WO2010038290A1 - ガスタービン装置 - Google Patents
ガスタービン装置 Download PDFInfo
- Publication number
- WO2010038290A1 WO2010038290A1 PCT/JP2008/067825 JP2008067825W WO2010038290A1 WO 2010038290 A1 WO2010038290 A1 WO 2010038290A1 JP 2008067825 W JP2008067825 W JP 2008067825W WO 2010038290 A1 WO2010038290 A1 WO 2010038290A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- gas
- mixed
- hydrogen
- gas turbine
- fuel
- Prior art date
Links
- 239000007789 gas Substances 0.000 claims abstract description 514
- 239000002737 fuel gas Substances 0.000 claims abstract description 72
- 238000002156 mixing Methods 0.000 claims abstract description 53
- 230000005484 gravity Effects 0.000 claims abstract description 27
- 239000000567 combustion gas Substances 0.000 claims abstract description 21
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 134
- 239000001301 oxygen Substances 0.000 claims description 134
- 229910052760 oxygen Inorganic materials 0.000 claims description 134
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 132
- 239000001257 hydrogen Substances 0.000 claims description 132
- 229910052739 hydrogen Inorganic materials 0.000 claims description 132
- 238000010790 dilution Methods 0.000 claims description 58
- 239000012895 dilution Substances 0.000 claims description 58
- 239000000203 mixture Substances 0.000 claims description 12
- 238000011144 upstream manufacturing Methods 0.000 claims description 9
- 238000007865 diluting Methods 0.000 claims description 7
- 238000003756 stirring Methods 0.000 claims description 4
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 239000000446 fuel Substances 0.000 description 24
- 238000004880 explosion Methods 0.000 description 16
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 13
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 8
- 239000006227 byproduct Substances 0.000 description 8
- 238000010586 diagram Methods 0.000 description 7
- 239000003345 natural gas Substances 0.000 description 6
- 239000000571 coke Substances 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 5
- 238000011084 recovery Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 239000001273 butane Substances 0.000 description 4
- IJDNQMDRQITEOD-UHFFFAOYSA-N n-butane Chemical compound CCCC IJDNQMDRQITEOD-UHFFFAOYSA-N 0.000 description 4
- OFBQJSOFQDEBGM-UHFFFAOYSA-N n-pentane Natural products CCCCC OFBQJSOFQDEBGM-UHFFFAOYSA-N 0.000 description 4
- 239000001294 propane Substances 0.000 description 4
- 239000003085 diluting agent Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000000926 separation method Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910001873 dinitrogen Inorganic materials 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000001568 sexual effect Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/40—Control of fuel supply specially adapted to the use of a special fuel or a plurality of fuels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/26—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension
- F02C3/28—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension using a separate gas producer for gasifying the fuel before combustion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/236—Fuel delivery systems comprising two or more pumps
-
- 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]
Definitions
- the present invention relates to a gas turbine apparatus that uses a mixed gas obtained by mixing three or more kinds of gases as a fuel gas for a combustor.
- a low-calorie gas-only-fired gas turbine device that can generally use a plurality of low-calorie gases having different calories at the same time It has been known.
- This low-calorie gas-only fired gas turbine device is used in, for example, an ironworks.
- various by-product gases such as blast furnace gas (B gas), coke oven gas (C gas), and converter gas (L gas) are generated in the manufacturing process of steel products.
- B gas blast furnace gas
- C gas coke oven gas
- L gas converter gas
- Patent Document 1 A specific example of such a gas turbine apparatus that uses a mixed gas obtained by mixing a plurality of types of by-product gas and natural gas as a fuel gas for a combustor is disclosed in Patent Document 1 below, for example.
- gas turbine apparatus disclosed in Patent Document 1 blast furnace gas, coke oven gas, and natural gas are mixed in a mixing section 51 as shown in FIG. 4, and the combustor of the gas turbine 52 is made by using the mixed gas as fuel gas. To supply.
- Patent Document 2 discloses an example of a gas turbine device that supplies a part of combustion gas discharged from a gas turbine to an air compressor and reuses it.
- JP 2004-27975 A Japanese Patent No. 295456
- the present invention is a gas in which three or more kinds of gases (for example, a single gas such as butane gas and propane gas, or a gas in which a plurality of kinds of gases such as blast furnace gas and converter gas are mixed) are used.
- a gas turbine apparatus capable of generating a mixed gas in which three or more of these gases are uniformly mixed, and further capable of preventing explosion by monitoring the hydrogen concentration and oxygen concentration in the mixed gas. This is the issue.
- a gas turbine device that solves the above-mentioned problem burns fuel gas supplied from a fuel gas supply device together with compressed air supplied from an air compressor in a combustor, and gas is generated by the combustion gas generated at this time.
- the fuel gas supply device configured to rotationally drive the turbine,
- the fuel gas supply device has a plurality of mixers. In these mixers, three or more kinds of gases are mixed in order from the lighter specific gravity or mixed in order from the higher specific gravity. The mixed gas is supplied to the combustor as the fuel gas.
- the gas turbine device of the second invention is the gas turbine device of the first invention
- the fuel gas supply device comprises: A hydrogen / oxygen sensor for detecting hydrogen concentration and oxygen concentration in the mixed gas; A dilution gas mixing device for mixing a dilution gas for diluting the hydrogen concentration and oxygen concentration with the mixed gas; A control device for operating the dilution gas mixing device to mix the dilution gas into the mixed gas when the hydrogen concentration and oxygen concentration detected by the hydrogen / oxygen sensor are equal to or higher than a set value; It is set as the structure which has these.
- the gas turbine device of the third invention is the gas turbine device of the second invention,
- the dilution gas mixing apparatus is characterized in that a part of the combustion gas discharged from the gas turbine is mixed with the mixed gas as the dilution gas.
- the gas turbine apparatus of 4th invention is the gas turbine apparatus of 1st invention
- the fuel gas supply device includes a remixer that stirs and remixes the mixed gas.
