JPS61169628A - Compressor driver - Google Patents
Compressor driverInfo
- Publication number
- JPS61169628A JPS61169628A JP869685A JP869685A JPS61169628A JP S61169628 A JPS61169628 A JP S61169628A JP 869685 A JP869685 A JP 869685A JP 869685 A JP869685 A JP 869685A JP S61169628 A JPS61169628 A JP S61169628A
- Authority
- JP
- Japan
- Prior art keywords
- compressor
- frequency
- induction motor
- frequency converter
- rotation
- 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
Landscapes
- Control Of Ac Motors In General (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
- Control Of Positive-Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
この発明は、ガスタービン等に加圧ガスを供給するコン
プレッサを駆動するために用いられる、コンプレッサの
駆動装置に関するものでおる。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a compressor drive device used to drive a compressor that supplies pressurized gas to a gas turbine or the like.
一般に、コンプレッサ駆動ガスタービンは、コンプレッ
サによって加圧空気を燃焼器に供給し、燃焼器から発生
する高温ガスによって駆動され、その出力は出力タービ
ンを介して被駆動機に伝えられる。これらの動力系を起
動するには、電動機あるいは蒸気タービン等の起動機に
よって、コンプレッサを起動し、コンプレッサが適切な
圧力を生ずるに相当の回転数になったら、燃焼器に燃料
の供給と点火を行なって起動が完了すると、起動機は空
転状態におかれるか、着脱継手による解列が行なわれる
。その後はコンプレッサ駆動ガ・スタービンの動力の一
部を利用してコンプレッサを駆動し、継続して燃焼器か
ら高温ガスを得ている。Generally, a compressor-driven gas turbine supplies pressurized air to a combustor by a compressor, is driven by hot gases generated from the combustor, and its output is transmitted to a driven machine via a power turbine. To start these power systems, a starter, such as an electric motor or steam turbine, starts the compressor, and once the compressor has reached a sufficient rotational speed to produce the appropriate pressure, it supplies fuel to the combustor and ignites it. When starting is completed, the starter is placed in an idling state or is disconnected from the line using a detachable joint. After that, part of the power from the compressor drive gas and turbine is used to drive the compressor, and high-temperature gas is continuously obtained from the combustor.
しかしながら、コンプレッサ駆動ガスタービンの回転数
は出力タービンと連係しておシ、被駆動機の目的に従っ
た回転数を維持するための制御を行なわねばならないの
で、負荷の変化あるいは燃料の熱量の変化にともなう燃
量調整に対応する最適空気量制御のための回転5数制御
は行なえないという欠点があった。この欠点を除去する
ために、コンプレッサの静翼角調整、油気バイパスによ
る空気量制御が行なわれているが、構造が複雑なうえ、
制御幅が狭いため、最適空気量制御の効果は不十分であ
った。However, the rotational speed of the compressor-driven gas turbine must be controlled in conjunction with the output turbine to maintain the rotational speed according to the purpose of the driven machine, so changes in the load or the calorific value of the fuel must be controlled. There is a drawback in that it is not possible to control the number of revolutions for optimum air amount control corresponding to the fuel amount adjustment accompanying this. In order to eliminate this drawback, the air volume is controlled by adjusting the stator vane angle of the compressor and by oil bypass, but the structure is complicated and
Because the control width was narrow, the effect of optimal air amount control was insufficient.
このような問題を解決するためKこの発明は、連続定格
の誘導電動機と、この誘導電動機に任意の周波数の電源
を供給する周波数変換器とで駆動装置を構成したもので
ある。In order to solve these problems, the present invention provides a drive device that includes a continuous rated induction motor and a frequency converter that supplies power at an arbitrary frequency to the induction motor.
起動時は連続可変周波数変換器の周波数を上昇、させる
ことによって、コンプレッサの回転数を上昇させ、適切
な圧力に達した時に、燃焼器への燃料供給と点火を行な
い、以後は空燃比の最適化計装信号によって周波数制御
を行ない、コンプレッサの回転数制御を行なう。At startup, the frequency of the continuously variable frequency converter is increased to increase the rotation speed of the compressor, and when the appropriate pressure is reached, fuel is supplied to the combustor and ignited, and from then on, the air-fuel ratio is optimized. Frequency control is performed using the chemical instrumentation signal, and the rotation speed of the compressor is controlled.
第1図はこの発明の一実施例を示すブロック図である。 FIG. 1 is a block diagram showing one embodiment of the present invention.
