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    • 23. 发明专利
    • CATALYTIC BURNER
    • JPH0252931A
    • 1990-02-22
    • JP20279088
    • 1988-08-16
    • TOKYO ELECTRIC POWER COTOSHIBA CORP
    • TANEMURA KATSUHEIOGOSHI AKIOTOMINAGA HITOSHIHANDA SUSUMUYAMANAKA CHIKAUFURUYA TOMIAKIHAYATA TERUNOBUHIZUKA JUNJI
    • F02C7/00F23D14/18F23R3/40
    • PURPOSE:To enable the replacement time of a catalyst assembly to be easily found, by providing a branched flow path which is connected to a vapor phase combustion chamber formed in the downstream of the catalyst assembly and which is packed with an unburnt detecting catalyst assembly, and by providing a temperature-rise detecting means for checking a catalytic reaction in the branched flow path. CONSTITUTION:Fuel 2 fed out of a fuel feeding nozzle 1 is mixed with air for combustion to be preburnt, and after the temperature of the fuel-air mixture is elevated up to a level of the action temperature of a catalyst assembly 10, said fuel-air mixture is mixed with fuel fed out of fuel feeding nozzles 9 to be converted into a fuel-air mixture gas and flows into the catalyst assembly 10. When a catalytic reaction is incomplete owing to deterioration of the catalyst assembly 10, the fuel gas discharged from the catalyst assembly 10 contains much of unburnt fuel, but such unburnt fuel is further subjected to catalytic combustion in a branched flow path 13 by a catalyst assembly 14 for unburnt fuel detection to elevate its temperature. In this case, a difference in a temperature is caused between thermocouples 16 and 17 adapted at the foe and aft parts of the detecting catalyst assembly 14, and a temperature rise is detected. The degree of deterioration of the catalyst assembly 10 is estimated on the basis of the degree of a temperature rise between the thermocouples 16 and 17, thereby enabling the replacement time of the catalyst assembly 10 to be found.
    • 25. 发明专利
    • GAS TURBINE COMBUSTOR
    • JPS62218727A
    • 1987-09-26
    • JP5959486
    • 1986-03-19
    • TOKYO ELECTRIC POWER COTOSHIBA CORP
    • ITO MASAMICHIOGOSHI AKIOSHIZUKAWA KENJIROUHAYATA TERUNOBUFURUYA TOMIAKIYAMANAKA CHIKAUHIZUKA JUNJI
    • F23R3/40
    • PURPOSE:To suppress an abnormal increase in temperature of a catalyst, enable a long life of the catalyst, reduce a pressure loss within a catalyst charging area and improve an efficiency of combustion by a method wherein a temperature of the catalyst charging area and a ratio in volume of fuel gas and air (F/A) are controlled to each other. CONSTITUTION:Fuel and air are injected from a fuel nozzle 11 and an air injection port into an area A indicated by a dotted line in compliance with a set condition of combustion gas within a gas turbine nozzle 6 so as to form first mixture of desired mixing ratio (F/A). A catalyst charging area B filled with a combustion catalyst 13 is arranged at a rear stage of the area A and a part of the first mixture is ignited with catalyst. The rear stage is provided with an area C for supplying a desired amount of fuel from a fuel nozzle 11a to the flowing-out gas containing unburnt material and igniting the mixture. The catalyst charging area B is provided with means 14 for sensing catalyst temperature and means 15 for adjusting air volume operating in cooperation with the sensing means 14. Since the catalyst temperature and F/A are controlled to each other, an abnormal high temperature of the catalyst can be suppressed.
    • 26. 发明专利
    • Gas turbine combustor
    • 气体涡轮搅拌机
    • JPS59108829A
    • 1984-06-23
    • JP21709682
    • 1982-12-13
    • Toshiba Corp
    • YAMANAKA CHIKAUFURUYA TOMIAKIHAYATA TERUNOBUHIZUKA JIYUNJI
    • F02C9/34F02C9/28F23R3/34F23R3/40
    • F23R3/346F23R3/40
    • PURPOSE:To reduce NOx and improve efficiency of combustion by detecting outflow temperature at a medium outlet to control air fuel ratio according to said temperature while regulating fuel supply downstream of the medium according to the air fuel ratio. CONSTITUTION:Outflow temperature at a medium outlet is detected by a thermometer 9. When said temperature is lower than fire point of thin fuel, an electromagnetic 10 for supplying fuel to a portion downstream of the medium is closed to reduce fuel supply from said portion and increase and air fuel raio in mixture supplied from a portion upstream of the medium. And when the temperature detected by the thermometer 19 exceeds the heat resisting temperature of the medium, said operation is reversely carried out. Thus, nitrogen oxide is reduced to improve the efficiency of combustion.
