JPH1113480A - Starting method for compressor in compressed air storage powder generating system - Google Patents

Starting method for compressor in compressed air storage powder generating system

Info

Publication number
JPH1113480A
JPH1113480A JP9170177A JP17017797A JPH1113480A JP H1113480 A JPH1113480 A JP H1113480A JP 9170177 A JP9170177 A JP 9170177A JP 17017797 A JP17017797 A JP 17017797A JP H1113480 A JPH1113480 A JP H1113480A
Authority
JP
Japan
Prior art keywords
compressor
gas turbine
compressed air
motor generator
air storage
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
JP9170177A
Other languages
Japanese (ja)
Inventor
Akimasa Mutsuyama
亮昌 六山
Noboru Nouchi
昇 野内
Hiroyuki Yamamoto
博之 山本
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP9170177A priority Critical patent/JPH1113480A/en
Publication of JPH1113480A publication Critical patent/JPH1113480A/en
Pending legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/16Mechanical energy storage, e.g. flywheels or pressurised fluids

Abstract

PROBLEM TO BE SOLVED: To provide a starting method that allows the drive and rotation of a compressor without setting up any starting equipment such as a starting motor and a thyristor or the like, in a compressed air storage power generating system. SOLUTION: Two clutches 2 and 3 at both sides of a motor generator 1 is made into a state of being connected to each other, and storage compressed air and fuel both are fed to gas turbines 4 and 5 from a cavity 15 and the gas turbines 4 and 5 are started to build up them up to the rated speed, thereby synchronizing the motor generator. Subsequently, the clutch 3 at the side of the gas turbines 4 and 5 is removed away and compressors 6 to 8 are rotated by the motor generator 1.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、電力需要の少いと
きに電動発電機で圧縮機を駆動して空気を圧縮して貯
え、電力需要時にその貯蔵圧縮空気を用いて燃料を燃焼
してガスタービンを駆動して発電するように構成した圧
縮空気貯蔵発電システム(CAES)の起動方法に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method of driving a compressor with a motor generator to compress and store air when power demand is small, and burning fuel using the stored compressed air when power demand is low. The present invention relates to a method for starting a compressed air storage power generation system (CAES) configured to drive a gas turbine to generate power.

【0002】[0002]

【従来の技術】圧縮空気貯蔵発電システムは、発電負荷
平準化のために考えられた発電システムであり、その基
本構成を図7に示してある。図7において、20は発電
機と電動機を兼ねる電動発電機を示している。
2. Description of the Related Art A compressed air storage power generation system is a power generation system that has been considered for power generation load leveling, and its basic configuration is shown in FIG. In FIG. 7, reference numeral 20 denotes a motor generator serving as both a generator and a motor.

【0003】電動発電機20は、両側にクラッチ21と
22を介して、それぞれ、圧縮機23とガスタービン2
6が設置されている。ガスタービン26は高圧段HPと
低圧段LPの2段で構成されたものが示されており、2
5は燃焼器を示している。
A motor generator 20 has a compressor 23 and a gas turbine 2 via clutches 21 and 22 on both sides, respectively.
6 are installed. The gas turbine 26 is shown as having two stages, a high pressure stage HP and a low pressure stage LP.
Reference numeral 5 denotes a combustor.

【0004】24は圧縮機23で加圧された空気を貯え
る空洞を示し、27は、ガスタービン26の排熱回収用
熱交換器としての再生器を示している。
[0004] Reference numeral 24 denotes a cavity for storing the air pressurized by the compressor 23, and reference numeral 27 denotes a regenerator as a heat exchanger for recovering exhaust heat of the gas turbine 26.

【0005】以上の構成をもつ圧縮空気貯蔵発電システ
ムでは、電動発電機20の両側にクラッチ21,22を
設置しており、このクラッチのON/OFFにより圧縮
機23の駆動による圧縮空気の充填と、ガスタービン2
6の駆動による発電を行っている。
In the compressed air storage and power generation system having the above configuration, clutches 21 and 22 are provided on both sides of the motor generator 20, and when the clutch is turned on / off, the compressor 23 is charged with compressed air. , Gas turbine 2
6 is generating power.