- the gas turbine apparatus of 5th invention is the gas turbine apparatus of 4th invention
- the fuel gas supply device comprises: A hydrogen / oxygen sensor for detecting hydrogen concentration and oxygen concentration in the mixed gas; A control device for remixing the mixed gas by operating the remixer when the hydrogen concentration and the oxygen concentration detected by the hydrogen / oxygen sensor exceed a set value; It is set as the structure which has these.
- the gas turbine apparatus of 6th invention is the gas turbine apparatus of 1st invention
- the fuel gas supply device comprises: A hydrogen / oxygen sensor for detecting hydrogen concentration and oxygen concentration in the mixed gas; An emergency release valve; A control device for operating the emergency release valve to release the mixed gas when the hydrogen concentration and the oxygen concentration detected by the hydrogen / oxygen sensor exceed a set value; It is set as the structure which has these.
- a gas turbine device is the gas turbine device according to any one of the second, fifth and sixth aspects of the invention.
- the fuel gas supply device is downstream of the hydrogen / oxygen sensor, mixing the dilution gas by the dilution gas mixing device, remixing the mixed gas by the remixer, or the emergency discharge valve.
- the mixed gas is discharged.
- a gas turbine apparatus is the gas turbine apparatus according to any one of the second to seventh inventions, A gas compressor that compresses the mixed gas and supplies the compressed gas to the combustor;
- the fuel gas supply device is arranged on the upstream side of the gas compressor to mix the dilution gas by the dilution gas mixing device, remix the gas mixture by the remixer, or the gas mixture by the emergency discharge valve. It is the structure which discharge
- the fuel gas supplied from the fuel gas supply apparatus is combusted in the combustor together with the compressed air supplied from the air compressor, and the gas turbine is rotated by the combustion gas generated at this time.
- the fuel gas supply apparatus includes a plurality of mixers, and these mixers mix three or more kinds of gases in order from a lighter specific gravity or a higher specific gravity. Since the mixed gas is generated in order from the one to produce a mixed gas, and this mixed gas is supplied to the combustor as the fuel gas, it is characterized in that it is mixed in order from the one with the lower specific gravity and the one with the higher specific gravity in order.
- mixing is performed sequentially from the one having a specific gravity. For this reason, it is possible to generate a mixed gas in which three or more kinds of gases are uniformly mixed. By using this uniform mixed gas as the fuel gas of the combustor, the occurrence of uneven combustion is prevented and stable combustion is possible. It becomes.
- the fuel gas supply device includes a hydrogen / oxygen sensor for detecting a hydrogen concentration and an oxygen concentration in the mixed gas, and the hydrogen A dilution gas mixing device that mixes a dilution gas for diluting the concentration and oxygen concentration with the mixed gas, and the dilution gas when the hydrogen concentration and oxygen concentration detected by the hydrogen / oxygen sensor exceed a set value. It is characterized by having a control device that operates a mixing device and mixes the dilution gas with the mixed gas, so that hydrogen and oxygen in the mixed gas are liberated and hydrogen and oxygen lumps are generated.
- the dilution gas mixing device converts a part of the combustion gas discharged from the gas turbine into the mixed gas as the dilution gas. Since the combustion gas is effectively used as the diluent gas and nitrogen gas is not required, an efficient and inexpensive gas turbine device can be realized.
- the fuel gas supply device includes a remixer for stirring and remixing the mixed gas. Therefore, even if hydrogen or oxygen in the mixed gas is liberated and hydrogen lumps or oxygen lumps are generated (even if specific gravity separation occurs), the mixed gas is supplied before being supplied to the combustor. A uniform mixing state can be obtained again by stirring and remixing in a remixer. For this reason, the danger of an explosion is reduced and the safe operation of the gas turbine apparatus becomes possible.
- the fuel gas supply device includes a hydrogen / oxygen sensor for detecting a hydrogen concentration and an oxygen concentration in the mixed gas, and the hydrogen A control device for operating the remixer to remix the mixed gas when the hydrogen concentration and oxygen concentration detected by an oxygen sensor exceed a set value; Even if hydrogen and oxygen in the mixed gas are liberated and hydrogen and oxygen lumps are generated (even if specific gravity separation occurs), before the mixed gas with high hydrogen concentration and oxygen concentration is supplied to the combustor By detecting that the hydrogen concentration and oxygen concentration of the mixed gas are equal to or higher than the set values, and before the mixed gas is supplied to the combustor, the mixed gas is stirred in the remixer and remixed again. , Average It can be mixed state. For this reason, the danger of an explosion is reduced and the safe operation of the gas turbine apparatus becomes possible.
- the fuel gas supply device includes a hydrogen / oxygen sensor that detects a hydrogen concentration and an oxygen concentration in the mixed gas, and an emergency release. And a control device that operates the emergency release valve to release the mixed gas when the hydrogen concentration and the oxygen concentration detected by the hydrogen / oxygen sensor exceed a set value. Therefore, when the hydrogen concentration and oxygen concentration of the mixed gas increase due to the release of hydrogen and oxygen in the mixed gas and the generation of hydrogen and oxygen lumps, the mixed gas is supplied to the combustor. It is possible to release the mixed gas by detecting that the hydrogen concentration and the oxygen concentration of the mixed gas are equal to or higher than the set values before the gas is discharged. For this reason, the danger of an explosion is reduced and the safe operation of the gas turbine apparatus becomes possible.
- the fuel gas supply device is located downstream of the hydrogen / oxygen sensor, and Since the configuration is such that the dilution gas is mixed by the dilution gas mixing device, the mixed gas is remixed by the remixer, or the mixed gas is released by the emergency discharge valve.
- the mixed gas with high hydrogen concentration and oxygen concentration detected by the hydrogen / oxygen sensor, it is more reliable to mix the dilution gas by the dilution gas mixing device, the remixing of the mixed gas by the remixer, or the emergency.
- the mixed gas can be discharged by the discharge valve.
- the gas turbine apparatus of any one of the second to seventh inventions further comprising a gas compressor that compresses the mixed gas and supplies the compressed mixed gas to the combustor.
