公开(公告)号：US06327845B2

公开(公告)日：2001-12-11

申请号：US09742389

申请日：2000-12-22

申请人： Yasuhiro Ojiro ,  Koichi Akagi ,  Yoichi Iwasaki ,  Jun Kubota ,  Sunao Umemura

发明人： Yasuhiro Ojiro ,  Koichi Akagi ,  Yoichi Iwasaki ,  Jun Kubota ,  Sunao Umemura

IPC分类号： F02C700

CPC分类号： F01D17/10 ,  F01D17/105 ,  F01D17/148 ,  F23R3/26

摘要： Gas turbine combustor by-pass valve device for opening and closing a by-pass valve is improved to uniformly control air supply into a combustion area for appropriate combustion. A drive shaft 21 for opening and closing a driven by-pass valve 20 is provided in turbine casing 010 where an outside obstruction is located which would interfere with a projecting drive shaft 09. The driven shaft 21 has a short length to be provided in the turbine casing 010. An adjacent main driving shaft 23 for opening and closing main driving by-pass valve 22 is provided adjacent to the driven shaft 21. Link mechanism 26 is provided between the adjacent main driving shaft 23 and the driven shaft 21 so that rotary movement of adjacent main driving shaft 23 driven by outside drive means via the drive shaft 09 is transmitted to the driven shaft 21 and, thus, to the driven by-pass valve 20. Thus, partial drive shafts 09 are made shorter so as not to project outside of the turbine casing 010 and interfere with outside obstruction, but all the by-pass valves 08 provided along circumferential direction of the turbine casing 010 can be operated to be opened and closed uniformly.

摘要翻译： 提高了用于打开和关闭旁通阀的燃气轮机燃烧器旁通阀装置，以均匀地控制进入燃烧区域的空气进行适当的燃烧。 用于打开和关闭从动旁通阀20的驱动轴21设置在涡轮机壳体010中，其外部阻塞件位于将会与突出的驱动轴09干涉。从动轴21具有短的长度 涡轮机壳体010.相邻的主驱动旁通阀22的相邻的主驱动轴23设置在从动轴21附近。连杆机构26设置在相邻的主驱动轴23与从动轴21之间， 通过驱动轴09由外部驱动装置驱动的相邻主驱动轴23的移动被传递到从动轴21，从而被传递到被驱动的旁通阀20.因此，部分驱动轴09被制成更短，以便不 在涡轮壳体010外部突出并干扰外部阻塞，但是沿着涡轮机壳体010的圆周方向设置的所有旁通阀08可以被均匀地打开和关闭。

公开(公告)号：US06237323B1

公开(公告)日：2001-05-29

申请号：US09365894

申请日：1999-08-03

申请人： Yasuhiro Ojiro ,  Koichi Akagi ,  Yoichi Iwasaki ,  Jun Kubota ,  Sunao Umemura

发明人： Yasuhiro Ojiro ,  Koichi Akagi ,  Yoichi Iwasaki ,  Jun Kubota ,  Sunao Umemura

IPC分类号： F23R326

CPC分类号： F01D17/10 ,  F01D17/105 ,  F01D17/148 ,  F23R3/26

摘要： Gas turbine combustor by-pass valve device for opening and closing by-pass valve is improved to control uniformly air supply into combustion area for appropriate combustion. Drive shaft 21 for opening and closing driven by-pass valve 20 is provided in turbine casing 010 where outside obstruction is located to interfere with projecting drive shaft 09. The driven shaft 21 is made in short length to be provided in the turbine casing 010. Adjacent main driving shaft 23 for opening and closing main driving by-pass valve 22 is provided adjacently to the driven shaft 21. Link mechanism 26 is provided between the adjacent main driving shaft 23 and the driven shaft 21, thereby rotary movement of adjacent main driving shaft 23 driven by outside drive means via the drive shaft 09 is transmitted to the driven shaft 21 and thus to the driven by-pass valve 20. Thus, partial drive shafts 09 are made shorter not to project outside of the turbine casing 010 to interfere with outside obstruction and still all the by-pass valves 08 provided along circumferential direction of the turbine casing 010 can be operated to be opened and closed uniformly.