【0006】すなわち、電力需要の少いとき(夜間)は
電動発電機20を電動機として電力で駆動して圧縮機2
3を作動させ、空気を圧縮して空洞24やタンクに貯え
る。
That is, when the power demand is small (at night), the motor generator 20 is driven by electric power as a motor to drive the compressor 2.
Activate 3 to compress the air and store it in cavity 24 or tank.

【0007】この圧縮空気の充填時は、クラッチ21を
ON、クラッチ22をOFFとし電動発電機20により
圧縮機23を駆動して地下空洞24へ圧縮空気を貯える
のである。
When the compressed air is filled, the clutch 21 is turned on and the clutch 22 is turned off, and the compressor 23 is driven by the motor generator 20 to store the compressed air in the underground cavity 24.

【0008】一方、電力需要時(昼間)は、上記のよう
に貯えた加圧空気を取り出してガスタービンを駆動し、
電動発電機20を発電機として駆動し発電を行わせる。
On the other hand, during power demand (daytime), the compressed air stored as described above is taken out to drive the gas turbine,
The motor generator 20 is driven as a generator to generate power.

【0009】この発電時はクラッチ21をOFF、クラ
ッチ22をONとし地下空洞24より圧縮空気を送気し
て燃焼器25に燃料を送り着火しガスタービンを廻して
電動発電機20で発電を行わせるのである。
At the time of power generation, the clutch 21 is turned off, the clutch 22 is turned on, compressed air is supplied from the underground cavity 24, fuel is sent to the combustor 25, ignition is performed, the gas turbine is turned, and power is generated by the motor generator 20. To make it happen.

【0010】[0010]

【発明が解決しようとする課題】圧縮空気貯蔵発電シス
テムにおいては、圧縮機を起動するために、トルクコン
バータ、起動用モータ或いはサイリスタ等の起動装置を
設置する必要がある。これは、電動発電機が同期型であ
り外部入力を必要とするためである。
In the compressed air storage and power generation system, it is necessary to install a starting device such as a torque converter, a starting motor or a thyristor in order to start the compressor. This is because the motor generator is of a synchronous type and requires an external input.

【0011】圧縮空気貯蔵発電システムでは、ガスター
ビン、電動発電機、圧縮機等の他に起動装置を設置する
と機器構成が複雑になり、またその操作も複雑となるた
めシステムの信頼性が低下する懸念がある。
In a compressed air storage and power generation system, if a starting device is installed in addition to a gas turbine, a motor generator, a compressor, and the like, the equipment configuration becomes complicated, and the operation becomes complicated, so that the reliability of the system decreases. There are concerns.

【0012】本発明はこの問題点を解消するためになさ
れたもので、圧縮空気貯蔵発電システムにおいて、起動
用モータやサイリスタ等の起動装置を設置することなく
圧縮機の起動を可能とする起動方法を提供することを課
題としている。
The present invention has been made to solve this problem, and a starting method for starting a compressor without installing a starting device such as a starting motor or a thyristor in a compressed air storage and power generation system. The challenge is to provide

【0013】[0013]

【課題を解決するための手段】本発明では空気貯蔵源を
利用することにより前記課題を解決しようとするもの
で、電動発電機の両側のクラッチをONの状態にしガス
タービンに圧縮空気及び燃料を送り着火しガスタービン
を起動して定格回転数まで立ち上げた後、ガスタービン
側のクラッチを切離して電動発電機にて圧縮機を回転さ
せるようにした圧縮機の起動方法を提供する。
SUMMARY OF THE INVENTION The present invention is to solve the above-mentioned problem by utilizing an air storage source. The clutches on both sides of a motor generator are turned on to supply compressed air and fuel to a gas turbine. A method for starting a compressor is provided, in which a gas turbine is started by feeding and igniting to start up to a rated rotation speed, then a clutch on a gas turbine side is disconnected and the compressor is rotated by a motor generator.

