公开(公告)号：US07340881B2

公开(公告)日：2008-03-11

申请号：US10730088

申请日：2003-12-09

申请人： Tomomi Koganezawa ,  Hiroshi Inoue ,  Kazuhiko Kawaike

发明人： Tomomi Koganezawa ,  Hiroshi Inoue ,  Kazuhiko Kawaike

IPC分类号： F02C7/00 ,  F02C3/14

CPC分类号： F01D9/023 ,  F02C3/145 ,  F02C7/08 ,  F05D2260/212

摘要： The invention provides a gas turbine combustor in which the size of a combustor outer casing can be reduced. A transition inner duct and a transition outer duct are disposed in a main housing, inlet openings for a fluid to cool the transition inner duct are formed at ends of the transition outer duct on both sides nearer to the combustor liner and the turbine, and the transition outer duct is formed as an extraction flow passage for extracting the cooling fluid having flown in through the inlet openings to a recuperator. A partition member is also provided to prevent the fluid in the main housing and the fluid in the combustor outer casing from mixing with each other.

摘要翻译： 本发明提供一种燃气轮机燃烧器，其中可以减小燃烧器外壳的尺寸。 过渡内管道和过渡外管道设置在主壳体中，用于冷却过渡内管道的流体的入口开口形成在过渡外管道的靠近燃烧器衬套和涡轮机的两侧的端部，并且 过渡外管形成为用于将通过入口开口流入的冷却流体提取到换热器的提取流路。 还设置有分隔构件以防止主壳体中的流体和燃烧器外壳体中的流体彼此混合。

公开(公告)号：US07028486B2

公开(公告)日：2006-04-18

申请号：US10782961

申请日：2004-02-23

申请人： Shinya Marushima ,  Manabu Matsumoto ,  Kazuhiko Kawaike ,  Takashi Ikeguchi ,  Takashi Machida ,  Masaru Sekihara

发明人： Shinya Marushima ,  Manabu Matsumoto ,  Kazuhiko Kawaike ,  Takashi Ikeguchi ,  Takashi Machida ,  Masaru Sekihara

IPC分类号： F02G7/12

CPC分类号： F02C7/18 ,  F01D25/12 ,  F05D2260/205 ,  F05D2260/2322

摘要： An object is to improve the operational reliability of a gas turbine by suppressing thermal stress and thermal deformation acting on the rotor of the gas turbine. The gas turbine has a rotor shaft constructed by arranging, in an axial direction in turn, a plurality of discs each having a plurality of combustion gas-driven moving blades annularly arranged on the peripheral portion and spacers arranged between the discs, and is characterized in that gap portions are formed between a region, on the rotor shaft center portion side, of the above-mentioned discs facing the spacers and spacers adjacent thereto, contact surfaces are formed both of which contact on both a region, on the rotor peripheral side, of the above-mentioned discs facing the spacers and adjacent spacers thereto, and a third flow path leading fluid to the above-mentioned gap portions is provided.

公开(公告)号：US5575153A

公开(公告)日：1996-11-19

申请号：US220251

申请日：1994-03-30

申请人： Kazuyuki Ito ,  Tadayoshi Murakami ,  Kazuhiko Kawaike ,  Shigeru Azuhata ,  Michio Kuroda

发明人： Kazuyuki Ito ,  Tadayoshi Murakami ,  Kazuhiko Kawaike ,  Shigeru Azuhata ,  Michio Kuroda

IPC分类号： F02C9/28 ,  F23R3/12 ,  F23R3/16 ,  F23R3/18 ,  F02C1/02

CPC分类号： F23N5/242 ,  F02C9/28 ,  F23R3/12 ,  F23R3/16 ,  F23R3/18 ,  F05D2240/127 ,  F23N2041/20

摘要： A plurality of turbulence promotors (11) are arranged on a surface of a stabilizer (11) comprising a stabilizer portion (14) contacting combustion gas and support portion (15) for rectifying flow except for a heat receiving surface (13) contacting with combustion gas to promote heat transfer from the stabilizer to an air fuel flow. The distance between the turbulence promotor closest to the heat receiving surface (13) and the heat receiving surface is at least 4 times the height of said turbulence promotor to prevent back fire due to provision of the turbulence promotor.