    • 目的:通过根据所述温度检测介质出口处的出口温度,根据空气燃料比调节介质下游的燃料供应,来减少NOx并提高燃烧效率。 构成:通过温度计9检测介质出口处的流出温度。当所述温度低于薄燃料的燃点时,用于向介质下游部分供应燃料的电磁体10被关闭以减少从所述部分的燃料供应, 从介质上游部分提供的混合物中的增加和空气燃料。 并且当温度计19检测到的温度超过介质的耐热温度时,反向进行操作。 因此,减少氮氧化物以提高燃烧效率。
    • 27. 发明专利
    • Combustion catalyst for gas turbine
    • 燃气涡轮机燃烧催化剂
    • JPS5962344A
    • 1984-04-09
    • JP16986982
    • 1982-09-30
    • Toshiba Corp
    • HAYATA TERUNOBUFURUYA TOMIAKIYAMANAKA CHIKAUHIZUKA JIYUNJI
    • B01J23/63B01J23/56F23R3/40
    • PURPOSE:To develop a combustion catalyst for a gas turbine having an excellent low temp. ignition characteristic and heat resistance by providing a gamma- alumina coating layer on a heat resistant carrier and incorporating catalyst particles of noble metals in said coating layer. CONSTITUTION:A gamma-alumina layer 2 as an active carrier is coated on a heat resistant carrier 1 of cordierite, mullite, etc. Pd and Ce are added and mixed in the form of chloride or nitrate to and with the alumina coating compsn. consisting of gamma-alumina, and the mixture is coated on the surface of the carrier 1 by a dipping method or the like. The compsn. is then dried at an ordinary temp. and is then calcined at about 650 deg.C. Pd is added as a metallic catalyst 3 at >=4g/l with respect to the entire volume of the catalyst, and Ce is added at 1-10wt% ratio based on the weight of the alumina. Such catalyst is ignitable at a low temp. of about 300 deg.C, and retains the original high activity with high temp. waste combustion gas of 800-1,500 deg.C, whereby the catalyst for combustion for a gas turbine having a long service life is obtd.
    • 目的:开发具有优良低温燃气轮机的燃烧催化剂。 点火特性和耐热性,在耐热载体上提供γ-氧化铝涂层,并在所述涂层中加入贵金属催化剂颗粒。 构成:将作为活性载体的γ-氧化铝层2涂覆在堇青石,莫来石等的耐热载体1上。将Pd和Ce以氯化物或硝酸盐的形式加入并与氧化铝涂层组合物混合。 由γ-氧化铝组成,并且通过浸渍方法等将该混合物涂覆在载体1的表面上。 compsn。 然后在普通温度下干燥。 然后在约650℃煅烧。 相对于催化剂的整个体积,以相对于催化剂的总体积为“= 4g / l”的金属催化剂3添加Pd,以氧化铝的重量比为1-10重量%添加Ce。 这种催化剂在低温下是可点燃的。 约300摄氏度,并保持原有的高活性高温。 800〜1500℃的废燃烧气体,具有使用寿命长的燃气轮机的燃烧用催化剂。
    • 29. 发明专利
    • Gas turbine combustor
    • 气体涡轮搅拌机
    • JPS5946423A
    • 1984-03-15
    • JP15593682
    • 1982-09-09
    • Toshiba Corp
    • YAMANAKA CHIKAUFURUYA TOMIAKIHAYATA TERUNOBUHIZUKA JIYUNJI
    • F23R3/16F23R3/34F23R3/40
    • F23R3/40
    • PURPOSE:To provide the titled device with an capability of maintaining a preset low ignition temperature, by arranging a group of columns transversely across a gaseous mixture stream between catalysts of honeycomb structure. CONSTITUTION:A visible radiation ray emitted between an upstream and a downstream sections can be shielded by a group of columns arranged in a zigzag manner between two catalysts of honeycomb structure. Moreover, a gaseous mixture is caused to change its flowing direction upon its collision with columns, resulting in bringing about a further mixing action. As a result, it is relatively easy to control the flow velocity of gaseous mixture at an even level after passed across the group of columns. The diameter, number and installation pitches etc., of columns may be determined with a basis on the magnitude of pressure drop required with an arrangement 8. The replacement of arrangements 8 can be performed conveniently by premounting the group of columns as a unit upon a cylinder which can be inserted into the inner diameter of combustion.
    • 目的:通过在蜂窝状结构的催化剂之间横跨气体混合物流布置一组柱,以提供具有保持预设低点火温度的标题装置。 构成:在上游和下游部分之间发射的可见辐射线可以通过在两个蜂窝结构催化剂之间以之字形方式布置的一组柱体来屏蔽。 此外,气体混合物在与塔碰撞时使其流动方向发生变化,导致进一步的混合作用。 结果,在穿过该组柱之后,将气体混合物的流速控制在均匀的水平是比较容易的。 列的直径,数量和安装间距等可以基于布置8所需的压降幅度来确定。布置8的替换可以通过将一组列作为一个单元预先安装在一个 可插入燃烧内径的气缸。