- the fuel gas supply device is arranged on the upstream side of the gas compressor to mix the dilution gas by the dilution gas mixing device, remix the gas mixture by the remixer, or the gas mixture by the emergency discharge valve. It is characterized by the structure that discharges the gas, and before the mixed gas with high hydrogen concentration and oxygen concentration flows into the gas compressor, the diluted gas is mixed by the diluted gas mixing device, and the mixed gas is remixed by the remixer. Alternatively, since the mixed gas is released by the emergency release valve, the risk of explosion can be reliably reduced even for the gas turbine device having the gas compressor.
- FIG. 1 is a configuration diagram of a gas turbine apparatus according to Embodiment 1 of the present invention.
- the gas turbine apparatus according to the first embodiment is a combined power generation apparatus that operates a gas turbine and a steam turbine to generate power, and includes a gas turbine 1, a steam turbine 5, a combustor 2, and air.
- the compressor 3, the generator 4, the gas compressor 6, the exhaust heat recovery boiler 7, and the fuel gas supply device 8 are provided.
- the mixed gas a generated by the fuel gas supply device 8 flows into the gas compressor 6 via the fuel supply line 9 and is compressed here, and then is supplied as fuel gas to the combustor 2 via the fuel supply line 10. Supplied.
- the fuel gas (mixed gas a) supplied from the fuel gas supply device 8 is burned together with the compressed air b supplied from the air compressor 3.
- the combustion gas c generated at this time is supplied to the gas turbine 1 to rotationally drive the gas turbine 1.
- the gas turbine 1, the steam turbine 5, the air compressor 3, the generator 4 and the gas compressor 6 are disposed on the same rotating shaft 11, and the air compressor 3, the generator 4 and the gas compressor 6 are gas turbines. 1 and the steam turbine 5 are rotationally driven.
- the air compressor 3 sucks outside air (air) g and compresses it, and supplies the compressed air b to the combustor 2 as described above.
- the generator 4 generates power and transmits this generated power to a power system (not shown) inside or outside the steelworks.
- the gas compressor 6 sucks and compresses the mixed gas a, and supplies the compressed mixed gas a to the combustor 2 as described above.
- the fuel gas supply device 8 which is a feature of the first embodiment, has two mixers 15, 16, and these mixers 15, 16 use the three types of first gas I, second gas.
- the gas II and the third gas III are mixed in order from a lighter specific gravity or mixed in order from a higher specific gravity to produce a mixed gas a, and the mixed gas a is passed through the gas compressor 6 as described above. It is configured to supply to the combustor 2.
- a downstream end of a fuel supply line 18 provided with a flow rate adjustment valve 17 and a downstream end of a fuel supply line 20 provided with a flow rate adjustment valve 19 are connected on the inlet side of the first mixer 15.
- the upstream end of the fuel supply line 21 is connected to the outlet side of the first mixer 15.
- the downstream end of the fuel supply line 21 and the downstream end of the fuel supply line 23 provided with the flow rate adjusting valve 22 are connected to the inlet side of the second mixer 16, while the outlet side of the second mixer 16 is connected. Is connected to the upstream end of the fuel supply line 9.
- the fuel gas supply device 8 first, in the first mixer 15, the first gas I supplied through the fuel supply line 18 while the flow rate is adjusted by the flow rate adjustment valve 17, and the flow rate adjustment by the flow rate adjustment valve 19.
- the second gas II supplied through the fuel supply line 20 is mixed while the mixed gas f is generated.
- the third gas III supplied through the fuel supply line 23 while the flow rate is adjusted by the flow control valve 22, and the mixed gas f supplied through the fuel supply line 21. Are mixed to generate a mixed gas a.
- the first gas I, the second gas II, and the third gas III have a specific gravity relationship such that the first gas I ⁇ second gas II ⁇ third gas III or the first gas I> second.
- the gas II is selected to be greater than the third gas III.
- the 1st gas I, the 2nd gas II, and the 3rd gas III are mixed in an order from light specific gravity, or are mixed in order from a heavy specific gravity.
- Table 1 shows the specific gravity of each gas type.
- the first gas I is blast furnace gas when they are mixed in descending order of specific gravity.
- the second gas II is natural gas
- the third gas III is coke oven gas
- the gases are mixed in order from lighter specific gravity
- the first gas I is coke oven gas
- the second gas II is natural gas
- the third gas III becomes blast furnace gas.
- the fuel gas supplied from the fuel gas supply device 8 is burned in the combustor 2 together with the compressed air b supplied from the air compressor 3, and is generated at this time.
- the fuel gas supply device 8 configured to rotationally drive the gas turbine 1 with the combustion gas c, the fuel gas supply device 8 has two mixers 15 and 16, and these mixers 15 and 16 use the three first types.
- the gas I, the second gas II, and the third gas III are mixed in order from the lighter specific gravity or mixed in order from the higher specific gravity to generate the mixed gas a, and the combustor uses the mixed gas a as the fuel gas.
- the components are mixed in order from the one with the lower specific gravity. Therefore, it is possible to generate a mixed gas a in which three kinds of the first gas I, the second gas II, and the third gas III are uniformly mixed, and this uniform mixed gas a is used as the fuel gas of the combustor 2. This prevents the occurrence of uneven combustion and enables stable combustion.
- the present invention there are three kinds of gases (for example, three kinds of gases such as a single gas such as butane gas and propane gas, or a mixture of plural kinds of gases such as blast furnace gas and converter gas).
- the gas is not limited to a mixture of three or more gases (for example, a single gas such as butane gas or propane gas, or a gas in which a plurality of gases such as blast furnace gas or converter gas are mixed). It can also be applied to the case of mixing three or more gases.
- FIG. 2 is a configuration diagram of a gas turbine apparatus according to Embodiment 2 of the present invention. 2 that are the same as those in FIG. 1 (Embodiment 1) are assigned the same reference numerals as in FIG. 1, and detailed descriptions thereof are omitted.
- a hydrogen / oxygen sensor is further provided in the fuel gas supply device 8 of the second embodiment.
- a hydrogen / oxygen sensor is further provided. 31, 39, an emergency discharge valve 32, a control device 33, and a dilution gas mixing device 34.
- the hydrogen / oxygen sensor 31 is provided in the fuel supply line 9 on the downstream side of the second mixer 16 and detects the hydrogen concentration and oxygen concentration in the mixed gas a.
