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1. 发明专利

JP2010286200A Solar heat collector 审中-公开
标题翻译：太阳能热收集器
公开(公告)号：JP2010286200A
公开(公告)日：2010-12-24
申请号：JP2009141566
申请日：2009-06-12
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： AOYAMA KUNIAKI , INOUE KEI , KOBAYASHI ICHITA
IPC分类号： F24S50/20 , F02C1/05 , F03G6/00 , F24S23/70
CPC分类号： Y02E10/46 , Y02E10/47
摘要： PROBLEM TO BE SOLVED: To provide a solar heat collector which improves light collecting efficiency by moving on the ground to follow the position of the sun and by changing the height of a support pillar which supports a mirror for reflecting the sunlight.
SOLUTION: The solar heat collector 12 is arranged on a mirror arrangement surface set on the ground 8 to collect the sunlight at a predetermined position by reflecting the sunlight on a flat mirror (mirror) 12c. The solar heat collector 12 is composed to be movable along the north-south direction and/or the east-west direction.
COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提供一种太阳能集热器，其通过在地面上移动以跟随太阳的位置并且通过改变支撑用于反射太阳光的反射镜的支撑柱的高度而提高聚光效率。解决方案：太阳能热收集器12布置在设置在地面8上的镜子布置表面上，以通过将太阳光反射在平面镜（反射镜）12c上来收集在预定位置的太阳光。太阳能热收集器12可以沿南北方向和/或东西方向移动。版权所有（C）2011，JPO＆INPIT

2. 发明专利

JP2004101105A Combustor 有权
公开(公告)号：JP2004101105A
公开(公告)日：2004-04-02
申请号：JP2002265281
申请日：2002-09-11
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： OOTA MASATOYO , BANDAI SHIGEMI , AOYAMA KUNIAKI , TANAKA KATSUNORI , NISHIDA KOICHI , AKIZUKI WATARU , KASAI TAKAKUNI , HASHIMURA JUNJI
IPC分类号： F23R3/28
摘要： PROBLEM TO BE SOLVED: To provide a combustor suppressing combustion vibration while making a pilot ratio low.
SOLUTION: Pilot fuel injected from a fuel injection port 21 of a pilot nozzle 2 collides with the internal wall surface of a cone inner peripheral taper part 41 of a pilot cone 4. The collision position of the pilot fuel from the fuel injection port 21 at this time is located in a range from the intermediate part to the downstream tip in the cone inner peripheral taper part 41.
COPYRIGHT: (C)2004,JPO

3. 发明专利

JP2004101071A Combustor 有权
公开(公告)号：JP2004101071A
公开(公告)日：2004-04-02
申请号：JP2002263663
申请日：2002-09-10
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： OOTA MASATOYO , BANDAI SHIGEMI , AOYAMA KUNIAKI , TANAKA KATSUNORI , AKAMATSU SHINJI , NAKAJIMA HISANARI , TACHIBANA TERUYA
IPC分类号： F23R3/18 , F02C7/232 , F23D14/02 , F23D14/74 , F23R3/28
摘要： PROBLEM TO BE SOLVED: To provide a combustor preventing the occurrence of a stagnant region at the outlet of a main combustor while making a flame stabilizing low speed region larger and more positive.
SOLUTION: A cone internal taper part 41 of a pilot cone 4a is provided with a collar 42 extending from the downstream tip toward the vicinity of the downstream tip of the main combustor 5. The flame stabilizing low speed region is formed downstream of the collar 42, and air between the collar 42 and a collar 44 of a cylinder 43 at the outer periphery of the cone internal taper part 41, flows in the form of a film to the downstream tip of the main combustor 5 to improve the flame stability of the flame stabilizing low speed region.
COPYRIGHT: (C)2004,JPO

4. 发明专利

JPH10280913A EXHAUST GAS RECOMBUSTION COMBINED CYCLE PLANT 失效
公开(公告)号：JPH10280913A
公开(公告)日：1998-10-20
申请号：JP8938597
申请日：1997-04-08
申请人： MITSUBISHI HEAVY IND LTD
发明人： BANDAI SHIGEMI , OOTA MASATOYO , AOYAMA KUNIAKI
IPC分类号： F01K23/10 , F02C6/18 , F02C7/22
摘要： PROBLEM TO BE SOLVED: To obtain a clean gasificated fuel without using an expensive clean up device by separating a raw fuel including a heavy distillate to a light fuel and a residual including the heavy distillate by a distilling plant, making the light fuel to a fuel for a. turbine by gasificating and burning the residual in an exhaust gas boiler. SOLUTION: At the operation time of a plant, in an exhaust gas boiler 111, an overheated vapour is generated by a gas turbine exhaust gas through an exhaust pipe 56 and this overheated vapour is led to a vaporizer 105 and distilling plant 101 through the vapour pipe 54 branched from a main vapour pipe 57 to a steam turbine 114 and by heating a coarse fuel by a steam in the steam pipe 54 at the distilling plant 101, it is separated to the light fuel and the residual including the heavy distillate and the obtained light fuel is sent to a condenser 102 and after cooling here, supplied to the combustor 106 of the gas turbine 108 through a fuel tank 103. While, the residual is supplied to the exhaust gas boiler 111 through a fuel tank 109 and pump 110 and burned and the vapour is generated.