同図において、1は連続定格の誘導電動機、2はコンプ
レッサ、3は燃焼器、4はコンプレッサ駆動ガスタービ
ン、5は被駆動機、6は出力周波数を0〜200ヘルツ
程度の範囲で任意制御することができる周波数変換器で
ある。In the figure, 1 is a continuous rated induction motor, 2 is a compressor, 3 is a combustor, 4 is a compressor-driving gas turbine, 5 is a driven machine, and 6 is an output frequency that is arbitrarily controlled in the range of about 0 to 200 Hz. It is a frequency converter that can be used.
このように構成された装置の動作は次の通シである。商
用電源の供給された周波数変換器6の出力周波数を徐々
に上昇させ、コンプレッサ2の回転数が適切な圧力を生
ずるに達した時点で燃焼器3への燃料供給と点火を行な
い自刃運転に入る、以後は誘導電導機1へ供給する周波
数を空燃比が最適となるように制御する。The operation of the device configured as described above is as follows. Gradually increases the output frequency of the frequency converter 6 to which commercial power is supplied, and when the rotation speed of the compressor 2 reaches an appropriate pressure, fuel is supplied and ignited to the combustor 3, and self-blade operation begins. Thereafter, the frequency supplied to the induction machine 1 is controlled so that the air-fuel ratio is optimized.
誘導電動機は周波数を高めることにより、例えば2極機
、電源周波数150ヘルツの場合、回転数は9000回
転/分となシ、電動機の体格寸法を縮少することが可能
となる。2極機を商用周波数で駆動した場合はこのよう
な回転数を得ることはできないが、この発明のように周
波数変換器6を介して商用電源を供給すれば、コンプレ
ッサ2の回転数はタービン駆動の場合と同等の値となる
。そして、この発明ではコンプレッサはタービンの回転
数とは無関係に回転数が決まるので、出力タービンとの
関連の制約なしに、自由に高効率設計が行なえるようK
なる。By increasing the frequency of the induction motor, for example, in the case of a two-pole machine with a power source frequency of 150 Hz, the rotation speed is 9000 revolutions per minute, and it is possible to reduce the physical size of the motor. If a two-pole machine is driven at a commercial frequency, it is not possible to obtain such a rotation speed, but if commercial power is supplied via the frequency converter 6 as in the present invention, the rotation speed of the compressor 2 can be adjusted to the turbine-driven speed. The value is the same as in the case of . In addition, in this invention, the rotation speed of the compressor is determined independently of the rotation speed of the turbine, so high efficiency design can be freely performed without restrictions related to the output turbine.
Become.
第2図は被駆動機5が発電機によって構成される場合で
アシ、この場合は発生電力を電力系統7に供給する他、
その発生電力の一部は周波数変換器6を介してコンプレ
ッサ駆動用として誘導電動機IKよって消費される。FIG. 2 shows a case where the driven machine 5 is constituted by a generator; in this case, in addition to supplying the generated power to the power system 7,
A part of the generated power is consumed by the induction motor IK via the frequency converter 6 for driving the compressor.
今後、ガスタービンのコンプレッサは単に燃焼器への燃
焼空気の供給機能に止どまらず、種々の可燃性ガスの吸
引機能などの要求も強まるが、この発明によればコンプ
レッサの容量、回転数も自由に選ぶことが可能でメジ、
そのような要求への対応も極めて容易である。なお、ガ
スタービンの負荷変動に対して燃焼器での燃料制御によ
る対応のみでなく、コンプレッサの回転数制御を連動さ
せれば、負荷変動に対するタービンの回転数変動特性を
改善することに効果があシ、特に被駆動機5が発電機の
場合、全負荷遮断による過速度の抑制のために、燃料制
御を行なうとともに、コンプレッサ回転数の抑制制御を
行なえば、極めて効果的である。In the future, gas turbine compressors will not only have the function of simply supplying combustion air to the combustor, but will also be required to have a suction function for various flammable gases. You can also choose freely.
It is also extremely easy to meet such requests. In addition to responding to gas turbine load fluctuations through fuel control in the combustor, it is effective to improve the turbine speed fluctuation characteristics in response to load fluctuations by linking compressor rotation speed control. In particular, when the driven machine 5 is a generator, it is extremely effective to perform fuel control and suppress the compressor rotation speed in order to suppress overspeed due to full load interruption.
以上説明したようにこの発明は、コンプレッサを誘導電
動機で駆動し、その誘導電動機を出力周波数が任意に設
定できる周波数変換器で駆動するようにしたので、構成
が簡単にな)、信頼性が向上するとともに、周波数変換
器の出力周波数を変えることKよってコンプレッサの回
転数を自由に設定することができるので、大幅な負荷変
動にも効率よく追従することができるという効果を有す
る。As explained above, in this invention, the compressor is driven by an induction motor, and the induction motor is driven by a frequency converter whose output frequency can be set arbitrarily, which simplifies the configuration and improves reliability. At the same time, since the rotation speed of the compressor can be freely set by changing the output frequency of the frequency converter, it is possible to efficiently follow large load fluctuations.