- the emergency release valve 32 is a three-way valve provided in the fuel supply line 9 on the downstream side of the hydrogen / oxygen sensor 31. Normally, the mixed gas a is circulated to the gas compressor 6 side and supplied to the combustor 2. In an emergency where the hydrogen concentration or oxygen concentration in the mixed gas a is high, the flow direction is switched and the mixed gas a is discharged from the fuel supply line 9.
- the dilution gas mixing device 34 has a configuration in which a ventilator 36, a gas cooler 37, and a flow rate adjusting valve 38 are arranged in the dilution gas supply line 35 sequentially from the upstream side.
- the upstream side of the dilution gas supply line 35 is connected to the exhaust line 12 on the downstream side of the exhaust heat recovery boiler 7, and the downstream side of the dilution gas supply line 35 is connected to the fuel supply line 9 on the downstream side of the emergency release valve 32. It is connected to the.
- the ventilator 36 when the ventilator 36 is activated, a part of the combustion gas (exhaust gas) c flowing through the exhaust line 12 is introduced into the dilution gas supply line 35, cooled by the gas cooler 37, and flowed by the flow rate adjustment valve 38. It is adjusted and mixed with the mixed gas a as a diluent gas. At this time, the hydrogen concentration and the oxygen concentration in the mixed gas a are diluted with a part of the fuel gas a (diluted gas) to be reduced.
- the connecting portion of the fuel supply line 9 and the dilution gas supply line 35 is a mixing portion, but a mixer is provided here to mix the mixed gas a and the combustion gas (exhaust gas) c. Also good.
- the hydrogen / oxygen sensor 39 supplies fuel immediately after the connecting portion (mixing portion) where the mixed gas a and the combustion gas (exhaust gas) c are mixed on the downstream side of the emergency release valve 32 and before entering the gas compressor 6. It is provided in the line 9 and detects the hydrogen concentration and oxygen concentration in the mixed gas a or the hydrogen concentration and oxygen concentration in the mixed gas of the mixed gas a and the combustion gas (exhaust gas) c.
- the dilution gas mixing device 34 when the hydrogen concentration and the oxygen concentration in the mixed gas a detected by the hydrogen / oxygen sensor 31 are equal to or higher than the first set value (value set lower than the explosion limit), the dilution gas mixing device 34 is used. Is activated. That is, the ventilator 36 is started and the flow rate adjustment valve 38 is opened to start the flow rate adjustment. As a result, as described above, a part of the combustion gas (exhaust gas) c is mixed with the mixed gas a as a diluent gas. Further, in the control device 33, the hydrogen concentration and oxygen concentration in the mixed gas a detected by the hydrogen / oxygen sensor 31 are higher than the first set value, the second set value (value set lower than the explosion limit).
- the emergency release valve 32 When the above is reached, the emergency release valve 32 is operated (the flow direction of the emergency release valve 32 is switched) to release the mixed gas a.
- the control device 33 operates the diluting gas mixing device 34 (starts the ventilator 36) when the hydrogen concentration and oxygen concentration in the mixed gas a detected by the hydrogen / oxygen sensor 39 exceeds the first set value.
- the flow rate adjustment valve 38 is opened to start the flow rate adjustment), and the emergency release valve 32 when the hydrogen concentration and the oxygen concentration in the mixed gas a detected by the hydrogen / oxygen sensor 39 become equal to or higher than the second set value. May be operated (by switching the flow direction of the emergency release valve 32) to release the mixed gas a.
- the fuel gas supply device 8 detects the hydrogen concentration and the oxygen concentration in the mixed gas a.
- the hydrogen / oxygen sensor 31 or 39
- the dilution gas mixing device 34 for mixing the diluted gas for diluting the hydrogen concentration and oxygen concentration with the mixed gas a
- the hydrogen / oxygen sensor 31 or 39
- the dilution gas mixing device 34 Since the dilution gas mixing device 34 is operated when the hydrogen concentration and the oxygen concentration are equal to or higher than the first set values, and the control device 33 mixes the dilution gas with the mixed gas a, the hydrogen in the mixed gas a Even if hydrogen and oxygen lumps are generated due to liberation of oxygen and oxygen, the hydrogen concentration and oxygen concentration of the mixed gas a are set before the mixed gas a having a high hydrogen concentration and oxygen concentration is supplied to the combustor 2. Greater than or equal to It detects that there can be reduced by diluting the hydrogen concentration and the oxygen concentration of the mixed gas a at a dilution gas. For this reason, it is possible to operate the gas turbine device safely by suppressing the hydrogen concentration and oxygen concentration of the mixed gas a to below the explosion limit.
- the dilution gas mixing device 8 is configured to mix a part of the combustion gas (exhaust gas) c discharged from the gas turbine 1 into the mixed gas a as a dilution gas. Since the combustion gas is effectively used as the dilution gas and nitrogen gas or the like is not required, an efficient and inexpensive gas turbine device can be realized.
- the fuel gas supply device 8 includes the hydrogen / oxygen sensor 31 (or 39) for detecting the hydrogen concentration and the oxygen concentration in the mixed gas a, and the emergency release valve. 32, and a control device 33 that operates the emergency release valve 32 to release the mixed gas a when the hydrogen concentration and the oxygen concentration detected by the hydrogen / oxygen sensor 31 (or 39) are equal to or higher than the second set value. Therefore, when the hydrogen concentration and the oxygen concentration of the mixed gas a increase due to the generation of hydrogen lumps and oxygen lumps by liberation of hydrogen and oxygen in the mixed gas a, the mixed gas a is combusted.
- the fuel gas supply device 8 is arranged on the downstream side of the hydrogen / oxygen sensor 31, and the dilution gas mixing by the dilution gas mixing device 34 and the emergency release valve are performed. Since the mixed gas a is released by 32, the dilution gas mixing device 34 is more reliably downstream than the mixed gas a having a high hydrogen concentration and high oxygen concentration detected by the upstream hydrogen / oxygen sensor 31. It is possible to mix the dilution gas by the above and the discharge of the mixed gas a by the emergency release valve 32.