摘要翻译： 多个湍流促进器（11）布置在稳定器（11）的表面上，稳定器（11）包括接触燃烧气体的稳定器部分（14）和用于整流的支撑部分（15），除了与燃烧接触的热接收表面（13） 气体以促进从稳定器到空气燃料流的热传递。 最接近热接收表面（13）的湍流促进器和受热表面之间的距离是所述湍流促进器的高度的至少4倍，以防止由于提供湍流启动器引起的反火。

公开(公告)号：US5399065A

公开(公告)日：1995-03-21

申请号：US114074

申请日：1993-08-31

申请人： Takeshi Kudo ,  Isao Takehara ,  Tetsuo Sasada ,  Shunichi Anzai ,  Kazuhiko Kawaike

发明人： Takeshi Kudo ,  Isao Takehara ,  Tetsuo Sasada ,  Shunichi Anzai ,  Kazuhiko Kawaike

IPC分类号： F01D5/18 ,  F02C7/18 ,  F02C7/28 ,  F01D9/02

CPC分类号： F01D5/187 ,  F05D2240/10 ,  F05D2260/201 ,  F05D2260/2212

摘要： In a cascade device for a gas turbine, cooling air which has passed through a trailing air cooling chamber of each stationary blade is discharged from a tip of the stationary blade toward a side surface of a base of a moving blade disposed adjacent to the stationary blade. With this arrangement, the cooling of the stationary blade as well as the sealing of a cascade portion is effected satisfactorily with a smaller amount of the air.

摘要翻译： 在用于燃气轮机的级联装置中，已经通过每个固定叶片的拖尾空气冷却室的冷却空气从静止叶片的尖端朝着与固定叶片相邻设置的活动叶片的底部的侧表面排出 。 通过这种布置，静止叶片的冷却以及级联部分的密封以较少量的空气令人满意地进行。

公开(公告)号：US5108198A

公开(公告)日：1992-04-28

申请号：US553375

申请日：1990-07-17

申请人： Katsutoshi Nii ,  Kazuhiko Kawaike ,  Jun Matsubayashi ,  Satosi Uno

发明人： Katsutoshi Nii ,  Kazuhiko Kawaike ,  Jun Matsubayashi ,  Satosi Uno

IPC分类号： F16C32/04 ,  F16C33/10 ,  F16C33/82 ,  F16J15/40 ,  F16J15/43

CPC分类号： F16J15/43 ,  F16C33/1035 ,  F16C33/746

摘要： A sliding bearing an an end ring are mounted on a housing. A magnetic fluid sealing member comprises a permanent magnet and a magnetic fluid. A space is formed between the magnetic fluid sealing member and a lubricating fluid. A shaft has projection member or the end ring forms a spiral groove on an inner peripheral portion. The projection member of the shaft or the spiral groove of the end ring is disposed in an opposite position of the magnetic fluid sealing member. A magnetic fluid flow is disturbed by the projection member of the shaft or the spiral groove of the end ring according to a rotation of the shaft, then a magnetic fluid film is destructed instantaneously and the pressure at the space lowers. Air in the space is discharged from the housing. The scatter degree of the magnetic fluid is made slightly.

摘要翻译： 一个端环的滑动轴承安装在外壳上。 磁性流体密封构件包括永磁体和磁性流体。 在磁性流体密封构件和润滑流体之间形成空间。 轴具有突出构件或端环在内周部分上形成螺旋槽。 轴的突出构件或端环的螺旋槽设置在磁性流体密封构件的相对位置。 根据轴的旋转，磁流体流动被轴的突出构件或端环的螺旋槽扰动，然后瞬时破坏磁性流体膜并且空间中的压力降低。 空间中的空气从外壳排出。 磁性流体的散射度略微变小。

公开(公告)号：US06393829B2

公开(公告)日：2002-05-28

申请号：US09308981

申请日：1999-05-28

申请人： Shinya Marushima ,  Manabu Matsumoto ,  Kazuhiko Kawaike ,  Takashi Ikeguchi ,  Takashi Machida ,  Masaru Sekihara

发明人： Shinya Marushima ,  Manabu Matsumoto ,  Kazuhiko Kawaike ,  Takashi Ikeguchi ,  Takashi Machida ,  Masaru Sekihara

IPC分类号： F02C300

CPC分类号： F02C7/18 ,  F01D25/12 ,  F05D2260/205 ,  F05D2260/2322

摘要： A gas turbine has a rotor shaft which includes a plurality of discs, each having a plurality of moving blades driven by combustion gas and arranged annularly on the peripheral portion and having spaces arranged between the discs. The respective discs and spacers are arranged in the axial direction. Gap portions are formed between the rotor axis side regions of the discs facing the spacers and adjacent spacers. Contact surfaces contacting each other on both rotor peripheral side regions of the discs facing the spaces and adjacent spacers are formed. A first flow path for supplying a coolant into the moving blades and a second flow path for recovering the coolant heated by the moving blades from the moving blade are provided. A third flow path for introducing fluid into the gap portions is formed in the discs with the third flow path being independent from the first and second flow paths.