5. 发明专利

JPH1047610A CATALYST COMBUSTOR OF GAS TURBINE 失效
公开(公告)号：JPH1047610A
公开(公告)日：1998-02-20
申请号：JP20813196
申请日：1996-08-07
申请人： MITSUBISHI HEAVY IND LTD
发明人： NAGAYASU HIROTSUGU , UEJIMA NAOYUKI , MORI KAZUTAKA , BANDAI SHIGEMI , AOYAMA KUNIAKI , NISHIDA KOICHI
IPC分类号： F23C99/00 , B01J23/34 , F23C13/00 , F23C11/00
摘要： PROBLEM TO BE SOLVED: To make a catalyst have a long lifetime by constructing a catalyst combustion portion of a catalyst combustor such that a catalyst layer containing palladium is arranged as a front part thereof and a catalyst layer containing manganese and having a magnetoplumbite structure is arranged as a rear part thereof. SOLUTION: A catalyst layer 1 containing palladium which is excellent in ignitability from a low temperature is arranged at a gas inlet side as a front part of a catalyst combustion portion thus enabling a start of a catalytic action from a discharge gas temperature of a compressor. A catalyst layer 2 containing manganese which has a resistance against lowering of its catalytic activity and having a megnetoplumbite structure is arranged at a gas outlet as a rear part of the catalyst combustion portion. A mixture gas of air and fuel discharged from a compressor is fed to the catalyst layer 1 where a contact oxidation reaction proceeds. Corresponding to the progress of the reaction, the catalyst temperature and the gas temperature are elevated. The heated gas is fed to the catalyst layer 2 where the reaction is further proceeded to a temperature which enables a gas phase combustion.

6. 发明专利

JPH07166889A SUPPLY METHOD FOR FUEL TO GAS TURBINE COMBUSTOR 失效
公开(公告)号：JPH07166889A
公开(公告)日：1995-06-27
申请号：JP31786893
申请日：1993-12-17
申请人： MITSUBISHI HEAVY IND LTD
发明人： BANDAI SHIGEMI , SATO NOBUO , AOYAMA KUNIAKI
IPC分类号： F02C7/22 , F02C9/28 , F23R3/28
摘要： PURPOSE:To provide a supply method for fuel to a gas turbine combustor formed so as to prevent supply of fuel from being unstable even at low load time. CONSTITUTION:Air from a compressor 101 and fuel via a flow regulating valve 104 are supplied to a combustor 102, to perform combustion. Combustion gas in the combustor 102 is guided to a turbine 103. An air bypass pipe line 106, guiding air from an air supply system from the compressor 101 to a fuel supply system through an air bypass valve 105, is provided. When the gas turbine is low loaded to decrease a fuel supply differential pressure lower than an air supply differential pressure, air is supplied into fuel from the air bypass pipe line 106, and by preventing the fuel supply differential pressure from decreasing equal to or less than the air supply differential pressure, combustion at the time of low load it stabilized.

7. 发明专利

JPH0544927A INNER CYLINDER OF GAS TURBINE COMBUSTOR 失效
公开(公告)号：JPH0544927A
公开(公告)日：1993-02-23
申请号：JP20283491
申请日：1991-08-13
申请人： MITSUBISHI HEAVY IND LTD
发明人： TANIMURA SATOSHI , UCHIMI ISAMU , AOYAMA KUNIAKI , TANAKA KATSUNORI , BANDAI SHIGEMI
IPC分类号： F02C7/18 , F23R3/06 , F23R3/42
摘要： PURPOSE:To carry out efficiently cooling of an inner cylinder of a gas turbine combustor with a small amount of air. CONSTITUTION:An inner cylinder of a gas turbine combustor has a plurality of airstream grooves 1 provided inside a wall of the inner cylinder and running in the same direction as a combustion gas flowing direction, and air holes 4 and 5 provided on both inner and outer surfaces of the wall and communicated with the airstream grooves 1. In this instance, the air holes 4 and 5 have a larger area than a cross sectional area of the air-stream grooves 1 with which it is communicated. Further, a plurality of cooling fins are provided in an outer surface of the wall and running in the same direction as the combustion gas flowing direction.