- the gas compressor 6 is provided with the gas compressor 6 that compresses the mixed gas a and supplies the mixed gas a to the combustor 2, and the fuel gas supply device 8 includes the gas compressor.
- the dilution gas mixing device 34 mixes the dilution gas and the emergency discharge valve 32 releases the mixed gas a.
- the gas mixture 6 having a high hydrogen concentration and oxygen concentration is used as the gas compressor 6.
- the dilution gas is mixed by the dilution gas mixing device 34 and the mixed gas a is discharged by the emergency discharge valve 32. Therefore, the gas turbine device having the gas compressor 6 is surely exploded. Risk can be reduced.
- FIG. 3 is a configuration diagram of a gas turbine apparatus according to Embodiment 3 of the present invention. 3 that are the same as those in FIG. 1 (Embodiment 1) and FIG. 2 (Embodiment 2) are assigned the same reference numerals as in FIGS. 1 and 2, and detailed descriptions thereof are omitted. To do.
- a hydrogen / oxygen sensor is further provided in the fuel gas supply device 8 of the third embodiment. 31, 39, an emergency discharge valve 32, a remixer 41, and a control device 42.
- the remixer 41 is installed in the fuel supply line 9 on the downstream side of the hydrogen / oxygen sensor 31 and the emergency release valve 32, and the mixed gas a generated in the second mixer 16 is stirred and remixed.
- the hydrogen / oxygen sensor 39 is provided in the fuel supply line 9 immediately after the remixer 41 and before entering the gas compressor 6, and detects the hydrogen concentration and oxygen concentration in the mixed gas a.
- the remixer 41 is turned on. Operate to remix gas mixture a.
- the hydrogen concentration and oxygen concentration in the mixed gas a detected by the hydrogen / oxygen sensor 31 are higher than the first set value, the second set value (value set lower than the explosion limit).
- the emergency release valve 32 is operated (the flow direction of the emergency release valve 32 is switched) to release the mixed gas a.
- the control device 42 operates the remixer 41 when the hydrogen concentration and the oxygen concentration in the mixed gas a detected by the hydrogen / oxygen sensor 39 are equal to or higher than the first set value, thereby reusing the mixed gas a.
- the emergency release valve 32 When the hydrogen concentration and the oxygen concentration in the mixed gas a detected by the hydrogen / oxygen sensor 39 are equal to or higher than the second set value, the emergency release valve 32 is operated (the flow direction of the emergency release valve 32 is changed). Alternatively, the mixed gas a may be released.
- the fuel gas supply device 8 includes a hydrogen / oxygen sensor 31 (or 39) for detecting the hydrogen concentration and oxygen concentration in the mixed gas a, and the hydrogen concentration detected by the hydrogen / oxygen sensor 31 (or 39) and Since the control device 42 is configured to operate the remixer 41 and remix the mixed gas a when the oxygen concentration becomes equal to or higher than the first set value, hydrogen and oxygen in the mixed gas a are liberated.
- the hydrogen concentration and oxygen concentration of the mixed gas a before the mixed gas a having a high hydrogen concentration and oxygen concentration is supplied to the combustor 2.
- the first set value By detecting that it is above and mixing the mixed gas a with the remixer 2 before the mixed gas a is supplied to the combustor 2, it is possible to obtain a uniform mixed state again. it can. For this reason, the danger of an explosion is reduced and the safe operation of the gas turbine apparatus becomes possible.
- the remixer 41 is not limited to the case where the control device 42 operates the remixer 41 based on the detection signal of the hydrogen / oxygen sensor 31 (or 39) as described above. Or you may make it operate
- the fuel gas supply device 8 is configured to remix the mixed gas a by the remixer 41 on the downstream side of the hydrogen / oxygen sensor 31.
- the mixed gas a detected by the upstream hydrogen / oxygen sensor 31 can be more reliably remixed by the remixer 41 on the downstream side with respect to the mixed gas a having a high hydrogen concentration and high oxygen concentration.
- the gas compressor 6 is compressed and supplied to the combustor 2 by compressing the mixed gas a
- the fuel gas supply apparatus 8 includes the gas compressor. 6
- the mixed gas a is remixed by the remixer 41, and the mixed gas a by the remixer 41 before the mixed gas a having a high hydrogen concentration and high oxygen concentration flows into the gas compressor 6. Since remixing of “a” is performed, the risk of explosion can be reliably reduced even for the gas turbine apparatus having the gas compressor 6.
- the configuration of the second embodiment may be combined with the configuration of the third embodiment.
- the present invention is not limited to a low-calorie gas-burning gas turbine apparatus, and can be applied to any gas turbine apparatus that uses a mixed gas obtained by mixing three or more kinds of gases as a fuel gas for a combustor.
- the present invention relates to three or more kinds of gases (for example, a single gas such as butane gas or propane gas, or a mixture of a plurality of kinds of gases such as a blast furnace gas or a converter gas). ) Is used as a fuel gas for the combustor. For example, it is applied to a case where a mixed gas mixed with various by-product gases generated at an ironworks is used as the fuel gas for the combustor. It is useful.
- gases for example, a single gas such as butane gas or propane gas, or a mixture of a plurality of kinds of gases such as a blast furnace gas or a converter gas.
