JPH1193621A - Hydrogen combustion turbine plant - Google Patents
Hydrogen combustion turbine plantInfo
- Publication number
- JPH1193621A JPH1193621A JP25209997A JP25209997A JPH1193621A JP H1193621 A JPH1193621 A JP H1193621A JP 25209997 A JP25209997 A JP 25209997A JP 25209997 A JP25209997 A JP 25209997A JP H1193621 A JPH1193621 A JP H1193621A
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- steam
- hydrogen
- combustor
- heat exchanger
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K25/00—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for
- F01K25/005—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for the working fluid being steam, created by combustion of hydrogen with oxygen
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Description
【０００１】[0001]
【発明の属する技術分野】本発明は、ＮＯx やＣＯ2 を
発生しない無公害の水素と酸素を燃焼させて高温の燃焼
ガス（高温の水蒸気）を発生し、その高温蒸気をタービ
ンに供給して発電するようにした水素燃焼タービンプラ
ントに関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for producing high-temperature combustion gas (high-temperature steam) by burning non-polluting hydrogen and oxygen that do not generate NO x and CO 2 , and supplying the high-temperature steam to a turbine. The present invention relates to a hydrogen combustion turbine plant configured to generate power.
【０００２】[0002]
【従来の技術】現在考えられている水素燃焼タービンプ
ラントとして高効率で実現性の高いサイクルの１つを図
２に示してある。図２において、２００は低圧圧縮機、
２０２は高圧圧縮機である。２０１は中間冷却器で、両
圧縮機２００，２０２の間に連絡されている。２０３は
第１熱交換器、２０４は燃焼器、２０５は第１タービン
である。2. Description of the Related Art FIG. 2 shows one of highly efficient and highly feasible cycles as a hydrogen combustion turbine plant currently considered. In FIG. 2, reference numeral 200 denotes a low-pressure compressor,
202 is a high-pressure compressor. An intercooler 201 is connected between the compressors 200 and 202. 203 is a first heat exchanger, 204 is a combustor, and 205 is a first turbine.
【０００３】２０６，２０７及び２０８は、図のように
第１タービン２０５の排気（水蒸気）が導かれてその排
熱を回収する第２熱交換器、第３熱交換器及び第４熱交
換器である。２０９は第２タービン、２１１は復水器、
２１７は第１給水加熱器、２１８は第２給水加熱器を示
している。２１２は第１ポンプ、２１３は第２ポンプで
ある。２１０は第３タービンを示し、２１４，２１５及
び２１６はそれぞれ発電機を示している。[0003] Reference numerals 206, 207, and 208 denote a second heat exchanger, a third heat exchanger, and a fourth heat exchanger for guiding the exhaust gas (steam) of the first turbine 205 and recovering the exhaust heat as shown in the figure. It is. 209 is a second turbine, 211 is a condenser,
217 denotes a first feed water heater, and 218 denotes a second feed water heater. 212 is a first pump, and 213 is a second pump. 210 indicates a third turbine, and 214, 215 and 216 each indicate a generator.
【０００４】このように構成された図２の水素燃焼ター
ビンプラントにおいて、後記するように第４熱交換器２
０８を出た第１タービン２０５の排気（水蒸気）は低圧
圧縮機２００で圧縮され、中間冷却器２０１で第２ポン
プ２１３で送られる給水と混合し冷却された後、高圧圧
縮機２０２で圧縮され、その後、第３タービン２１０の
出口蒸気の一部と混合された後、第１熱交換器２０３に
導かれる。In the hydrogen combustion turbine plant of FIG. 2 configured as described above, the fourth heat exchanger 2
08, the exhaust gas (steam) of the first turbine 205 is compressed by the low-pressure compressor 200, mixed with the feed water sent by the second pump 213 in the intercooler 201, cooled, and then compressed by the high-pressure compressor 202. Then, after being mixed with a part of the outlet steam of the third turbine 210, it is led to the first heat exchanger 203.