摘要翻译： 提高了用于打开和关闭旁通阀的燃气轮机燃烧器旁通阀装置，以均匀地控制进入燃烧区域的空气进行适当的燃烧。 用于打开和关闭驱动的旁通阀20的驱动轴21设置在涡轮机壳体010中，其中外部阻塞件位于外部障碍物处以与突出的驱动轴09干涉。从动轴21制成较短的长度以设置在涡轮机壳体010中。 相邻的主驱动旁通阀22的主驱动轴23与从动轴21相邻地设置。连杆机构26设置在相邻的主驱动轴23和从动轴21之间，从而相邻的主驱动 通过驱动轴09由外部驱动装置驱动的轴23被传递到从动轴21，从而被传递到被驱动的旁通阀20.因此，部分驱动轴09被制成更短，不会突出到涡轮机壳体010的外部以干涉 具有外部阻塞，并且沿着涡轮机壳体010的圆周方向设置的所有旁通阀08可以被均匀地打开和关闭。

公开(公告)号：US08776369B2

公开(公告)日：2014-07-15

申请号：US12521671

申请日：2008-05-27

申请人： Junya Michinishi ,  Koichi Akagi ,  Shuichi Kajiwara ,  Katsunori Akiyama ,  Sunao Aoki

发明人： Junya Michinishi ,  Koichi Akagi ,  Shuichi Kajiwara ,  Katsunori Akiyama ,  Sunao Aoki

IPC分类号： B23P15/16 ,  B23P17/00

CPC分类号： B23P15/16 ,  B23K28/02 ,  B23K2101/006 ,  B23K2101/04 ,  F02C7/22 ,  F02M61/168 ,  F02M2200/8069 ,  F02M2200/8084 ,  F05D2230/232 ,  F05D2240/128 ,  F23D2206/10 ,  F23D2213/00 ,  F23R3/28 ,  Y10T29/49316 ,  Y10T29/49323 ,  Y10T29/49405 ,  Y10T29/49426 ,  Y10T29/49432 ,  Y10T29/49995

摘要： There is provided a through-hole manufacturing method for a cylindrical body wall that enables the operation of forming a through-hole without leaving a machining burr on the wall of a cylindrical member to be easily and reliably carried out without depending on experts. A through-hole manufacturing method for a cylindrical body wall in which a machining burr is not formed on inner walls of through holes formed by a tool piercing the wall of a cylindrical body, the method including a hole forming step of forming one pair or a plurality of pairs of the through-holes in the cylindrical body wall by the tool piercing the cylindrical body from the outside orthogonally or substantially orthogonally to a cylindrical body axis of the cylindrical body; and a welding step of sealing the through-hole formed by the tool piercing the cylindrical body from the outer wall to the inner wall by welding using a welding jig made of a material having better heat conductivity than the cylindrical body, wherein the through-hole formed by the tool piercing the cylindrical body from the inner wall to the outer wall is left as a nozzle hole.

摘要翻译： 提供了一种圆筒体壁的通孔制造方法，其能够在不依赖专家的情况下容易且可靠地执行，从而能够在圆柱形构件的壁上形成通孔而不留下加工毛刺的操作。 一种圆筒体壁的通孔制造方法，其中在穿过圆筒体的壁的工具形成的通孔的内壁上没有形成加工毛刺，所述方法包括形成一对的孔形成步骤或 多个成对的通孔通过工具将圆柱体从正交或大致正交地与圆筒体的圆柱体轴线正交地从外侧穿入圆筒体壁; 以及焊接工序，其使用由比所述圆筒体更好的导热性的材料制成的焊接夹具通过焊接将由所述工具穿过所述圆筒体的所述工具形成的通孔从所述外壁密封到所述内壁，其中，所述通孔 由从内壁向外壁穿过圆柱体的工具形成为喷嘴孔。