摘要翻译： 燃气轮机具有转子轴，该转子轴包括多个盘，每个盘具有由燃烧气体驱动的多个活动叶片，环形地布置在周边部分上，并且在盘之间具有间隔。 相应的盘和间隔件沿轴向布置。 间隙部分形成在面向间隔物和相邻间隔物的盘的转子轴线侧区域之间。 形成面对空间和相邻间隔物的圆盘的两个转子周边区域彼此接触的接触表面。 提供了用于将冷却剂供应到动叶片中的第一流动路径和用于从动叶片回收由移动叶片加热的冷却剂的第二流路。 用于将流体引入间隙部分的第三流动路径形成在盘中，其中第三流动路径独立于第一和第二流动路径。

公开(公告)号：USRE35718E

公开(公告)日：1998-01-27

申请号：US528059

申请日：1995-09-14

申请人： Katsutoshi Nii ,  Kazuhiko Kawaike ,  Hiroo Hiroyama ,  Satoshi Uno

发明人： Katsutoshi Nii ,  Kazuhiko Kawaike ,  Hiroo Hiroyama ,  Satoshi Uno

IPC分类号： F16C33/10 ,  F16C33/82 ,  F16C32/06

CPC分类号： F16C33/10 ,  F16C33/1035 ,  F16C33/746

摘要： A bearing apparatus comprises a housing formed of a non-magnetizable material and having a bottom portion, a fluid lubricating type radial bearing device provided coaxial with the housing and having a magnetic fluid sealing section and a radial bearing section, a thrust bearing device provided at the bottom portion of the housing, and a rotating shaft of a permeable material rotatable supported by the radial bearing device and thr thrust bearing device to extend through the radial bearing device. The magnetic fluid sealing section is disposed on the opening side of the housing with a predetermined spacing away from the radial bearing section whereby a space is provided between the magnetic fluid sealing section and a liquid surface of fluid lubricant filled in the radial bearing section.

摘要翻译： 轴承装置包括由不可磁化材料形成并具有底部的壳体，与壳体同轴设置并具有磁性流体密封部分和径向轴承部分的流体润滑型径向轴承装置，其中设置有推力轴承装置 壳体的底部以及由径向轴承装置和推力轴承装置可旋转地支撑的可渗透材料的旋转轴，以延伸穿过径向轴承装置。 磁性流体密封部分以距离径向轴承部分预定间隔的方式设置在壳体的开口侧上，从而在磁性流体密封部分和填充在径向支承部分中的流体润滑剂的液体表面之间设置空间。

公开(公告)号：US5139349A

公开(公告)日：1992-08-18

申请号：US771107

申请日：1991-10-04

申请人： Masaaki Nakano ,  Kazuhiko Kawaike ,  Eiichi Okuyama ,  Kenzo Kajiwara

发明人： Masaaki Nakano ,  Kazuhiko Kawaike ,  Eiichi Okuyama ,  Kenzo Kajiwara

IPC分类号： F16C33/10 ,  F16N7/18 ,  F16N39/00

CPC分类号： F16C33/103 ,  F16C33/10 ,  F16N39/002 ,  F16N7/18

摘要： A bearing device for a horizontal shaft type rotating machine includes an oil tank formed at the lower portion of the bearing box for storing lubricant oil for the bearing, the oil tank being divided by a bearing support plate between an oil feeding chamber and an oil collecting chamber; an oil feeding apparatus which pumps up the lubricant oil in the oil feeding chamber and feeds the lubricant oil onto the bearing; and a pair of diffusion flow passages; each of the pair of diffusion flow passages being formed along the inner wall of the oil tank and connects the oil collecting chamber with the oil feeding chamber; each of the diffusion flow passages permitting diffusion and movement of the lubricant oil from the oil collecting chamber to the oil feeding chamber. Each of the diffusion flow passages including a baffle chamber and a narrow gap flow passage downstream of the baffle chamber and having a smaller cross section flow passage area than the baffle chamber and the upper portion of the baffle chamber being open to the air, whereby air bubbles contained in the collected high temperature lubricant oil are removed at an early stage of their return travel from the oil collecting chamber to the oil feeding chamber.