【０００５】第１熱交換器２０３で昇温した後の蒸気
は、燃焼器２０４に供給された水素および酸素と混合さ
れて燃焼され、その燃焼により発生した高温の燃焼ガス
（水蒸気）は第１タービン２０５に導入されてこれを駆
動する。[0005] The steam whose temperature has been raised in the first heat exchanger 203 is mixed with hydrogen and oxygen supplied to the combustor 204 and burned, and the high-temperature combustion gas (steam) generated by the combustion is converted into the first gas. It is introduced into the turbine 205 to drive it.
【０００６】第１タービン２０５を出た燃焼ガス（水蒸
気）は、熱交換器２０３，２０６に並列に分岐して導か
れて温度を下げた後、熱交換器２０７および２０８に導
かれ更に温度を下げた後、前記したように低圧圧縮機２
００へ流れる。[0006] The combustion gas (steam) leaving the first turbine 205 branches off in parallel to the heat exchangers 203 and 206 and is led to lower the temperature, and is then led to the heat exchangers 207 and 208 to further lower the temperature. After lowering, as described above, the low pressure compressor 2
Flows to 00.
【０００７】一方、第３熱交換器２０７を出て第４熱交
換器２０８へ流れる第１タービン２０５の排気（水蒸
気）の一部は分岐されて第２タービン２０９へ導かれて
これを駆動する。第２タービン２０９からの蒸気は復水
器２１１に導かれ、復水器２１１を出た復水は第１及び
第２給水加熱器２１７及び２１８で加熱された後、第１
ポンプ２１２により第４、第３、第２熱交換器２０８，
２０７，２０６に送られ更に加熱されて、蒸気となって
第３タービン２１０に供給されてこれを駆動する。On the other hand, a part of the exhaust gas (water vapor) of the first turbine 205 flowing out of the third heat exchanger 207 and flowing to the fourth heat exchanger 208 is branched and guided to the second turbine 209 to drive it. . The steam from the second turbine 209 is led to the condenser 211, and the condensate exiting the condenser 211 is heated by the first and second feed water heaters 217 and 218,
The fourth, third, and second heat exchangers 208,
The third turbine 210 is sent to the third turbine 210 and is driven there.
【０００８】第３タービン２１０を出た排気の一部は、
第１タービン２０５の冷却蒸気２１９として用いられ、
残部の排気は、前記したように高圧圧縮機２０２の出口
蒸気と混合される。また、復水器２１１を出た復水の一
部は、前記したように第２ポンプ２１３によって中間冷
却器２０１へ送られ低圧圧縮機２００の出口蒸気と混合
される。[0008] Part of the exhaust gas leaving the third turbine 210 is:
Used as cooling steam 219 for the first turbine 205,
The remaining exhaust gas is mixed with the outlet steam of the high-pressure compressor 202 as described above. Part of the condensate that has exited the condenser 211 is sent to the intercooler 201 by the second pump 213 and mixed with the outlet steam of the low-pressure compressor 200 as described above.
【０００９】[0009]
【発明が解決しようとする課題】図２に示した水素燃焼
タービンプラントでは、第３タービンを出た排気（水蒸
気）の一部が第１タービン２０５のタービン翼などの冷
却蒸気として用いられるが、このタービンプラントの更
なる高効率化のためには、第１タービン２０５の冷却蒸
気をできるだけ減少させるか、もしくは、発電端効率の
低下率の少ない冷却方式を採用することが必要となる。In the hydrogen combustion turbine plant shown in FIG. 2, a part of the exhaust gas (steam) exiting the third turbine is used as cooling steam for the turbine blades of the first turbine 205. In order to further increase the efficiency of this turbine plant, it is necessary to reduce the cooling steam of the first turbine 205 as much as possible, or to adopt a cooling method in which the rate of decrease in the power generation end efficiency is small.
【００１０】本発明は、水素と酸素とを燃焼させて高温
蒸気を発生し、この高温蒸気でタービンを駆動すると共
にタービン翼を蒸気で冷却するように構成した水素燃焼
タービンプラントにおいて、発電端効率の低下率を少く
することのできる冷却系統を採用した水素燃焼タービン
プラントを提供することを課題としている。[0010] The present invention relates to a hydrogen combustion turbine plant configured to generate high-temperature steam by burning hydrogen and oxygen, drive a turbine with the high-temperature steam, and cool turbine blades with steam. It is an object of the present invention to provide a hydrogen combustion turbine plant that employs a cooling system that can reduce the rate of decrease in fuel consumption.