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
前記燃料ガス供給装置は複数の混合器を有しており、これらの混合器で3種以上のガスを、比重の軽いものから順に混合して又は比重の重いものから順に混合して混合ガスを生成し、この混合ガスを前記燃料ガスとして前記燃焼器に供給する構成とした特徴とする。
前記燃料ガス供給装置は、
前記混合ガス中の水素濃度及び酸素濃度を検出する水素・酸素センサと、
前記水素濃度及び酸素濃度を希釈するための希釈ガスを前記混合ガスに混合する希釈ガス混合装置と、
前記水素・酸素センサで検出した前記水素濃度及び酸素濃度が設定値以上になったときに前記希釈ガス混合装置を作動させて前記希釈ガスを前記混合ガスに混合させる制御装置と、
を有する構成としたことを特徴とする。
前記希釈ガス混合装置は、前記ガスタービンから排出された燃焼ガスの一部を前記希釈ガスとして前記混合ガスに混合する構成としたことを特徴とする。
前記燃料ガス供給装置は、前記混合ガスを攪拌して再混合する再混合器を有する構成としたことを特徴とする。
前記燃料ガス供給装置は、
前記混合ガス中の水素濃度及び酸素濃度を検出する水素・酸素センサと、
この水素・酸素センサで検出した前記水素濃度及び酸素濃度が設定値以上になったときに前記再混合器を作動させて前記混合ガスを再混合させる制御装置と、
を有する構成としたことを特徴とする。
前記燃料ガス供給装置は、
前記混合ガス中の水素濃度及び酸素濃度を検出する水素・酸素センサと、
緊急放出弁と、
前記水素・酸素センサで検出した前記水素濃度及び酸素濃度が設定値以上になったときに前記緊急放出弁を作動させて前記混合ガスを放出させる制御装置と、
を有する構成としたことを特徴とする。
前記燃料ガス供給装置は、前記水素・酸素センサよりも下流側で、前記希釈ガス混合装置による前記希釈ガスの混合、前記再混合器による前記混合ガスの再混合、又は、前記緊急放出弁による前記混合ガスの放出を行なう構成としたことを特徴とする。
前記混合ガスを圧縮して前記燃焼器へ供給するガス圧縮機を有しており、
前記燃料ガス供給装置は、このガス圧縮機の上流側で、前記希釈ガス混合装置による前記希釈ガスの混合、前記再混合器による前記混合ガスの再混合、又は、前記緊急放出弁による前記混合ガスの放出を行なう構成としたことを特徴とする。
図1は本発明の実施の形態例1に係るガスタービン装置の構成図である。図1に示すように、本実施の形態例1のガスタービン装置はガスタービンと蒸気タービンとを稼動させて発電を行うコンバインド発電装置であり、ガスタービン1と蒸気タービン5と燃焼器2と空気圧縮機3と発電機4とガス圧縮機6と排熱回収ボイラ7と燃料ガス供給装置8とを有している。
図2は本発明の実施の形態例2に係るガスタービン装置の構成図である。なお、図2において図1(実施の形態例1)と同様の部分については図1と同一の符号を付し、重複する詳細な説明は省略する。
図3は本発明の実施の形態例3に係るガスタービン装置の構成図である。なお、図3において図1(実施の形態例1)及び図2(実施の形態例2)と同様の部分については図1及び図2と同一の符号を付し、重複する詳細な説明は省略する。
Claims (8)
- 燃料ガス供給装置から供給される燃料ガスを空気圧縮機から供給される圧縮空気とともに燃焼器で燃焼し、このときに発生する燃焼ガスによってガスタービンを回転駆動する構成のガスタービン装置において、
前記燃料ガス供給装置は複数の混合器を有しており、これらの混合器で3種以上のガスを、比重の軽いものから順に混合して又は比重の重いものから順に混合して混合ガスを生成し、この混合ガスを前記燃料ガスとして前記燃焼器に供給する構成とした特徴とするガスタービン装置。 - 請求項1に記載のガスタービン装置において、
前記燃料ガス供給装置は、
前記混合ガス中の水素濃度及び酸素濃度を検出する水素・酸素センサと、
前記水素濃度及び酸素濃度を希釈するための希釈ガスを前記混合ガスに混合する希釈ガス混合装置と、
前記水素・酸素センサで検出した前記水素濃度及び酸素濃度が設定値以上になったときに前記希釈ガス混合装置を作動させて前記希釈ガスを前記混合ガスに混合させる制御装置と、
を有する構成としたことを特徴とするガスタービン装置。 - 請求項2に記載のガスタービン装置において、
前記希釈ガス混合装置は、前記ガスタービンから排出された燃焼ガスの一部を前記希釈ガスとして前記混合ガスに混合する構成としたことを特徴とするガスタービン装置。 - 請求項1に記載のガスタービン装置において、
前記燃料ガス供給装置は、前記混合ガスを攪拌して再混合する再混合器を有する構成としたことを特徴とするガスタービン装置。 - 請求項4に記載のガスタービン装置において、
前記燃料ガス供給装置は、
前記混合ガス中の水素濃度及び酸素濃度を検出する水素・酸素センサと、
この水素・酸素センサで検出した前記水素濃度及び酸素濃度が設定値以上になったときに前記再混合器を作動させて前記混合ガスを再混合させる制御装置と、
を有する構成としたことを特徴とするガスタービン装置。 - 請求項1に記載のガスタービン装置において、
前記燃料ガス供給装置は、
前記混合ガス中の水素濃度及び酸素濃度を検出する水素・酸素センサと、
緊急放出弁と、
前記水素・酸素センサで検出した前記水素濃度及び酸素濃度が設定値以上になったときに前記緊急放出弁を作動させて前記混合ガスを放出させる制御装置と、
を有する構成としたことを特徴とするガスタービン装置。 - 請求項2,5,6の何れか1項に記載のガスタービン装置において、
前記燃料ガス供給装置は、前記水素・酸素センサよりも下流側で、前記希釈ガス混合装置による前記希釈ガスの混合、前記再混合器による前記混合ガスの再混合、又は、前記緊急放出弁による前記混合ガスの放出を行なう構成としたことを特徴とするガスタービン装置。 - 請求項2~7の何れか1項に記載のガスタービン装置において、
前記混合ガスを圧縮して前記燃焼器へ供給するガス圧縮機を有しており、
前記燃料ガス供給装置は、このガス圧縮機の上流側で、前記希釈ガス混合装置による前記希釈ガスの混合、前記再混合器による前記混合ガスの再混合、又は、前記緊急放出弁による前記混合ガスの放出を行なう構成としたことを特徴とするガスタービン装置。
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020107028985A KR101324900B1 (ko) | 2008-10-01 | 2008-10-01 | 가스 터빈 장치 |
EP08877149.8A EP2330281B1 (en) | 2008-10-01 | 2008-10-01 | Gas turbine device |
KR1020137014303A KR101369102B1 (ko) | 2008-10-01 | 2008-10-01 | 가스 터빈 장치 |
PCT/JP2008/067825 WO2010038290A1 (ja) | 2008-10-01 | 2008-10-01 | ガスタービン装置 |
CN2008801300542A CN102076941B (zh) | 2008-10-01 | 2008-10-01 | 燃气轮机装置 |
US12/999,374 US9097188B2 (en) | 2008-10-01 | 2008-10-01 | Gas turbine device |
KR1020137014304A KR101369116B1 (ko) | 2008-10-01 | 2008-10-01 | 가스 터빈 장치 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/JP2008/067825 WO2010038290A1 (ja) | 2008-10-01 | 2008-10-01 | ガスタービン装置 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2010038290A1 true WO2010038290A1 (ja) | 2010-04-08 |
Family
ID=42073083
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2008/067825 WO2010038290A1 (ja) | 2008-10-01 | 2008-10-01 | ガスタービン装置 |
Country Status (5)
Country | Link |
---|---|
US (1) | US9097188B2 (ja) |
EP (1) | EP2330281B1 (ja) |
KR (3) | KR101324900B1 (ja) |
CN (1) | CN102076941B (ja) |
