | 1988-03-18 | 1989-10-26 | Gutehoffnungshuette Man | METHOD FOR THE SAFE OPERATION OF TURBO COMPRESSORS |
| DE3809881A1 (en) * | 1988-03-24 | 1989-10-12 | Gutehoffnungshuette Man | CONTROL METHOD FOR AVOIDING THE PUMPING OF A TURBO COMPRESSOR |
| DE3810717A1 (en) * | 1988-03-30 | 1989-10-19 | Gutehoffnungshuette Man | METHOD FOR PREVENTING THE PUMPING OF A TURBO COMPRESSOR BY MEANS OF A BLOW-OFF CONTROL |
| DE3811230A1 (en) * | 1988-04-02 | 1989-10-26 | Gutehoffnungshuette Man | METHOD FOR PROTECTING A TURBO COMPRESSOR FROM PUMPS BY BLOW-OFF WITH A BLOW-OFF VALVE, AND DEVICE FOR CARRYING OUT THE METHOD |
| US5012637A (en) * | 1989-04-13 | 1991-05-07 | General Electric Company | Method and apparatus for detecting stalls |
| DE19528253C2 (en) * | 1995-08-01 | 1997-10-16 | Gutehoffnungshuette Man | Method and device for avoiding controller instabilities in surge limit controls when operating turbomachines with controllers with high proportional gain |
| CN119532221B (en) * | 2024-11-28 | 2025-09-19 | 百事德机械(江苏)有限公司 | Calculation method for closing emptying valve of centrifugal fan according to slope |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1428023A1 (en) * | 1962-04-03 | 1969-04-10 | Bbc Brown Boveri & Cie | Process and device to prevent pumping in axial compressors |
| DE2155311A1 (en) * | 1971-11-06 | 1973-05-10 | Daimler Benz Ag | DEVICE FOR CONTROLLING A TURBO COMPRESSOR |
| GB1413791A (en) * | 1971-11-17 | 1975-11-12 | Rolls Royce | Control systems |
-
1976
- 1976-05-28 DE DE19762623899 patent/DE2623899C3/en not_active Expired
-
1977
- 1977-05-05 CH CH565077A patent/CH621855A5/en not_active IP Right Cessation
- 1977-05-17 AT AT354277A patent/AT350704B/en not_active IP Right Cessation
- 1977-05-26 FR FR7716099A patent/FR2352970A1/en active Granted
- 1977-05-27 IT IT2405677A patent/IT1086338B/en active
- 1977-05-27 GB GB2260077A patent/GB1578936A/en not_active Expired
- 1977-05-28 JP JP6313577A patent/JPS52145803A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| ATA354277A (en) | 1978-11-15 |
| DE2623899C3 (en) | 1989-06-08 |
| FR2352970A1 (en) | 1977-12-23 |
| IT1086338B (en) | 1985-05-28 |
| DE2623899A1 (en) | 1977-12-15 |
| DE2623899B2 (en) | 1979-11-29 |
| CH621855A5 (en) | 1981-02-27 |
| GB1578936A (en) | 1980-11-12 |
| JPS52145803A (en) | 1977-12-05 |
| AT350704B (en) | 1979-06-11 |
| FR2352970B1 (en) | 1983-10-07 |
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