【0014】圧縮空気貯蔵発電システムでは電動機と発
電機の機能を兼ねた電動発電機を採用している。電動発
電機はその特性により同期型であり、小型ガスタービン
で使用している誘導型とは異り外部から力を与えて定格
回転数まで立ち上げないと動力を取り出すことができな
い。
In the compressed air storage power generation system, a motor generator having both functions of a motor and a generator is employed. The motor generator is of a synchronous type due to its characteristics. Unlike an induction type used in a small gas turbine, power cannot be taken out unless an external force is applied to start up to a rated speed.

【0015】本発明の起動方法によれば、圧縮空気貯蔵
発電システムにおける圧縮空気源を利用し、ガスタービ
ンにその圧縮空気と燃料を送り着火しガスタービンによ
って定格回転数まで立ち上げることができる。
According to the starting method of the present invention, the compressed air and the fuel can be sent to the gas turbine using the compressed air source in the compressed air storage power generation system, ignited, and the gas turbine can be started up to the rated speed.

【0016】ガスタービンが定格回転数となればガスタ
ービン側のクラッチを切離して電動発電機で圧縮機を回
転させれば良い。以上のように、本発明によれば圧縮機
起動のための専用の起動装置を設置することなく圧縮機
を起動させることができる。
When the gas turbine reaches the rated speed, the clutch on the gas turbine side is disengaged and the compressor is rotated by the motor generator. As described above, according to the present invention, the compressor can be started without installing a dedicated starting device for starting the compressor.

【0017】[0017]

【発明の実施の形態】以下、本発明を図1〜図6を用い
て、実施の一形態に基づいて具体的に説明する。まず、
図1に示した圧縮空気貯蔵発電システムの構成について
説明する。図1において、1は電動発電機である。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be specifically described below with reference to FIGS. First,
The configuration of the compressed air storage and power generation system shown in FIG. 1 will be described. In FIG. 1, reference numeral 1 denotes a motor generator.

【0018】電動発電機1の両側にはクラッチ2,3を
介して第1段圧縮機6、第2段圧縮機7及び第3段圧縮
機8からなる圧縮機と、高圧ガスタービン4と低圧ガス
タービン5からなるガスタービンが配設されている。1
3はガスタービンの燃焼器、14はガスタービン排熱回
収用熱交換器(再生器)、15は圧縮空気を貯える空洞
である。
On both sides of the motor generator 1, a compressor comprising a first stage compressor 6, a second stage compressor 7 and a third stage compressor 8 via clutches 2 and 3, a high pressure gas turbine 4 and a low pressure A gas turbine including the gas turbine 5 is provided. 1
Reference numeral 3 denotes a gas turbine combustor, reference numeral 14 denotes a gas turbine exhaust heat recovery heat exchanger (regenerator), and reference numeral 15 denotes a cavity for storing compressed air.

【0019】9−1,9−2、10−1,10−2、1
1−1,11−2は放風弁であり、これらの放風弁を含
め、図示した弁については白地のものが開、黒く塗りつ
ぶしたものが閉の状態を示している。
9-1, 9-2, 10-1, 10-2, 1
Reference numerals 1-1 and 11-2 denote air release valves. With respect to the illustrated valves including these air release valves, those with a white background are open and those with black fill are closed.

【0020】以上の構成をもつ圧縮空気貯蔵発電システ
ムにおいて空洞15に貯蔵されている圧縮空気を利用し
て本発明により圧縮機を起動する場合の例を図1〜図6
を用いて説明する。
FIGS. 1 to 6 show an example in which the compressor is started according to the present invention using the compressed air stored in the cavity 15 in the compressed air storage and power generation system having the above configuration.
This will be described with reference to FIG.