【００１１】[0011]
【課題を解決するための手段】前記課題を解決するた
め、本発明は、水素と酸素とを燃焼器で燃焼させて高温
蒸気を発生し、その高温蒸気を第１タービンに供給して
これを駆動し、同第１タービンからの排気蒸気を熱交換
器に入れて排熱を与え、その熱交換器から流出した蒸気
を圧縮機に送り、同圧縮機からの圧縮蒸気を前記燃焼器
へ戻すサイクルを構成し、前記熱交換器で回収した排熱
を前記サイクルとは別置の第３タービンの入口流路に与
えると共に、前記熱交換器に前記第１タービンから流入
する蒸気の一部を前記圧縮機へ送る流路から抽気して別
置の第２タービンに送り、同第２タービンの戻り蒸気は
復水器に戻るように構成した水素燃焼タービンプラント
において次の構成を採用する。In order to solve the above-mentioned problems, the present invention generates high-temperature steam by burning hydrogen and oxygen in a combustor and supplies the high-temperature steam to a first turbine. Driven, and the exhaust steam from the first turbine is put into a heat exchanger to give exhaust heat, the steam flowing out of the heat exchanger is sent to a compressor, and the compressed steam from the compressor is returned to the combustor. Constitute a cycle, while providing the exhaust heat recovered by the heat exchanger to an inlet flow path of a third turbine separately provided from the cycle, and a part of steam flowing from the first turbine into the heat exchanger. The following configuration is adopted in a hydrogen combustion turbine plant configured to extract air from a flow passage to the compressor and send the extracted steam to a separately provided second turbine, and return steam of the second turbine is returned to a condenser.
【００１２】すなわち、本発明にあっては、前記第３タ
ービンの出口から抽気した蒸気を前記第１タービンに回
収型冷却蒸気として供給してタービン翼を冷却させ昇温
した蒸気を前記燃焼器の入口に回収する回収型冷却系統
を設ける。That is, according to the present invention, the steam extracted from the outlet of the third turbine is supplied to the first turbine as recovery cooling steam to cool the turbine blades and raise the temperature of the steam to the combustor. A recovery cooling system for recovery is provided at the entrance.
【００１３】本発明による水素燃焼タービンプラントで
は、前記したように第３タービンから第１タービンへ回
収型冷却系統によって導かれた冷却蒸気は燃焼器の入口
に回収されるので、その分、第１タービンガスパス内部
へ流れる冷却蒸気量が減少される。In the hydrogen combustion turbine plant according to the present invention, as described above, the cooling steam guided from the third turbine to the first turbine by the recovery type cooling system is recovered at the inlet of the combustor. The amount of cooling steam flowing into the turbine gas path is reduced.
【００１４】従って、本発明の水素燃焼タービンプラン
トではタービンガスパス内部への冷却蒸気の混入量が減
らされ、ガスパス内部流体の温度低下と冷却蒸気がガス
パス内流体と混合するときの圧力損失が減り、また、第
１タービンを冷却して得られた熱を燃焼器に回収し燃料
流量を減少させることができ、これにより発電端効率が
向上される。Therefore, in the hydrogen combustion turbine plant of the present invention, the amount of cooling steam mixed into the turbine gas path is reduced, and the temperature drop of the gas path internal fluid and the pressure loss when the cooling steam mixes with the gas path fluid are reduced. Further, the heat obtained by cooling the first turbine can be recovered in the combustor to reduce the fuel flow rate, thereby improving the power generation end efficiency.
【００１５】[0015]
【発明の実施の形態】以下、本発明による水素燃焼ター
ビンプラントを図１に示した実施の一形態に基づいて具
体的に説明する。なお、図１において、各部の符号に
は、１００台の数字を用いているが、１０台以下の数字
において、図２に示した２００台を除いた各部の符号と
同じ符号は同等の構成部分を示しており、それらについ
ての重複する説明は省略する。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, a hydrogen combustion turbine plant according to the present invention will be specifically described based on one embodiment shown in FIG. In FIG. 1, the reference numerals of each unit are 100 units. However, in the numbers of 10 units or less, the same reference numerals as those of the units except 200 units shown in FIG. , And redundant description thereof will be omitted.