公开(公告)号：US6164908A

公开(公告)日：2000-12-26

申请号：US230946

申请日：1999-02-04

申请人： Miki Nishida ,  Taku Ichiryu ,  Koichi Akagi ,  Hiroki Shibata ,  Tadakazu Sakaguchi

发明人： Miki Nishida ,  Taku Ichiryu ,  Koichi Akagi ,  Hiroki Shibata ,  Tadakazu Sakaguchi

IPC分类号： F01D9/04 ,  F01D9/02 ,  F01D11/00 ,  F01D11/04 ,  F02C7/18 ,  F02C7/28 ,  F01D5/00

CPC分类号： F01D9/02 ,  F01D11/005 ,  F02C7/18 ,  Y02T50/675

摘要： A gas turbine first-stage stator blade sealing structure for preventing the sealing air from leaking from the inside even if the blade falls or inclines due to thermal stress. A rear flange (12) of a first-stage stator blade (31) is formed in an arcuate shape having a straight rib (10). A stator blade support ring (13) contacts the straight rib (10) to form a sealing face. When the rear flange (12) and the stator blade support ring (13) fall or incline relative to each other due to thermal stress during operation, the upper end or lower end of the rib (10) contacts linearly with the face of the stator blade support ring (13) so that no clearance is established to inhibit leakage of the sealing air. In the prior art, where the horizontal rib (10) is absent, an arcuate clearance is established between the stator blade support ring (13) and the rear flange (12) as the support ring (13) inclines, and thus sealing air is allowed to leak from the inside to the gas passages.

摘要翻译： PCT No.PCT / JP98 / 02477 Sec。 371日期1999年2月4日 102（e）日期1999年2月4日PCT提交1998年6月4日PCT公布。 出版物WO98 / 55737 日期1998年12月10日用于防止密封空气从内部泄漏的燃气轮机第一级定子叶片密封结构，即使叶片由于热应力而下降或倾斜。 第一级定子叶片（31）的后凸缘（12）形成为具有直肋（10）的弓形。 定子叶片支撑环（13）接触直肋（10）以形成密封面。 当后凸缘（12）和定子叶片支撑环（13）由于操作期间的热应力而相对于彼此落下或倾斜时，肋（10）的上端或下端与定子的表面线性接触 叶片支撑环（13），使得不建立间隙以阻止密封空气的泄漏。 在不存在水平肋（10）的现有技术中，当支撑环（13）倾斜时，在定子叶片支撑环（13）和后凸缘（12）之间建立弓形间隙，因此密封空气 允许从内部泄漏到气体通道。

公开(公告)号：US20140290255A1

公开(公告)日：2014-10-02

申请号：US14009004

申请日：2012-05-18

申请人： Koichi Akagi ,  Katsuyoshi Omae ,  Kunihiro Ohashi ,  Toshio Fujii ,  Junya Michinishi ,  Fumiko Machida

发明人： Koichi Akagi ,  Katsuyoshi Omae ,  Kunihiro Ohashi ,  Toshio Fujii ,  Junya Michinishi ,  Fumiko Machida

IPC分类号： F02C7/00

CPC分类号： F02C7/00 ,  B21D5/06 ,  B21D53/92 ,  B23K20/02 ,  B23K2101/001 ,  F01D11/08 ,  F05D2230/236 ,  F05D2250/291 ,  F05D2250/71 ,  F05D2260/20 ,  F23R3/002 ,  F23R3/005 ,  F23R3/06 ,  F23R2900/00012 ,  F23R2900/00018 ,  F23R2900/03042 ,  F23R2900/03044 ,  Y10T29/49229

摘要： Hollow curved plates (20, 50, 70) include first plate members 241-243 having a first groove 22 and second plate members 341-343 having a second groove 32 of approximately the same width as the first groove 22, the second plate members 341-343 being bonded to the first plate members 241-243 by diffusion bonding. The hollow curved plate is formed of the first plate members 241-243 and the second plate members 341-343 curved by bending in a state where the first plate members 241-243 and the second plate members 341-343 are bonded together. The first groove 22 faces the second groove 32, a position of the first groove 22 substantially coincides with a position of the second groove 32 in a width direction, and hollow parts 401-403 are formed by the first groove 22 and the second groove 32.