WO (1) | WO2010038290A1 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2013535604A (ja) * | 2010-07-02 | 2013-09-12 | エクソンモービル アップストリーム リサーチ カンパニー | 低エミッショントリプルサイクル発電システム及び方法 |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009031436A1 (de) * | 2009-07-01 | 2011-01-05 | Uhde Gmbh | Verfahren und Vorrichtung zur Warmhaltung von Koksofenkammern während des Stillstandes eines Abhitzekessels |
US20140250892A1 (en) * | 2011-10-17 | 2014-09-11 | Kawasaki Jukogyo Kabushiki Kaisha | Lean fuel intake gas turbine |
US9778776B2 (en) | 2012-07-30 | 2017-10-03 | Beijing Lenovo Software Ltd. | Method and system for processing data |
JP6099408B2 (ja) * | 2013-01-18 | 2017-03-22 | 三菱日立パワーシステムズ株式会社 | 発電システム、及び発電システムの運転方法 |
JP6134587B2 (ja) * | 2013-06-11 | 2017-05-24 | ヤンマー株式会社 | ガスエンジン |
US20150082800A1 (en) * | 2013-09-25 | 2015-03-26 | Korea Electric Power Corporation | Method for suppressing generation of yellow plum of complex thermal power plant using high thermal capacity gas |
PL3269948T3 (pl) * | 2016-07-15 | 2022-07-18 | Carbon-Clean Technologies Gmbh | Sposób dostosowania mocy elektrowni z turbiną parową i elektrownia z turbiną parową |
NL2021484B1 (nl) * | 2018-08-20 | 2020-04-23 | Micro Turbine Tech B V | Fuel/air supply device |
EP3862549B1 (en) * | 2020-02-05 | 2025-05-07 | General Electric Technology GmbH | Method for operating a power plant, and power plant |
KR102773279B1 (ko) * | 2022-07-11 | 2025-02-27 | 에이치디한국조선해양 주식회사 | 선박 연료 공급 제어 장치 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2954456B2 (ja) | 1993-07-14 | 1999-09-27 | 株式会社日立製作所 | 排気再循環型コンバインドプラント |
JP2003254090A (ja) * | 2002-02-26 | 2003-09-10 | Jfe Steel Kk | 高炉ガスと添加ガスとの混合装置および混合方法 |
JP2004027975A (ja) | 2002-06-26 | 2004-01-29 | Jfe Steel Kk | 副生ガスを用いた発電方法および発電設備 |
JP2004332057A (ja) * | 2003-05-08 | 2004-11-25 | Sumitomo Metal Ind Ltd | 転炉又は真空脱炭炉におけるガス測定装置の異常検出方法 |
JP2007291905A (ja) * | 2006-04-24 | 2007-11-08 | Chugoku Electric Power Co Inc:The | ガス置換方法、ガス置換装置及び燃料ガス置換用ガス |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4761948A (en) * | 1987-04-09 | 1988-08-09 | Solar Turbines Incorporated | Wide range gaseous fuel combustion system for gas turbine engines |
JPH0439392Y2 (ja) * | 1987-12-18 | 1992-09-16 | ||
JPH01286260A (ja) | 1988-05-13 | 1989-11-17 | Fuji Electric Co Ltd | 燃料電池の保護装置 |
JPH083770Y2 (ja) | 1989-08-04 | 1996-01-31 | 株式会社鶴見製作所 | メカニカルシールにおける固定密封環の固定部構造 |
JPH05125958A (ja) | 1991-11-01 | 1993-05-21 | Mitsubishi Heavy Ind Ltd | 液体燃料の供給装置 |
JPH05138308A (ja) | 1991-11-15 | 1993-06-01 | Kawasaki Steel Corp | 金属鋳造薄帯の表面性状改善方法および装置 |
JP2001107743A (ja) * | 1999-10-05 | 2001-04-17 | Mitsubishi Heavy Ind Ltd | ガスタービンシステムおよびそれを備えたコンバインドプラント |
US6397575B2 (en) * | 2000-03-23 | 2002-06-04 | General Electric Company | Apparatus and methods of reheating gas turbine cooling steam and high pressure steam turbine exhaust in a combined cycle power generating system |
KR100785955B1 (ko) * | 2002-10-10 | 2007-12-14 | 엘피피 컴버션, 엘엘씨 | 연소용 액체 연료의 기화 기구 및 사용 방법 |
US7007487B2 (en) * | 2003-07-31 | 2006-03-07 | Mes International, Inc. | Recuperated gas turbine engine system and method employing catalytic combustion |
JP4011572B2 (ja) | 2004-09-10 | 2007-11-21 | カワサキプラントシステムズ株式会社 | ガス改質設備 |
CN101023255B (zh) | 2004-09-29 | 2010-05-05 | 川崎重工业株式会社 | 燃气轮机设备、低热量气体供给设备以及该气体的热量上升的抑制方法 |
EP1645804A1 (de) * | 2004-10-11 | 2006-04-12 | Siemens Aktiengesellschaft | Verfahren zum Betrieb eines Brenners, insbesondere eines Brenners einer Gasturbine, sowie Vorrichtung zur Durchführung des Verfahrens |
BRPI0519804A2 (pt) | 2005-02-18 | 2009-03-17 | Kawasaki Heavy Ind Ltd | método para controlar o valor de gás calorìfico e dispositivo de controle de valor calorìfico de gás |
JP2006233920A (ja) | 2005-02-28 | 2006-09-07 | Mitsubishi Heavy Ind Ltd | 燃料ガスカロリー制御装置及びガスタービンシステム |
JP4563242B2 (ja) * | 2005-04-19 | 2010-10-13 | 三菱重工業株式会社 | 燃料ガスカロリ制御方法及び装置 |
JP4728176B2 (ja) * | 2005-06-24 | 2011-07-20 | 株式会社日立製作所 | バーナ、ガスタービン燃焼器及びバーナの冷却方法 |
JP4642630B2 (ja) * | 2005-10-20 | 2011-03-02 | カワサキプラントシステムズ株式会社 | ガスタービンの制御システムおよび制御方法 |
