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    • 13. 发明申请
    • HEAT-RECOVERY GAS TURBINE ROTOR
    • 热回收气体涡轮转子
    • WO1997019256A1
    • 1997-05-29
    • PCT/JP1996003416
    • 1996-11-21
    • MITSUBISHI JUKOGYO KABUSHIKI KAISHASUENAGA, KiyoshiKASAI, Yoshikuni
    • MITSUBISHI JUKOGYO KABUSHIKI KAISHA
    • F01D05/08
    • F01D5/084F01D5/085F05D2260/205F05D2260/2322
    • A heat-recovery gas turbine rotor (5) having multi-stage moving blades designed to be mounted on each disc (12) comprising inside cavities (9) and outside cavities (8) that are provided between respective discs (12), blade cooling paths (6) for respective moving blades except the rear-most stage moving blade, a cooled steam supply path (13) provided between a rearward portion of the rear-most stage moving blade and the front edge portion of the front-most stage moving blade, a branch path (16) provided at the front-most stage disc portion (12) in such a manner as to communicate with the cooled steam supply path (13) at the proximal end and be branched at the distal end thereof to thereby communicate with one of the blade cooling paths (6) at one of the branches and with the outside cavities (8) at the other, a blade return path (17) designed to communicate with the other blade cooling path (6) at the proximal end thereof and with the inside cavities (9) at the distal end thereof, a cavity connecting path (20) for establishing a connection between the respective inside cavities (9), a return path (11) extending from the inside cavity (9) of the rear-most stage moving blade along the cooled steam supply path (13), blade connecting paths (18) each provided on each disc portion except the front-most and rear-most stage discs for establishing a communication between the blade cooling paths (6) and the outside cavities (8), and an inter-cavity path (19) for connecting the rear-most stage outside cavity (8) to inside cavities (9).
    • 一种具有设计成安装在每个盘(12)上的多级活动叶片的热回收燃气涡轮机转子(5),其包括设置在各个盘(12)之间的内腔(9)和外腔(8),叶片冷却 用于除最后级动叶片之外的各个动叶片的路径(6),设置在最后级动叶片的后部和最前级移动的前缘部之间的冷却蒸汽供给路径(13) 叶片,设置在最前级盘部分(12)处的分支路径(16),以便在近端与冷却的蒸汽供应路径(13)连通并且在其远端处分支,从而 在一个分支处的叶片冷却路径(6)中的另一个与另一个外部空腔(8)连通,叶片返回路径(17)被设计成在近端处与另一个叶片冷却路径(6)连通 端部,并且在其远端处具有内腔(9),具有气穴 连接路径(20),用于在相应的内腔(9)之间建立连接;从最后级动叶片的内腔(9)沿着冷却的蒸汽供应路径(13)延伸的返回路径(11) ,每个设置在每个盘部分之外的刀片连接路径(18),除了最前面和最后级的盘之间,用于建立刀片冷却路径(6)和外部腔(8)之间的连通,以及腔间路径 (19),用于将最后级的外腔(8)连接到内腔(9)。
    • 15. 发明申请
    • EXCHANGING DEVICE FOR COMBUSTOR
    • 燃烧器交换装置
    • WO1997014529A1
    • 1997-04-24
    • PCT/JP1996003030
    • 1996-10-18
    • MITSUBISHI JUKOGYO KABUSHIKI KAISHASHIMOYAMA, HiroshiTSUNEWAKI, HiroshiYASHIKI, TadaoSATOH, Yoshichika
    • MITSUBISHI JUKOGYO KABUSHIKI KAISHA
    • B23P19/04
    • F23R3/60F01D25/285F05D2230/60F05D2230/70
    • Combustors (b) provided centrally of a gas turbine body (g) in a radial manner are held in such a manner that a hand (7) is supported through a centering slide (6), which vertically moves in a diametrical direction (y) of the combustors (b), on a drawing slide (5), which is supported through a vertical rotating shaft (3) directed ( alpha ) toward a central axis of the gas turbine body (g) and a lateral rotating shaft (4) about a radial axis ( beta ) of the gas turbine body (g) on a truck (2) adapted to revolve ( theta ) around the combustors (b) through a rail (1) mounted to outer peripheries of the combustors (b) in a ring-like manner and which moves in an axial direction (z) of the radially arranged combustors (b). Also, a drawing slide (103) adapted to advance and retreat in the axial direction of the combustors (b) is supported on the truck (2) adapted to move along the rail (1) provided on the outer peripheries of the radially arranged combustors (b) in a ring-like manner, an expansion slide (104) adapted to expand and contract in the axial direction of the combustors (b) is supported by the drawing slide (103), and a hand (5) adapted for holding the combustor (b) is provided on a tip end of the expansion slide (104). Accordingly, a combustor replacing operation is mechanized to replace the combustor at a time without the need of manpower and subdividing the combustor into sections, so that a term of work in the combustor replacing operation is sharply shortened and manpower is saved. Also, safety and accuracy in the combustor replacing operation are improved, so that damages to a combustor and a gas turbine body are eliminated and cost and a term of work for repair are made unnecessary.
