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    • 5. 发明专利
    • WATER JET PEENING METHOD UNDER WATER
    • JPH0679626A
    • 1994-03-22
    • JP23183392
    • 1992-08-31
    • BABCOCK HITACHI KKHITACHI LTD
    • OSHIMA RYOICHIROKIKUCHI KINYASATOU KAZUNORISHINDOU TAKENORIKUROSAWA KOICHI
    • B24C1/10
    • PURPOSE:To reduce the residual stress of a material to be worked by selecting the optimal water temperature for generating the cavitation appropriate for water jet peening. CONSTITUTION:The high pressure water 2 at 15-70 deg.C is jetted for collision by a high pressure from a nozzle 1 to an objective material 6 of construction of an underwater structure 5 in the ambient water 4 at 15-70 deg.C. This high pressure water 2 as a highspeed water jet with powerful cavitation collides with the objective material 6 of construction, at this stage, a huge number of cavitation bubbles are broken on the surface of the objective material 6 of construction and near by to generate a lot of impact pressure pulses. Crystal grains of the surface of the objective material 6 of construction is plastically deformed so as to be collapsed by this impact pressure, and the condition of residual stress of the objective material 6 of construction is improved from the tensile direction to the compressive direction. With this work, one of three elements (sensitization of material, corrosive environment, and stress) essential for the generation of stress corrosion cracking is eliminated.
    • 7. 发明专利
    • Ceramic stationary blade support structure
    • 陶瓷静态刀片支撑结构
    • JPS6189909A
    • 1986-05-08
    • JP21139284
    • 1984-10-11
    • Central Res Inst Of Electric Power IndHitachi Ltd
    • ABE TOSHIOISHIKAWA HIROSHIHISAMATSU NOBORUMIYATA HIROSHIIIJIMA SHIROOSHIMA RYOICHIRO
    • F01D9/02F01D5/28
    • F01D5/284
    • PURPOSE:To prevent a ceramic liner from being broken by configurating a side wall in such a way that members in a form of a letter 'L' are fitted in grooves in a form of a letter 'U' of the liner arranged to a stationary blade. CONSTITUTION:Grooves 21 and 22 in a form of a letter 'U' are cut on both outside surfaces of ceramic liners 4 arranged outside a ceramic blade 1, and one end of members in a form of a letter 'L' 6 and 7 which are fitted in the grooves 21 and 22, is fastened to a side wall 2. And packing 23, 24, 27 and 28 are installed on the outside of the ceramic liners 4. This configuration enables the ceramic liners to be elastically supported allowing the thermal expansion to be absorbed, resultantly this enables the strength reliability to be augmented.
    • 目的:为了防止通过配置侧壁来破坏陶瓷衬垫,使得将字母“L”形式的构件安装在布置成静止的衬垫的字母“U”形式的凹槽中 刀。 构成:在陶瓷刀片1外部布置的陶瓷衬里4的两个外表面上切割有字母“U”形式的凹槽21和22,并且以“L”6和7形式的构件的一端切割 安装在凹槽21和22中,被紧固到侧壁2.并且衬垫23,24,27和28安装在陶瓷衬垫4的外侧。这种构造使得陶瓷衬垫能够弹性地支撑,从而允许热 膨胀被吸收,从而可以增强强度的可靠性。
    • 8. 发明专利
    • Method of starting gas turbine plant and device therefor
    • 启动气体涡轮机的方法及其装置
    • JPS61142335A
    • 1986-06-30
    • JP26278284
    • 1984-12-14
    • Hitachi Ltd
    • IIZUKA NOBUYUKIKUNO KATSUKUNIOSHIMA RYOICHIROWADA KATSUOHIROSE FUMIYUKIKURODA MICHIOUCHIYAMA YOSHIHIROISHIBASHI YOJISATO ISAOINOSE HIROSHI
    • F01K23/10F02C7/26F02C9/18F02C9/28F02C9/52F23R3/26F23R3/34
    • F23R3/26F02C7/26F02C9/18F05D2270/31F23R3/34Y02E20/16
    • PURPOSE: To facilitate the ignition of secondary fuel in a gas turbine provided with a burner utilizing a two-stage combustion system, by bleeding compressed air after initiation of combustion of secondary fuel upon starting, and by initiating the combustion of secondary air in such a condition that the amount of air flowing into the burner is reduced.