JP2007113541A (ja) | 2005-10-24 | 2007-05-10 | Kawasaki Plant Systems Ltd | ガスタービン用燃料ガスの減熱設備および減熱方法 |
US7950216B2 (en) | 2007-01-30 | 2011-05-31 | Pratt & Whitney Canada Corp. | Gas turbine engine fuel control system |
-
2008
- 2008-10-01 WO PCT/JP2008/067825 patent/WO2010038290A1/ja active Application Filing
- 2008-10-01 KR KR1020107028985A patent/KR101324900B1/ko active Active
- 2008-10-01 US US12/999,374 patent/US9097188B2/en active Active
- 2008-10-01 KR KR1020137014303A patent/KR101369102B1/ko active Active
- 2008-10-01 EP EP08877149.8A patent/EP2330281B1/en active Active
- 2008-10-01 KR KR1020137014304A patent/KR101369116B1/ko active Active
- 2008-10-01 CN CN2008801300542A patent/CN102076941B/zh active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2954456B2 (ja) | 1993-07-14 | 1999-09-27 | 株式会社日立製作所 | 排気再循環型コンバインドプラント |
JP2003254090A (ja) * | 2002-02-26 | 2003-09-10 | Jfe Steel Kk | 高炉ガスと添加ガスとの混合装置および混合方法 |
JP2004027975A (ja) | 2002-06-26 | 2004-01-29 | Jfe Steel Kk | 副生ガスを用いた発電方法および発電設備 |
JP2004332057A (ja) * | 2003-05-08 | 2004-11-25 | Sumitomo Metal Ind Ltd | 転炉又は真空脱炭炉におけるガス測定装置の異常検出方法 |
JP2007291905A (ja) * | 2006-04-24 | 2007-11-08 | Chugoku Electric Power Co Inc:The | ガス置換方法、ガス置換装置及び燃料ガス置換用ガス |
Non-Patent Citations (1)
Title |
---|
See also references of EP2330281A4 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2013535604A (ja) * | 2010-07-02 | 2013-09-12 | エクソンモービル アップストリーム リサーチ カンパニー | 低エミッショントリプルサイクル発電システム及び方法 |
Also Published As
Publication number | Publication date |
---|---|
CN102076941A (zh) | 2011-05-25 |
KR20110028462A (ko) | 2011-03-18 |
EP2330281B1 (en) | 2015-12-23 |
EP2330281A1 (en) | 2011-06-08 |
US20110167783A1 (en) | 2011-07-14 |
CN102076941B (zh) | 2013-11-06 |
KR20130065740A (ko) | 2013-06-19 |
US9097188B2 (en) | 2015-08-04 |
KR20130065739A (ko) | 2013-06-19 |
EP2330281A4 (en) | 2014-11-05 |
KR101324900B1 (ko) | 2013-11-04 |
KR101369116B1 (ko) | 2014-03-04 |
KR101369102B1 (ko) | 2014-02-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2010038290A1 (ja) | ガスタービン装置 | |
EP2141335B1 (en) | An inlet air heating system for a gas turbine engine | |
EP0785975B1 (en) | Improvements in the combustion and utilisation of fuel gases | |
JP6520309B2 (ja) | 燃焼装置、ガスタービン及び発電装置 | |
JP4898594B2 (ja) | ガスタービン装置 | |
RU2509904C2 (ru) | Способ и устройство для окисления топлива | |
CN100432536C (zh) | 采用催化燃烧的换热气体涡轮发动机系统和方法 | |
JP2012145111A5 (ja) | ||
EP2309189A2 (en) | Low NOx combustor for hydrogen-containing fuel and its operation | |
TWI320071B (ja) | ||
JP2009276053A (ja) | ガスタービンNOxの乾式三元触媒還元法 | |
US20130276433A1 (en) | Lean-fuel gas turbine engine | |
WO2009151073A1 (ja) | 希薄燃料吸入ガスタービンシステム | |
US9500127B2 (en) | Power plant and method for its operation | |
RU2629850C2 (ru) | Система и способ получения водорода | |
JP2018162936A (ja) | 燃焼装置及びガスタービン | |
EP2588809B1 (en) | Method and system for low-emission incineration of low-calorific waste gas | |
JP5200150B2 (ja) | ガスタービン装置 | |
JP5124041B2 (ja) | ガスタービン装置 | |
CN114450521B (zh) | 氧燃料燃烧过程中的火焰控制 | |
JP2005023798A (ja) | 再生サイクルガスタービン及びガスタービンの再生器 | |
JP4795999B2 (ja) | ガスタービン発電システム | |
AU698257B2 (en) | Improvements in the combustion and utilisation of fuel gases | |
WO2014129226A1 (ja) | 希薄燃料吸入ガスタービンの制御方法および制御装置 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 200880130054.2 Country of ref document: CN |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 08877149 Country of ref document: EP Kind code of ref document: A1 |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2008877149 Country of ref document: EP |
|
ENP | Entry into the national phase |
Ref document number: 20107028985 Country of ref document: KR Kind code of ref document: A |
|
WWE | Wipo information: entry into national phase |
Ref document number: 12999374 Country of ref document: US |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
NENP | Non-entry into the national phase |
Ref country code: JP |