8. 发明专利

JPH04159423A GAS TURBINE AND CHANGE-OVER METHOD OF GAS TURBINE COMBUSTOR 失效
公开(公告)号：JPH04159423A
公开(公告)日：1992-06-02
申请号：JP28533490
申请日：1990-10-23
申请人： MITSUBISHI HEAVY IND LTD
发明人： AOYAMA KUNIAKI
IPC分类号： F02C3/14 , F02C7/26
摘要： PURPOSE:To enable start control step by step in the stable operation area at the time of change-over with a main combustor by connecting the main combustor to a plural number of combustors for start in parallel between a compressor and a turbine, and controlling a flow amount control valve which is provided in each pipe. CONSTITUTION:A gas turbine is provided with a main combustor 3 and a plural number of combustors for start 8a, 8b,..., which are connected in parallel by a group of pipes 11 between a compressor 1 and a turbine 5. That is, the group of pipes 11 consist of a main pipe 12 which connects the compressor 1, a main combustor 2, and the turbine 5 and a plural number of crossover pipes 10a, 10b, 10c,... which are connected to the main pipe 12 in parallel. The main pipe 12 is provided with an air control valve 2 and a gas control valve 4. On the other hand, each crossover pipe 10a,... is provided with start control valves 9a, 9b,... upstream of the combustors for start 8a,.... At the time of change-over between the combustors for start 8a,... and the main combustor 3, each start control valve 9a,' is operated from open to close or from close to open sequentially.

9. 发明专利

JPS63281767A PRODUCTION OF LAMINATED HEAT RESISTANT ALLOY PLATE 失效
公开(公告)号：JPS63281767A
公开(公告)日：1988-11-18
申请号：JP11452887
申请日：1987-05-13
申请人： MITSUBISHI HEAVY IND LTD , OSAKA YAKIN KOGYO KK
发明人： TSUJI ICHIRO , MAEKAWA ATSUSHI , MOCHIZUKI YOSHIHIRO , AOYAMA KUNIAKI , TERAUCHI HACHIRO
IPC分类号： B23K20/00 , B23K1/00 , B23K1/008 , B23K1/19 , B23K31/02
摘要： PURPOSE:To surely form a good joining part by superposing an upper plate via a Ni brazing filler metal by forming numerous fine grooves on the Ni alloy plate in the specified thickness and executing pressurizing and heat treatment under the specified conditions by facing the groove downwards. CONSTITUTION:Numerous fine grooves C are formed at fixed intervals on the Ni alloy plate 4 in 0.5-5.0mm thickness and the upper plate 5 having the same or different material as or from that of this fine grooved plate is super posed so as to cover the groove C via a Ni brazing filler metal. For the Ni brazing filler metal an acrylic resin is blended at about 10:1wt.% with the powder of a Ni solder BNi-2, etc., and solidified in a sheet shape is used. The uniform loading load >=30g/cm is exerted on the fine grooved plate 4 by divid ing the load area into by plural blocks and it is subjected to heat treatment for 5-60min at 1,000+ or -20 deg.C under inert atmosphere or vacuum, 15-60min at 1,050-1,150 deg.C thereafter and further >=2hr at 1,060-1,140 deg.C. On completion of the heat treatment it is left for cooling to about 900 deg.C inside heating chamber, then rapidly cooled under reducing gas to about 200 deg.C to make at

10. 发明专利

JPS6196333A Gas turbine combustor bypass valve controlling method 失效
标题翻译：气体涡轮机旁通阀控制方法
公开(公告)号：JPS6196333A
公开(公告)日：1986-05-15
申请号：JP21888684
申请日：1984-10-18
申请人： Mitsubishi Heavy Ind Ltd
发明人： FUKUE ICHIRO , AOYAMA KUNIAKI
IPC分类号： F02C9/18 , F23R3/26 , F23R3/42
CPC分类号： F23R3/26
摘要： PURPOSE:To contrive to decrease NOx producing as least as possible and perform the stable combustion by a method wherein an air pressure in the casing of a combustor and a generator output are measured and calculated, then a fuel-air ratio at the burning part in the gas turbine combustor is controlled. CONSTITUTION:The air pressure P2 in the casing of a gas turbine combustor and a generator output Lgen are measured. A factor F(P2) is calculated based on the air pressure P2. In a calculating device 17, alpha=Lgen/F(P2) is calculated based on the air pressure P2 and the generator output Lgen. In a factor setting device 18, a bypass valve open degree setting signal CSO is set for the alpha calculated by the calculating device 17. The bypass valve open degree is controlled by the signal CSO.
摘要翻译：目的：通过测量和计算燃烧器壳体和发电机输出中的空气压力的方法，尽可能地减少NOx产生并进行稳定燃烧，然后在燃烧部分的燃料部分的燃料 - 空气比控制燃气轮机燃烧器。构成：测量燃气轮机燃烧室和发电机输出Lgen的壳体内的气压P2。基于空气压力P2计算因子F（P2）。在计算装置17中，基于空气压力P2和发电机输出Lgen计算α= Lgen / F（P2）。在因数设定装置18中，由计算装置17计算的α设定旁通阀开度设定信号CSO。旁通阀开度由信号CSO控制。

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