【0021】図1は圧縮機起動前の状態で、電動発電機
1の両側のクラッチ2,3をONとしガスタービン4,
5と圧縮機6,7,8をつなげた状態にしている。な
お、この時、第1段(低圧)圧縮機6の可変前置静翼を
最底ブローの位置にしておく。
FIG. 1 shows a state before starting the compressor, in which the clutches 2 and 3 on both sides of the motor generator 1 are turned on, and the gas turbine 4 is turned on.
5 and the compressors 6, 7, 8 are connected. At this time, the variable front stationary blade of the first-stage (low-pressure) compressor 6 is set at the lowest blow position.

【0022】図2は、圧縮機起動前の圧縮機側の放風弁
の操作を示し、3台の圧縮機6,7,8の放風弁9−
1,9−2、10−1,10−2、11−1,11−2
を開とする。
FIG. 2 shows the operation of the blower valves on the compressor side before the compressor is started, and shows the blower valves 9- of the three compressors 6, 7, and 8.
1, 9-2, 10-1, 10-2, 11-1, 11-2
Open.

【0023】図3は、空洞15から圧縮空気をガスター
ビンに導いて燃焼器13に着火しガスタービンを駆動す
る状態を示し、通風〜着火を行う。通風〜着火で図中の
矢印のように弁操作を行う。図3においては、起動用の
流量調節弁12の系統にて燃焼器13に着火する。燃焼
器着火時の空気流量は定格時に対し大きく変化する。
FIG. 3 shows a state in which the compressed air is guided from the cavity 15 to the gas turbine and ignites the combustor 13 to drive the gas turbine. Valve operation is performed as shown by the arrow in the figure from ventilation to ignition. In FIG. 3, the combustor 13 is ignited by the system of the flow control valve 12 for starting. The air flow rate when the combustor ignites greatly changes from the rated time.

【0024】またこのシステムにおいては効率アップの
ためガスタービン排熱回収用熱交換器である再生器14
が設置されていてガスタービンに供給される空気は再生
器14を通過するときガスタービン排気により加熱され
る。
In this system, a regenerator 14 which is a heat exchanger for recovering exhaust heat of a gas turbine is used for improving efficiency.
The air supplied to the gas turbine is heated by the gas turbine exhaust when passing through the regenerator 14.

【0025】従って再生器14及び空洞15又は空気タ
ンクの状況によって起動時に流入する空気温度は大きく
変化するので流量調節弁12の弁開度を固定すると高圧
ガスタービン入口温度によって空気流量も大きく変化す
るのでコルドスタート(Coldstart )とホットスタート
(Hot start )の2つの運転モードで運転を行う必要が
ある。
Accordingly, the temperature of the air flowing in at the time of start-up greatly changes depending on the condition of the regenerator 14 and the cavity 15 or the air tank. Therefore, it is necessary to operate in two operation modes, cold start and hot start.

【0026】図4はガスタービンの起動後、ガスタービ
ンが定格回転数に到達するまでの状態を示しており、ガ
スタービンを定格回転数まで昇速し定格回転数に到達し
たら電動発電機1を同期する。
FIG. 4 shows a state after the gas turbine is started until the gas turbine reaches the rated speed. When the gas turbine is accelerated to the rated speed and reaches the rated speed, the motor generator 1 is turned off. Synchronize.

【0027】図5は、ガスタービンが定格回転数に達し
ガスタービンを離脱した状態を示しており、この状態に
おいては、燃焼器13の燃料を遮断しこれによってガス
タービン側クラッチ3をOFFとする。
FIG. 5 shows a state in which the gas turbine reaches the rated speed and separates from the gas turbine. In this state, the fuel in the combustor 13 is shut off, thereby turning off the gas turbine side clutch 3. .

【0028】図6は、圧縮機の起動が完了し、電動発電
機1によって駆動されている圧縮機から空洞15へ送風
を開始した状態を示している。すなわち、図6において
第1段圧縮機6の可変前置静翼を開きつつ放風弁9−
1,9−2、10−1,10−2、11−1,11−2
を閉操作し吐出圧力が空洞15又は空気タンクの圧を上
回った時点で送風を開始する。
FIG. 6 shows a state in which the start of the compressor has been completed, and air has been blown into the cavity 15 from the compressor driven by the motor generator 1. That is, in FIG. 6, while opening the variable front stationary blade of the first stage compressor 6, the blow-off valve 9-
1, 9-2, 10-1, 10-2, 11-1, 11-2
Is closed, and when the discharge pressure exceeds the pressure of the cavity 15 or the air tank, the blowing is started.