摘要翻译： 一种用于水平轴式旋转机械的轴承装置，包括形成在用于轴承的润滑油的轴承箱的下部的油箱，油箱由供油室和集油器之间的轴承支撑板分隔开 房间 一个给油装置，其将润滑油泵送在给油室中并将润滑油供给到轴承上; 和一对扩散流路; 所述一对扩散流路沿着所述油箱的内壁形成，并将所述集油室与所述给油室连接; 每个扩散流通道允许润滑油从集油室扩散和移动到给油室。 每个扩散流通道包括挡板室和在挡板室下游的窄间隙流动通道，并且具有比挡板室更小的横截面流动通道面积，并且挡板室的上部向空气敞开，由此空气 收集的高温润滑油中的气泡在从油收集室返回给油室的返回的早期阶段被除去。

公开(公告)号：US4878820A

公开(公告)日：1989-11-07

申请号：US194917

申请日：1988-05-17

申请人： Motomichi Doi ,  Minetoshi Izushi ,  Kazuhiko Kawaike ,  Masayuki Urashin

发明人： Motomichi Doi ,  Minetoshi Izushi ,  Kazuhiko Kawaike ,  Masayuki Urashin

IPC分类号： F04C18/16 ,  F04C29/00 ,  F04C29/02 ,  F16C17/26

CPC分类号： F16C17/26 ,  F04C29/0021 ,  F16C33/106

摘要： A screw compressor comprises a casing and a pair of male and female rotors respectively having herical teeth and grooves formed in their outer peripheries. The rotors are arranged within the casing in meshing relation to each other through the teeth and grooves. Each rotor is rotatably supported by a pair of first and second radial plain bearings and a thrust plain bearing which is arranged at an end of the rotor shaft and adjacent the second radial plain bearing. Each of the thrust plain bearings is of dynamic-pressure type in which with rotation of a corresponding one of the shafts of the respective rotors, pressure is applied to lubricant by sliding movement of the thrust plain bearing to produce an anti-thrust force. The lubricant for each of the second radial plain bearings and for a corresponding one of the thrust plain bearings is fed to a space between the second radial plain bearing and the thrust plain bearing, and is distributed to the second radial plain bearing more in amount than that fed to the thrust bearing due to a difference between flow resistance with which the lubricant passes through the second radial plain bearing and flow resistance with which the lubricant passes through the thrust plain bearing.

摘要翻译： 螺杆式压缩机包括壳体和一对分别具有在其外周部形成的齿状齿和凹槽的阳和阴转子。 转子通过齿和凹槽以彼此啮合的关系布置在壳体内。 每个转子由一对第一和第二径向滑动轴承和推力滑动轴承可旋转地支撑，所述推力滑动轴承布置在转子轴的端部并与第二径向滑动轴承相邻。 每个推力滑动轴承都是动压型，其中通过相应转子的相应一个轴的旋转，通过推力滑动轴承的滑动运动将压力施加到润滑剂以产生抗推力。 每个第二径向滑动轴承和对应的一个推力滑动轴承的润滑剂被供给到第二径向滑动轴承和推力滑动轴承之间的空间，并且分配到第二径向滑动轴承的数量大于 由于润滑剂通过第二径向滑动轴承的流动阻力和润滑剂通过推力滑动轴承的流动阻力之间的差异而被馈送到推力轴承。

公开(公告)号：US06735957B2

公开(公告)日：2004-05-18

申请号：US10403124

申请日：2003-04-01

申请人： Shinya Marushima ,  Manabu Matsumoto ,  Kazuhiko Kawaike ,  Takashi Ikeguchi ,  Takashi Machida ,  Masaru Sekihara

发明人： Shinya Marushima ,  Manabu Matsumoto ,  Kazuhiko Kawaike ,  Takashi Ikeguchi ,  Takashi Machida ,  Masaru Sekihara

IPC分类号： F02G712

CPC分类号： F02C7/18 ,  F01D25/12 ,  F05D2260/205 ,  F05D2260/2322

摘要： An object is to improve the operational reliability of a gas turbine by suppressing thermal stress and thermal deformation acting on the rotor of the gas turbine. The gas turbine has a rotor shaft constructed by arranging, in an axial direction in turn, a plurality of discs each having a plurality of combustion gas-driven moving blades annularly arranged on the peripheral portion and spacers arranged between the discs, and is characterized in that gap portions are formed between a region, on the rotor shaft center portion side, of the above-mentioned discs facing the spacers and spacers adjacent thereto, contact surfaces are formed both of which contact on both a region, on the rotor peripheral side, of the above-mentioned discs facing the spacers and adjacent spacers thereto, and a third flow path leading fluid to the above-mentioned gap portions is provided.

摘要翻译： 目的是通过抑制作用在燃气轮机的转子上的热应力和热变形来提高燃气轮机的操作可靠性。 燃气轮机具有转子轴，转子轴沿轴向方向依次布置有多个盘，每个盘具有环形地设置在周边部分上的多个燃烧气体驱动的移动叶片和布置在盘之间的间隔件，其特征在于 在转子轴中心部分侧的面对间隔件的盘和相邻的间隔件之间形成间隙部分，形成两个接触表面，这两个接触表面在转子周边侧的两个区域上接触， 上述圆盘面对间隔件和相邻的间隔件，并且提供了将流体引导到上述间隙部分的第三流动路径。