【００１６】図１に示された水素燃焼タービンプラント
において図２に示したタービンプラントとの違いは、第
１タービン１０５の冷却において、従来と同様の第１タ
ービン冷却蒸気１１９に加え、第１タービン回収型冷却
蒸気１２０を第３タービン１１０出口より抽気し、第１
タービン１０５を冷却後、熱交換器１０３出口蒸気（燃
焼器１０４入口蒸気）と混合させる回収型冷却系統を追
加した点である。その他の系統は図２と実質同一であ
る。The difference between the hydrogen combustion turbine plant shown in FIG. 1 and the turbine plant shown in FIG. 2 is that, in cooling the first turbine 105, the first turbine cooling steam 119 similar to the conventional one and the first turbine The recovered cooling steam 120 is extracted from the third turbine 110 outlet,
The point is that a recovery type cooling system for cooling the turbine 105 and mixing it with the steam at the outlet of the heat exchanger 103 (the steam at the inlet of the combustor 104) is added. Other systems are substantially the same as those in FIG.
【００１７】図１の水素酸素燃焼タービンプラントで
は、前記したように、第１タービン１０５の冷却に、通
常の冷却方式に使用する第１タービン冷却蒸気１１９に
加え、第１タービン回収型冷却蒸気１２０を追加する。
表１と表２に本発明と従来の水素酸素燃焼タービンプラ
ントのサイクル計算例を示している。なお、表１と表２
は、それぞれ図１と図２に番号を記した位置での流量、
温度、圧力を示している。In the hydrogen-oxygen combustion turbine plant shown in FIG. 1, as described above, the first turbine 105 is cooled in addition to the first turbine cooling steam 119 used in the ordinary cooling method. Add.
Tables 1 and 2 show cycle calculation examples of the present invention and a conventional hydrogen-oxygen combustion turbine plant. Table 1 and Table 2
Are the flow rates at the positions numbered in FIGS. 1 and 2, respectively.
Shows temperature and pressure.
【００１８】[0018]
【表１】 [Table 1]
【００１９】[0019]
【表２】 [Table 2]
【００２０】表１及び表２に示されているように、本発
明では、従来より第１タービンの冷却媒体割合の総量は
０．１５から０．１７２へ増加するものの、この０．１
７２の内、０．１０９が回収型冷却蒸気へ置きかわり、
第１タービンガスパス内部への冷却蒸気混入量が０．１
５（従来）から０．０６３（本発明）へと減少する。こ
れによって、発電端効率は６０．３％から６１．０％へ
相対的に１．２％向上する作用がある。（計算上の仮定
には表３を使用した。） すなわち、第１タービン冷却蒸気１１９のような通常の
冷却方式と第１タービン回収型冷却蒸気１２０のような
回収型の冷却方式では、回収型の冷却方式の方がタービ
ンガスパス内部への冷却媒体の混入によるガスパス内部
流体の温度低下、および冷却媒体とガスパス内部流体が
混合する時の圧力損失が無くなるため、冷却によるター
ビン出力の低下が小さくなる作用がある。また、回収型
の冷却によりタービンより得られた熱量を燃焼器の上流
へ回収することにより、燃料流量が減少できることも発
電端効率を向上させる理由である。As shown in Tables 1 and 2, in the present invention, although the total amount of the cooling medium in the first turbine is increased from 0.15 to 0.172, the amount of the cooling medium in the first turbine is increased by 0.1%.
Of the 72, 0.109 is replaced by recovery type cooling steam,
The amount of cooling steam mixed into the first turbine gas path is 0.1
5 (conventional) to 0.063 (present invention). As a result, there is an effect that the power generation end efficiency is relatively improved by 1.2% from 60.3% to 61.0%. (Table 3 was used for the calculation assumption.) That is, in the normal cooling method such as the first turbine cooling steam 119 and the recovery cooling method such as the first turbine recovery type cooling steam 120, the recovery type cooling method is used. The cooling method reduces the temperature drop of the fluid inside the gas path due to mixing of the cooling medium into the turbine gas path, and reduces the pressure loss when the cooling medium and the gas path internal fluid are mixed. There is a function. In addition, the amount of heat obtained from the turbine by the recovery type cooling is recovered to the upstream of the combustor, so that the fuel flow rate can be reduced, which is another reason for improving the power generation end efficiency.