摘要翻译： 中空弯曲板（20,50,70）包括具有第一槽22的第一板构件241-243和具有与第一槽22大致相同宽度的第二槽32的第二板构件341-343，第二板构件341 -343通过扩散接合结合到第一板构件241-243。 中空弯曲板由第一板构件241-243和第二板构件341-343形成，第一板构件241-243和第二板构件341-343在第一板构件241-243和第二板构件341-343接合在一起的状态下通过弯曲弯曲。 第一槽22面对第二槽32，第一槽22的位置与宽度方向上的第二槽32的位置基本一致，中空部401-403由第一槽22和第二槽32形成 。

公开(公告)号：US08769957B2

公开(公告)日：2014-07-08

申请号：US13526010

申请日：2012-06-18

申请人： Satoshi Hada ,  Sosuke Nakamura ,  Katsunori Tanaka ,  Koichi Akagi ,  Tetsu Konishi ,  Hiroki Shibata

发明人： Satoshi Hada ,  Sosuke Nakamura ,  Katsunori Tanaka ,  Koichi Akagi ,  Tetsu Konishi ,  Hiroki Shibata

IPC分类号： F02C1/00 ,  F02G3/00 ,  F02C7/12

CPC分类号： F01D9/023 ,  F23R3/002 ,  F23R3/005 ,  F23R3/60 ,  F23R2900/00017 ,  F23R2900/00018 ,  F23R2900/03043

摘要： A transition piece of a combustor which is sustainable even under conditions of more severe thermal environments is provided in the present invention. A transition piece of a combustor is provided with a cylindrical trunk main body, a cylindrical exit trunk part which is joined to the downstream end of the trunk main body and which cooperates with the trunk main body to constitute a trunk part, and an inner flange which extends from the downstream end part of the exit trunk part toward the outer periphery side of the exit trunk part. The exit trunk part and the inner flange are of an one-piece product. On the exit trunk part, there is formed a groove, and there is formed a cooling fluid passage which opens at the groove.

摘要翻译： 在本发明中提供了即使在更严重的热环境的条件下也是可持续的燃烧器的过渡件。 燃烧器的过渡件设置有圆筒形主体，圆筒形出口主体部分，其连接到主体主体的下游端并与主体主体配合以构成主体部分;以及内凸缘 其从出口主干部分的下游端部朝向出口主干部分的外周侧延伸。 出口主体部分和内部凸缘是一体式产品。 在出口主体部分上形成有一个凹槽，并形成一个在凹槽处开口的冷却流体通道。

公开(公告)号：US06324829B1

公开(公告)日：2001-12-04

申请号：US09237845

申请日：1999-01-27

申请人： Yoshiyuki Kita ,  Tomoka Tanaka ,  Yasuhiro Hashimoto ,  Masayuki Takahama ,  Jun Yasuraoka ,  Hidetoshi Iida ,  Koichi Akagi ,  Hideki Haruta

发明人： Yoshiyuki Kita ,  Tomoka Tanaka ,  Yasuhiro Hashimoto ,  Masayuki Takahama ,  Jun Yasuraoka ,  Hidetoshi Iida ,  Koichi Akagi ,  Hideki Haruta

IPC分类号： F02C600

CPC分类号： F01K23/108 ,  Y02E20/16 ,  Y02P80/152

摘要： A gas turbine steam cooled system has a high temperature portion 8 outlet steam temperature maintained to a predetermined value without a cooling steam pressure becoming lower than the pressure in the gas turbine cylinder. Steam coming from an intermediate pressure superheater 10 of a waste heat recovery boiler 2 is led into the high temperature portion 8 of the gas turbine for cooling thereof. The temperature of the cooling steam at the outlet of the high temperature portion 8 is detected by a high temperature portion outlet steam temperature detector 15, and a signal thereof is sent a lower value selector 19 via a temperature controller 11. Pressure in the gas turbine cylinder is detected by a gas turbine cylinder pressure detector 17, and pressure of the cooling steam at the high temperature portion 8 outlet is detected by a high temperature portion outlet steam pressure detector 16. A differential signal thereof is sent to a pressure controller 18. Signals from the temperature controller 11 and the pressure controller 18 are inputted into the lower selector 19, and temperature control valve 12 is controlled by the lower value thereof to be opened and closed.