【0029】以上の操作によって、空洞15に貯えられ
た圧縮空気を利用してガスタービンにより圧縮機を起動
することができる。
With the above operation, the compressor can be started by the gas turbine using the compressed air stored in the cavity 15.

【0030】[0030]

【発明の効果】以上説明したように、本発明による圧縮
空気貯蔵発電システムにおける圧縮機の起動方法によれ
ば、電動発電機の両側のクラッチを接続の状態にしガス
タービンに貯蔵圧縮空気と燃料を送ってガスタービンを
起動し定格回転数まで立ち上げた後、ガスタービン側の
クラッチを切離して電動発電機によって圧縮機を回転さ
せる。
As described above, according to the method for starting the compressor in the compressed air storage and power generation system according to the present invention, the clutches on both sides of the motor generator are connected and the stored compressed air and fuel are supplied to the gas turbine. After sending the gas turbine to start up the gas turbine to the rated speed, the clutch on the gas turbine side is disconnected and the compressor is rotated by the motor generator.

【0031】従って、本発明の起動方法によれば、貯蔵
された加圧空気を利用してガスタービンによって圧縮機
を立ち上げることにより、従来必要とされていた起動装
置を省略することができる。
Therefore, according to the starting method of the present invention, by starting up the compressor by the gas turbine using the stored pressurized air, the starting device conventionally required can be omitted.

【0032】従って本発明によれば、圧縮空気貯蔵発電
システムの機器構成がシンプル化することができ、圧縮
空気貯蔵発電システムの信頼性が向上する。
Therefore, according to the present invention, the equipment configuration of the compressed air storage and power generation system can be simplified, and the reliability of the compressed air storage and power generation system is improved.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明の実施の一形態による圧縮機起動方法を
適用する圧縮空気貯蔵発電システムの構成を示す説明
図。
FIG. 1 is an explanatory diagram showing a configuration of a compressed air storage and power generation system to which a compressor starting method according to an embodiment of the present invention is applied.

【図2】図1の発電システムにおいて圧縮機起動に当り
放風弁を操作した状態を示す説明図。
FIG. 2 is an explanatory diagram showing a state in which a blow-off valve is operated in starting the compressor in the power generation system of FIG. 1;

【図3】図1の発電システムにおいて、圧縮機起動のた
めガスタービンへ通気しガスタービン燃焼器に着火する
までの状態を示す説明図。
FIG. 3 is an explanatory diagram showing a state in the power generation system of FIG. 1 from venting to a gas turbine to start a compressor to igniting a gas turbine combustor.

【図4】図1の発電システムにおいて、ガスタービン起
動後、電動発電機を同期駆動するまでの状態を示す説明
図。
FIG. 4 is an explanatory diagram showing a state after the gas turbine is started and before the motor generator is synchronously driven in the power generation system of FIG. 1;

【図5】図1の発電システムにおいて、圧縮機起動後、
ガスタービンを離脱した状態を示す説明図。
FIG. 5 In the power generation system of FIG. 1, after starting the compressor,
Explanatory drawing which shows the state which detached the gas turbine.

【図6】図1の発電システムにおいて、圧縮機により空
洞へ送風を開示した状態を示す説明図。
FIG. 6 is an explanatory diagram showing a state in which air is blown to the cavity by the compressor in the power generation system of FIG. 1;

【図7】従来の圧縮空気貯蔵発電システムの構成を示す
説明図。
FIG. 7 is an explanatory diagram showing a configuration of a conventional compressed air storage power generation system.