【００２１】[0021]
【表３】 [Table 3]
【００２２】[0022]
【発明の効果】以上説明したように、本発明は、水素燃
焼器からの高温蒸気で駆動される第１タービンと、排熱
を一部回収した第１タービンの排気の一部を抽気して導
かれる第２タービンと、第１タービンの排熱を回収した
蒸気により駆動される第３タービンを有する水素燃焼タ
ービンプラントにおいて、第３タービンの出口から抽気
した蒸気を第１タービンに回収型冷却蒸気として供給し
てタービン翼を冷却させ昇温した蒸気を水素燃焼器の入
口に回収する回収型冷却系統を設けたものである。As described above, according to the present invention, the first turbine driven by the high-temperature steam from the hydrogen combustor and a part of the exhaust gas of the first turbine which partially recovers the exhaust heat are extracted. In a hydrogen combustion turbine plant having a second turbine guided and a third turbine driven by steam recovered from exhaust heat of the first turbine, steam extracted from an outlet of the third turbine is recovered and cooled to the first turbine. And a recovery-type cooling system for recovering steam that has been supplied to cool the turbine blades and raise the temperature at the inlet of the hydrogen combustor.
【００２３】この本発明の水素燃焼タービンプラントに
よれば、第３タービンから冷却のため第１タービンへ導
かれた蒸気は燃焼器の入口に回収されるので、その分だ
け、第１タービンガスパス内部へ流れる冷却蒸気量が減
少される。According to the hydrogen combustion turbine plant of the present invention, since the steam guided from the third turbine to the first turbine for cooling is recovered at the inlet of the combustor, the first turbine gas path is correspondingly recovered. The amount of cooling steam flowing into the inside is reduced.
【００２４】このようにタービンガスパス内部への冷却
蒸気の混入量が減らされるので、ガスパス内部流体の温
度低下と冷却蒸気がガスパス内流体と混合するときの圧
力損失が減り、また、第１タービンを冷却して得られた
熱を燃焼器に回収し燃料流量を減少させることができ、
これらの作用により発電端効率が向上される。As described above, since the amount of cooling steam mixed into the turbine gas path is reduced, the temperature drop of the gas path internal fluid and the pressure loss when the cooling steam mixes with the gas path fluid are reduced. The heat obtained by cooling is recovered in the combustor and the fuel flow rate can be reduced,
By these actions, the power generation end efficiency is improved.
【図１】本発明の実施の一形態による水素燃焼タービン
プラントの系統図。FIG. 1 is a system diagram of a hydrogen combustion turbine plant according to an embodiment of the present invention.
【図２】従来の水素燃焼タービンプラントの系統図。FIG. 2 is a system diagram of a conventional hydrogen combustion turbine plant.