摘要翻译： 燃气轮机蒸汽冷却系统具有保持预定值的高温部分8出口蒸汽温度，而冷却蒸汽压力变得低于燃气轮机气缸中的压力。 来自废热回收锅炉2的中压过热器10的蒸汽被引入燃气轮机的高温部8，以进行冷却。 高温部分8出口处的冷却蒸汽的温度由高温部分出口蒸气温度检测器15检测，其信号通过温度控制器11送到低值选择器19.燃气轮机中的压力 气缸由燃气轮机气缸压力检测器17检测，高温部分8出口处的冷却蒸汽的压力由高温部分出口蒸汽压力检测器16检测。其差分信号被发送到压力控制器18。 来自温度控制器11和压力控制器18的信号被输入到下部选择器19中，并且温度控制阀12被其较低的值控制为打开和关闭。

公开(公告)号：US6089827A

公开(公告)日：2000-07-18

申请号：US242108

申请日：1999-02-09

申请人： Taku Ichiryu ,  Koichi Akagi ,  Yasuoki Tomita

发明人： Taku Ichiryu ,  Koichi Akagi ,  Yasuoki Tomita

IPC分类号： F01D5/06 ,  F01D5/08 ,  F01D11/00 ,  B63H1/00

CPC分类号： F01D5/066 ,  F01D11/005 ,  F01D5/084

摘要： A gas turbine rotor, in which a plurality of discs having teeth of a bevel gear are juxtaposed to engage the teeth and are integrally fastened by a bolt extending through the discs, so that the discs may be cooled by feeding cooling air to the air passages of the individual discs sequentially at the running time, is provided whereby the cooling air is prevented from leaking by means having no wear. Radially outward of an air passage through hole of the faces of the adjoining discs, there are provided arms which are made lower than the dedendums of the teeth and protruded in an annular shape to confront each other; one of the arms has a tip made to have an elastically deformable thickness and a sectional shape bent inward or outward, whereas there is welded to the other arm an extension which has a tip made to have an elastically deformable thickness and a sectional shape bent inward or outward; and the end face of the tip of the one arm and the end face of the tip of the extension of the other arm are held in abutment against each other so that the two end faces may be forced, when the discs are integrated, into contact with each other to prevent leakage of cooling air.

摘要翻译： PCT No.PCT / JP98 / 02564 Sec。 371日期1999年2月9日 102（e）1999年2月9日PCT PCT 1996年6月10日PCT公布。 第WO98 / 57040号公报 日期1998年12月17日一种燃气轮机转子，其中具有锥齿轮齿的多个盘并列配合以接合齿，并且通过延伸穿过盘的螺栓一体地紧固，使得盘可以通过进给冷却来冷却 提供了在运行时间顺序地对各个盘的空气通道的空气，由此通过没有磨损的装置防止冷却空气泄漏。 设置在相邻盘的表面的空气通道通孔的径向外侧，设置有比齿的齿根低的突出的环状并相互对置的臂。 其中一个臂具有制成具有可弹性变形的厚度和向内或向外弯曲的截面形状的尖端，而焊接到另一个臂的延伸部，该延伸部具有制成具有可弹性变形的厚度和向内弯曲的截面形状 或向外; 并且一个臂的末端的端面和另一个臂的延伸部的末端的端面保持彼此抵靠，使得当盘被一体化时两个端面可能被强制接触 相互防止冷却空气泄漏。