      CONSTITUTION: Upon starting of a gas turbine 2 a compressor 1 is at first driven with the use of an auxiliary prime-mover, and when the rotational speed of the turbine reaches a certain value, a fuel adjusting valve 21 is controlled to jet primary fuel from a primary fuel nozzle 19 so that the jetted fuel is ignited. With this arrangement, the gas turbine 2 enters into its self-sustaining operation. When the rotational speed of the gas turbine 2 reaches a predetermined value, a bleed valve 33 is opened to relief air in the compressor 1 to the atmosphere so that the amount of air flowing into a burner 3 may be reduced. Under this bleeding operation a fuel adjusting valve 22 is controlled to feed secondary fuel from a secondary fuel supply port 13 in a step-like manner while the primary fuel is decreased in a step-like manner, and therefore, the secondary fuel is burnt by flame 16 in a head combustion chamber 7.
      COPYRIGHT: (C)1986,JPO&Japio
    • 目的:为了便于在设有燃烧器的燃气轮机中使用二级燃烧系统点燃二次燃料,通过在起动后二次燃料燃烧后排空压缩空气,并通过在这种燃烧系统中启动二次空气的燃烧 条件是流入燃烧器的空气量减少。 构成:在启动燃气轮机2时,首先利用辅助原动机来驱动压缩机1,并且当涡轮机的转速达到一定值时,控制燃料调节阀21以喷射初级燃料 从主燃料喷嘴19喷射喷射的燃料。 利用这种布置,燃气轮机2进入其自维持操作。 当燃气轮机2的旋转速度达到预定值时,打开排气阀33以将压缩机1中的空气释放到大气中,从而可以减少流入燃烧器3的空气量。 在这种排气操作下,燃料调节阀22被控制成以阶梯状的方式从二次燃料供给口13供给二次燃料,同时一级燃料以阶梯状的方式减少,因此二次燃料被燃烧 火焰16在头部燃烧室7中。
    • 9. 发明专利
    • Cooling device for ceramics metal compound stationary blade
    • 用于陶瓷金属化合物固定式叶片的冷却装置
    • JPS6189906A
    • 1986-05-08
    • JP21139384
    • 1984-10-11
    • Central Res Inst Of Electric Power IndHitachi Ltd
    • ABE TOSHIOISHIKAWA HIROSHIHISAMATSU NOBORUMIYATA HIROSHIIIJIMA SHIROOSHIMA RYOICHIRO
    • F01D9/02F01D5/28
    • F01D5/284
    • PURPOSE:To reduce the required cooling air volume by configurating cooling air passages inside a metal member arranged within a ceramic stationary blade. CONSTITUTION:A metal member 8 is arranged in the hollow section of a ceramic stationary blade 7 where an upper side wall 3 and an upper ceramic liner 5 are fastened with a respective lower side wall and a respective ceramic liner allowing cooling air passages to be formed inside the metal member 8. Cooling air A enters inside of the blade 7 through the cooling air passages allowing it to be exhausted through fit sections between the blade 7 and the ceramic liners 5 into combustion gas C. This configuration enables the cooling to be limited only to the metal member permitting the required cooling air volume to be reduced significantly.
    • 目的:通过在布置在陶瓷固定刀片内的金属构件内配置冷却空气通道来减少所需的冷却风量。 构成:金属构件8布置在陶瓷固定刀片7的中空部分中,其中上侧壁3和上陶瓷衬垫5用相应的下侧壁和相应的陶瓷衬里紧固,允许形成冷却空气通道 冷却空气A通过冷却空气通道进入叶片7的内部,从而允许其通过叶片7和陶瓷衬垫5之间的配合部分排出到燃烧气体C中。这种结构使冷却受到限制 仅允许使所需的冷却空气体积显着减小的金属构件。