１００，２００ 低圧圧縮機 １０１，２０１ 中間冷却器 １０２，２０２ 高圧圧縮機 １０３，２０３ 第１熱交換器 １０４，２０４ 燃焼器 １０５，２０５ 第１タービン １０６，２０６ 第２熱交換器 １０７，２０７ 第３熱交換器 １０８，２０８ 第４熱交換器 １０９，２０９ 第２タービン １１０，２１０ 第３タービン １１１，２１１ 復水器 １１２，２１２ 第１ポンプ １１３，２１３ 第２ポンプ １１４，２１４ 第１発電機 １１５，２１５ 第２発電機 １１６，２１６ 第３発電機 １１７，２１７ 第１給水加熱器 １１８，２１８ 第２給水加熱器 １１９，２１９ 第１タービン冷却蒸気 １２０ 第１タービン回収型冷却蒸気 100, 200 Low-pressure compressor 101, 201 Intercooler 102, 202 High-pressure compressor 103, 203 First heat exchanger 104, 204 Combustor 105, 205 First turbine 106, 206 Second heat exchanger 107, 207 Third Heat exchangers 108, 208 Fourth heat exchangers 109, 209 Second turbines 110, 210 Third turbines 111, 211 Condensers 112, 212 First pumps 113, 213 Second pumps 114, 214 First generators 115, 215 Second generator 116,216 Third generator 117,217 First feedwater heater 118,218 Second feedwater heater 119,219 First turbine cooling steam 120 First turbine recovery type cooling steam
Claims (1)
蒸気を発生し、その高温蒸気を第１タービンに供給して
これを駆動し、同第１タービンからの排気蒸気を熱交換
器に入れて排熱を与え、その熱交換器から流出した蒸気
を圧縮機に送り、同圧縮機からの圧縮蒸気を前記燃焼器
へ戻すサイクルを構成し、前記熱交換器で回収した排熱
を前記サイクルとは別置の第３タービンの入口流路に与
えると共に、前記熱交換器に前記第１タービンから流入
する蒸気の一部を前記圧縮機へ送る流路から抽気して別
置の第２タービンに送り、同第２タービンの戻り蒸気は
復水器に戻るように構成した水素燃焼タービンプラント
において、前記第３タービンの出口から抽気した蒸気を
前記第１タービンに回収型冷却蒸気として供給してター
ビン翼を冷却させ昇温した蒸気を前記燃焼器の入口に回
収する回収型冷却系統を設けたことを特徴とする水素燃
焼タービンプラント。1. A high-temperature steam is generated by burning hydrogen and oxygen in a combustor, and the high-temperature steam is supplied to and driven by a first turbine, and exhaust steam from the first turbine is converted into a heat exchanger. To give a waste heat, send out the steam flowing out of the heat exchanger to the compressor, constitute a cycle to return the compressed steam from the compressor to the combustor, the waste heat recovered in the heat exchanger The cycle is supplied to an inlet flow path of a third turbine separately provided, and a part of steam flowing into the heat exchanger from the first turbine is extracted from a flow path that is sent to the compressor, and the steam is extracted from a flow path of the separately provided third turbine. In the hydrogen combustion turbine plant configured to send steam to the second turbine and return steam from the second turbine to the condenser, supply steam extracted from the outlet of the third turbine to the first turbine as recovered cooling steam. To cool and raise the turbine blades A hydrogen-fired turbine plant comprising a recovery-type cooling system for recovering heated steam at an inlet of the combustor.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP25209997A JPH1193621A (en) | 1997-09-17 | 1997-09-17 | Hydrogen combustion turbine plant |
| EP98115532A EP0900921A3 (en) | 1997-09-05 | 1998-08-18 | Hydrogen burning turbine plant |
| CA002245470A CA2245470A1 (en) | 1997-09-05 | 1998-08-25 | Hydrogen burning turbine plant |
| US09/145,018 US6282883B1 (en) | 1997-09-05 | 1998-09-01 | Hydrogen burning turbine plant |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP25209997A JPH1193621A (en) | 1997-09-17 | 1997-09-17 | Hydrogen combustion turbine plant |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH1193621A true JPH1193621A (en) | 1999-04-06 |
Family
ID=17232510
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP25209997A Pending JPH1193621A (en) | 1997-09-05 | 1997-09-17 | Hydrogen combustion turbine plant |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH1193621A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105134318A (en) * | 2015-08-07 | 2015-12-09 | 上海交通大学 | Energy storage device based on hydrogen-steam turbine compound cycle |
| GB2533547A (en) * | 2014-10-30 | 2016-06-29 | Parsons Brinckerhoff Ltd | Process and plant for power generation |
-
1997
- 1997-09-17 JP JP25209997A patent/JPH1193621A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2533547A (en) * | 2014-10-30 | 2016-06-29 | Parsons Brinckerhoff Ltd | Process and plant for power generation |
| GB2533547B (en) * | 2014-10-30 | 2018-10-03 | Parsons Brinckerhoff Ltd | Process and plant for power generation |
| CN105134318A (en) * | 2015-08-07 | 2015-12-09 | 上海交通大学 | Energy storage device based on hydrogen-steam turbine compound cycle |
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