公开(公告)号：US5967746A

公开(公告)日：1999-10-19

申请号：US124058

申请日：1998-07-29

申请人： Naoki Hagi ,  Koichi Akagi

发明人： Naoki Hagi ,  Koichi Akagi

IPC分类号： F01D11/02 ,  F01D11/12 ,  F02C7/28 ,  F16J15/44

CPC分类号： F01D11/127 ,  F02C7/28 ,  F16J15/444

摘要： In order to realize a seal device of a gas turbine interstage portion which is excellent in a sealing ability during regular operation of the gas turbine, a gas turbine interstage portion seal device is constructed comprising a honeycomb seal (2) of a ring shape provided to an inner side of a turbine stationary blade inner ring (1) and a plurality of seal fins (5) of a ring shape provided to an outer side of a turbine disc seal arm portion (4). Also, an inner side surface of the honeycomb seal and outer peripheries of the plurality of seal fins, comprise large diameters and small diameters, and convex and concave portions formed thereby respectively are mated with each other.

摘要翻译： 为了实现燃气轮机的正常运行时的密封能力优异的燃气轮机级间部分的密封装置，构成了一种燃气轮机级间部分密封装置，包括蜂窝状密封件（2） 涡轮固定叶片内圈（1）的内侧和设置在涡轮盘密封臂部（4）的外侧的环形的多个密封翅片（5）。 此外，蜂窝状密封件的内侧表面和多个密封翅片的外周包括大直径和小直径，并且由此形成的凸凹部分彼此配合。

公开(公告)号：US5755622A

公开(公告)日：1998-05-26

申请号：US230797

申请日：1994-04-21

申请人： Hiroshi Kanki ,  Tadao Yashiki ,  Koichi Akagi ,  Taku Ichiryu

发明人： Hiroshi Kanki ,  Tadao Yashiki ,  Koichi Akagi ,  Taku Ichiryu

IPC分类号： F16D3/14 ,  F16D3/72 ,  F16D3/79 ,  F16D43/18 ,  F16D3/64

CPC分类号： F16D3/14 ,  F16D3/72 ,  F16D3/79 ,  F16D43/18

摘要： A vibration reducer for a diaphragm coupling is capable of suppressing axial vibrations as well as torsional vibrations. A diaphragm pack 3 is mounted between a diaphragm mount flange 2 provided on an intermediate shaft 1 serving as a drive shaft and a shaft flange 4 of another shaft serving as a driven shaft. An elastic arm 5 extends through the diaphragm pack 3 and is mounted to the diaphragm mount flange 2. The elastic arm 5 is a cylindrical member, whose circumferential portion is severed by slits formed by wire-cutting. Free ends 5a of the elastic arm 5 are expanded in the radial directions by centrifugal forces caused by rotation of a shafts and come into pressure-contact with the liner member 8 formed integrally within a cylindrical portion 7 of the shaft flange 4. A part of a torque is thereby transmitted via the pressure-contact portion, and rigidity in the axial direction of the elastic arm 5 is added to that of the diaphragm pack 3 to suppress vibrations. An alternative construction has a large pressure-contact force caused by centrifugal forces realized by making use of centrifugal weights 22, a centrifugal weight holder 23, and an elongated bolt 24.

摘要翻译： 用于隔膜联轴器的减振器能够抑制轴向振动以及扭转振动。 膜片组3安装在设置在用作驱动轴的中间轴1上的隔膜安装凸缘2和用作从动轴的另一个轴的轴凸缘4之间。 弹性臂5延伸穿过膜片组件3并安装在隔膜安装凸缘2上。弹性臂5是一圆柱形构件，其圆周部分被切线形成的狭缝切断。 弹性臂5的自由端5a通过由轴的旋转引起的离心力在径向方向上膨胀，并与与轴法兰4的圆柱形部分7中的整体形成的衬里构件8压力接触。 因此通过压力接触部分传递扭矩，并且将弹性臂5的轴向刚性添加到隔膜组件3的刚性以抑制振动。 替代结构具有由通过使用离心重物22，离心重量保持器23和细长螺栓24而实现的离心力引起的大的压力接触力。