第1図はこの発明の一実施例を示すブロック図、第2図
は他の実施例を示すブロック図である。
1・・・・誘導電動機、2・・・・コンプレッサ、3・
Φ・・燃焼器、4・・・・タービン、5・・−・被駆動
機、6・・・・周波数変換器。FIG. 1 is a block diagram showing one embodiment of the invention, and FIG. 2 is a block diagram showing another embodiment. 1...Induction motor, 2...Compressor, 3...
Φ...Combustor, 4...Turbine, 5...Driven machine, 6...Frequency converter.
Claims (1)
ンプレッサの駆動装置において、コンプレッサを駆動す
る誘導電動機と、入力周波数を任意の周波数に変換して
出力する周波数変換器とを備えたことを特徴とするコン
プレッサの駆動装置。A compressor drive device that drives a compressor that supplies pressurized air to a combustor, characterized by comprising an induction motor that drives the compressor and a frequency converter that converts an input frequency to an arbitrary frequency and outputs the frequency. Compressor drive device.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP869685A JPS61169628A (en) | 1985-01-21 | 1985-01-21 | Compressor driver |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP869685A JPS61169628A (en) | 1985-01-21 | 1985-01-21 | Compressor driver |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS61169628A true JPS61169628A (en) | 1986-07-31 |
JPH0312211B2 JPH0312211B2 (en) | 1991-02-19 |
Family
ID=11700082
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP869685A Granted JPS61169628A (en) | 1985-01-21 | 1985-01-21 | Compressor driver |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS61169628A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0898362A1 (en) * | 1997-08-18 | 1999-02-24 | Asea Brown Boveri AG | Method for supplying a gas turbine plant |
WO2014020772A1 (en) * | 2012-08-03 | 2014-02-06 | 株式会社日立製作所 | Twin-shaft gas turbine power generation system, and control device and control method for gas turbine system |
WO2016098156A1 (en) * | 2014-12-15 | 2016-06-23 | 株式会社日立製作所 | Gas turbine power generation system |
JP2018526565A (en) * | 2015-08-06 | 2018-09-13 | ツリー アソシエイツ エルティーディー. | engine |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55114847A (en) * | 1979-02-26 | 1980-09-04 | Toshiba Corp | Gas turbine |
-
1985
- 1985-01-21 JP JP869685A patent/JPS61169628A/en active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55114847A (en) * | 1979-02-26 | 1980-09-04 | Toshiba Corp | Gas turbine |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0898362A1 (en) * | 1997-08-18 | 1999-02-24 | Asea Brown Boveri AG | Method for supplying a gas turbine plant |
WO2014020772A1 (en) * | 2012-08-03 | 2014-02-06 | 株式会社日立製作所 | Twin-shaft gas turbine power generation system, and control device and control method for gas turbine system |
CN104487678A (en) * | 2012-08-03 | 2015-04-01 | 株式会社日立制作所 | Twin-shaft gas turbine power generation system, and control device and control method for gas turbine system |
GB2519014A (en) * | 2012-08-03 | 2015-04-08 | Hitachi Ltd | Twin-shaft gas turbine power generation system, and control device and control method for gas turbine system |
JPWO2014020772A1 (en) * | 2012-08-03 | 2016-07-11 | 株式会社日立製作所 | Two-shaft gas turbine power generation system, control device and control method for gas turbine system |
US9520757B2 (en) | 2012-08-03 | 2016-12-13 | Hitachi, Ltd. | Dual-shaft gas turbine power generation system, and control device and control method for gas turbine system |
CN104487678B (en) * | 2012-08-03 | 2017-06-06 | 株式会社日立制作所 | Twin-shaft turbine electricity generation system, the control device of gas turbine engine systems and control method |
US10193383B2 (en) | 2012-08-03 | 2019-01-29 | Hitachi, Ltd. | Dual-shaft gas turbine power generation system, and control device and control method for gas turbine system |
WO2016098156A1 (en) * | 2014-12-15 | 2016-06-23 | 株式会社日立製作所 | Gas turbine power generation system |
JPWO2016098156A1 (en) * | 2014-12-15 | 2017-09-21 | 株式会社日立製作所 | Gas turbine power generation system |
JP2018526565A (en) * | 2015-08-06 | 2018-09-13 | ツリー アソシエイツ エルティーディー. | engine |
Also Published As
Publication number | Publication date |
---|---|
JPH0312211B2 (en) | 1991-02-19 |
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