【符号の説明】[Explanation of symbols]

1 電動発電機 2,3 クラッチ 4 高圧段ガスタービン 5 低圧段ガスタービン 6 第1段圧縮機 7 第2段圧縮機 8 第3段圧縮機 9−1 放風弁 9−2 放風弁 10−1 放風弁 10−2 放風弁 11−1 放風弁 11−2 放風弁 12 流量調節弁 13 燃焼器 14 再生器 15 空洞 DESCRIPTION OF SYMBOLS 1 Motor generator 2, 3 Clutch 4 High pressure gas turbine 5 Low pressure gas turbine 6 1st stage compressor 7 2nd stage compressor 8 3rd stage compressor 9-1 Blow-off valve 9-2 Blow-off valve 10- DESCRIPTION OF SYMBOLS 1 Blow-off valve 10-2 Blow-off valve 11-1 Blow-off valve 11-2 Blow-off valve 12 Flow control valve 13 Combustor 14 Regenerator 15 Cavity

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 電動発電機の両側に、それぞれクラッチ
を介して設置された圧縮機及びガスタービンを備え、か
つ、前記圧縮機の下流側と前記ガスタービンの上流側の
間に空気貯蔵源を備え、電力需要の少いときに前記電動
発電機を駆動して前記圧縮機で圧縮した空気を前記空気
貯蔵源に貯え、電力需要時に貯蔵圧縮空気を用いて燃料
を燃焼して前記ガスタービンを駆動し発電するようにし
た圧縮空気貯蔵発電システムにおいて、前記電動発電機
の両側のクラッチを接続の状態にし前記ガスタービンに
貯蔵圧縮空気と燃料を送り前記ガスタービンを起動して
定格回転数まで立ち上げた後、前記ガスタービン側のク
ラッチを切離して前記電動発電機によって前記圧縮機を
回転させることを特徴とする圧縮空気貯蔵発電システム
における圧縮機の起動方法。
1. A compressor and a gas turbine respectively provided on both sides of a motor generator via a clutch, and an air storage source is provided between a downstream side of the compressor and an upstream side of the gas turbine. When the power demand is low, the motor generator is driven to store the air compressed by the compressor in the air storage source, and the fuel is burned using the stored compressed air at the time of power demand to operate the gas turbine. In the compressed air storage and power generation system configured to drive and generate electric power, the clutches on both sides of the motor generator are connected, the stored compressed air and fuel are sent to the gas turbine, and the gas turbine is started to stand up to a rated rotation speed. After raising, the clutch on the gas turbine side is disengaged, and the compressor is rotated by the motor generator. Movement method.
JP9170177A 1997-06-26 1997-06-26 Starting method for compressor in compressed air storage powder generating system Pending JPH1113480A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9170177A JPH1113480A (en) 1997-06-26 1997-06-26 Starting method for compressor in compressed air storage powder generating system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9170177A JPH1113480A (en) 1997-06-26 1997-06-26 Starting method for compressor in compressed air storage powder generating system

Publications (1)

Publication Number Publication Date
JPH1113480A true JPH1113480A (en) 1999-01-19

Family

ID=15900126

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9170177A Pending JPH1113480A (en) 1997-06-26 1997-06-26 Starting method for compressor in compressed air storage powder generating system

Country Status (1)

Country Link
JP (1) JPH1113480A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1119383C (en) * 2000-07-11 2003-08-27 湖北省化学研究所 Anisotyopic conductive adhesive and its preparing method
WO2007032978A3 (en) * 2005-09-14 2007-06-07 Conocophillips Co Rotation coupling employing torque converter and synchronization motor
US9249728B2 (en) 2011-06-30 2016-02-02 Hanwha Techwin Co., Ltd. Power generation system and power generation method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1119383C (en) * 2000-07-11 2003-08-27 湖北省化学研究所 Anisotyopic conductive adhesive and its preparing method
WO2007032978A3 (en) * 2005-09-14 2007-06-07 Conocophillips Co Rotation coupling employing torque converter and synchronization motor
US9249728B2 (en) 2011-06-30 2016-02-02 Hanwha Techwin Co., Ltd. Power generation system and power generation method

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