    • 以径向方式设置在燃气轮机体(g)中央的燃烧器(b)以使得手(7)通过沿直径方向(y)垂直移动的定心滑块(6)支撑的方式被保持, 通过朝向燃气轮机体(g)的中心轴指向(α)的垂直旋转轴(3)支撑的牵引滑块(5)和侧旋转轴(4)上的燃烧器(b) 围绕适于通过安装在燃烧器(b)的外周的轨道(1)围绕燃烧器(b)旋转(θ)的卡车(2)上的燃气涡轮机体(g)的径向轴线(β) 环状,并且在径向布置的燃烧器(b)的轴向方向(z)上移动。 而且,适于沿着燃烧器(b)的轴向前进和后退的牵引滑动件(103)被支撑在所述卡车(2)上,适于沿设置在径向布置的燃烧器的外周上的轨道(1)移动 (b)以环状的方式,适于在燃烧器(b)的轴向方向膨胀和收缩的膨胀滑块(104)由牵引滑动件(103)支撑,以及适于保持 燃烧器(b)设置在膨胀滑块(104)的末端。 因此,燃烧器更换动作被机械化以一次更换燃烧器,而不需要人力并将燃烧器再分成多个部分,从而可以大大缩短燃烧器更换操作中的工作时间并节省人力。 此外,燃烧器更换运转的安全性和精度得到改善,从而消除了对燃烧器和燃气轮机体的损坏,并且不需要成本和修理工作。
    • 17. 发明申请
    • METHOD FOR PRODUCING SUPERHEAVY OIL EMULSION FUEL
    • 生产超级油乳化燃料的方法
    • WO1996038519A1
    • 1996-12-05
    • PCT/JP1996001431
    • 1996-05-27
    • KAO CORPORATIONMITSUBISHI JUKOGYO KABUSHIKI KAISHAMORIYAMA, NoboruHIRAKI, AkioICHINOSE, ToshimitsuSAKAMOTO, Koichi
    • KAO CORPORATIONMITSUBISHI JUKOGYO KABUSHIKI KAISHA
    • C10L01/32
    • C10L1/328
    • The method for producing a superheavy oil emulsion fuel includes the steps of (a) adding to a superheavy oil 0.1 to 0.6 parts by weight of a nonionic surfactant having an HLB (hydrophilic-lipophilic balance) of 13 to 19, based on 100 parts by weight of the superheavy oil, and water, to prepare a homogeneous liquid mixture; and (b) mechanically mixing the homogeneous liquid mixture with a high shearing stress, to produce a superheavy oil emulsion fuel having a particle size distribution. In this method, a 10 %-cumulative particle size is from 1.5 to 8 mu m, a 50 %-cumulative particle size is from 11 to 30 mu m, and a 90 %-cumulative particle size is from 25 to 150 mu m, and coarse particles having particle sizes of 150 mu m or more occupy 3 % by weight or less in the entire emulsion fuel, and the concentration of the superheavy oil is from 76.5 to 82.0 % by weight.
    • 制造超重油乳液燃料的方法包括以下步骤:(a)将100重量份以上的100重量份添加至超重油0.1〜0.6重量份的HLB(亲水亲油平衡)为13〜19的非离子表面活性剂 重量的超重油和水,以制备均匀的液体混合物; 和(b)机械混合均匀的液体混合物与高剪切应力,以产生具有粒度分布的超重油乳化燃料。 在该方法中,10%的累积粒径为1.5〜8μm,50%的累积粒径为11〜30μm,90%的累积粒径为25〜150μm, 在整个乳化燃料中,粒径为150μm以上的粗粒子占3重量%以下,超重油的浓度为76.5〜82.0重量%。