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1. 发明申请

US20070271930A1 Gas turbine having cooling-air transfer system 审中-公开
标题翻译：具有冷却空气传输系统的燃气轮机
公开(公告)号：US20070271930A1
公开(公告)日：2007-11-29
申请号：US11416454
申请日：2006-05-03
申请人： Yoshimasa Takaoka , Masato Araki , Vincent Laurello , Masahito Kataoka , Junichiro Masada , Koichi Ishizaka , Naoki Hagi
发明人： Yoshimasa Takaoka , Masato Araki , Vincent Laurello , Masahito Kataoka , Junichiro Masada , Koichi Ishizaka , Naoki Hagi
IPC分类号： F02C7/12
CPC分类号： F01D5/06 , F01D5/082 , F01D5/084 , F01D5/085 , Y02T50/676
摘要： A gas turbine includes a cooling-air transfer system. The cooing-air transfer system extracts part of air discharged from a compressor to a chamber, and transfers the part of air as cooling air to a rotor disk. The cooling-air transfer system includes a plurality of tubular nozzles independently arranged in a circle inside the chamber to surround a rotor, and a seal disk having seal-disk cooling conduits arranged in a circle around the axis of the rotor so as to receive cooling air ejected from the tubular nozzles. The cooling-air transfer system swirls the cooling air ejected from the tubular nozzles.
摘要翻译：燃气轮机包括冷却空气输送系统。冷凝空气输送系统将从压缩机排出的空气的一部分提取到室，并将作为冷却空气的空气的一部分转移到转子盘。冷却空气传送系统包括多个管状喷嘴，其独立地设置在腔室内的圆周中以围绕转子;以及密封盘，其具有围绕转子轴线布置成圆形的密封盘冷却导管，以便接收冷却从管状喷嘴排出的空气。冷却空气传送系统使从管状喷嘴喷出的冷却空气旋转。

2. 发明申请

US20100303608A1 Two-shaft gas turbine 审中-公开
标题翻译：双轴燃气轮机
公开(公告)号：US20100303608A1
公开(公告)日：2010-12-02
申请号：US11528690
申请日：2006-09-28
申请人： Masahito Kataoka , Eisaku Ito , Vincent Laurello
发明人： Masahito Kataoka , Eisaku Ito , Vincent Laurello
IPC分类号： F01D1/24
CPC分类号： F01D25/162
摘要： A two-shaft gas turbine includes a high-pressure turbine having an annular gas-passage outlet, a low-pressure turbine having an annular gas-passage inlet, an annular intermediate duct that connects the gas-passage outlet to the gas-passage inlet, a bearing that supports a rotor of the high-pressure turbine and that is attached to a bearing case, and a plurality of struts that support the bearing case. The struts are arranged radially along the circumference of the bearing case so as to extend though the intermediate duct in a space between an outer peripheral surface of the bearing case and an inner peripheral surface of a casing wall that surrounds the intermediate duct. The intermediate duct has strut covers through which the struts extend and which function as first-stage stator blades for the low-pressure turbine.
摘要翻译：双轴燃气轮机包括具有环形气体通道出口的高压涡轮机，具有环形气体通道入口的低压涡轮机，将气体通道出口连接到气体通道入口的环形中间管道支撑高压涡轮机的转子并且附接到轴承箱的轴承以及支撑轴承箱的多个支柱。支柱沿着轴承箱的圆周径向布置，以便在轴承箱的外周表面和围绕中间管的壳体壁的内周表面之间的空间中延伸通过中间管道。中间管道具有支柱盖，支柱通过支柱延伸，并且用作低压涡轮机的第一级定子叶片。

3. 发明授权

US06773225B2 Gas turbine and method of bleeding gas therefrom 有权
标题翻译：燃气轮机及其气体渗出方法
公开(公告)号：US06773225B2
公开(公告)日：2004-08-10
申请号：US10156922
申请日：2002-05-30
申请人： Masanori Yuri , Vincent Laurello , Charles Ellis , Mitsuhiro Noguchi , Keita Fujii
发明人： Masanori Yuri , Vincent Laurello , Charles Ellis , Mitsuhiro Noguchi , Keita Fujii
IPC分类号： F01D518
CPC分类号： F01D5/08 , F01D11/005 , F01D11/02
摘要： In order to provide a gas turbine and a gas bleeding method which can prevent the loss of drive power due to gas bleeding to the rotor disk, bleed gas is imparted with swirling flow in the same rotational direction as that of a first stage rotor disk by being passed through a set of TOBI nozzles which constitute a flow conduit therefor, and is supplied to this first stage rotor disk, with a portion of this bleed gas flow being bypassed and being supplied between first stage stationary blades and first stage moving blades.
摘要翻译：为了提供一种能够防止由于气体向转子盘流出而引起的驱动力的损失的燃气轮机和排气方式，排出气体与第一级转子盘的旋转方向相同地旋转，通过一组构成其流动管道的TOBI喷嘴，并且被供应到该第一级转子盘，该排出气体流的一部分被旁路并被供应在第一级固定叶片和第一级动叶片之间。

4. 发明授权

US06732530B2 Gas turbine compressor and clearance controlling method therefor 有权
标题翻译：燃气轮机压缩机及其间隙控制方法
公开(公告)号：US06732530B2
公开(公告)日：2004-05-11
申请号：US10158062
申请日：2002-05-31
申请人： Vincent Laurello , Masanori Yuri
发明人： Vincent Laurello , Masanori Yuri
IPC分类号： F02C604
CPC分类号： F01D11/24 , F01D11/18 , F01D25/14 , F04D29/164 , F04D29/522 , F04D29/584
摘要： A plurality of moving blades are provided around rotor disks and rotate together with said rotor disks. Compressor rear case rings surround the periphery of these moving blades and form a compression flow path therein. A bleeding chamber is provided around the compressor rear case rings and introduces a portion of a main flow moving through the compression flow path as bleed air. Cooling flow path is formed between the compressor rear case rings and the bleeding chamber in which bleed air cf on its way to the bleeding chamber flows along the outer surface of the compressor rear case rings.
摘要翻译：在转子盘周围设有多个活动叶片，并与转子盘一起转动。压缩机后壳环围绕这些活动叶片的周边并在其中形成压缩流动路径。在压缩机后壳环周围设置有出血室，并且将作为流过压缩流路的主流的一部分作为排气引入。在压缩机后壳环和排气室之间形成有冷却流路，其中在其到排气室的途中的排出空气沿着压缩机后壳环的外表面流动。

5. 发明授权

US06655906B1 Axial compressor and gas bleeding method to thrust balance disk thereof 有权
标题翻译：轴向压缩机和排气方法推力平衡盘
公开(公告)号：US06655906B1
公开(公告)日：2003-12-02
申请号：US10156887
申请日：2002-05-30
申请人： Masanori Yuri , Vincent Laurello
发明人： Masanori Yuri , Vincent Laurello
IPC分类号： F01D302
CPC分类号： F01D5/082 , F01D3/02 , F01D11/04
摘要： In order to provide an axial compressor, and a gas bleeding method to the thrust balance disks thereof, which are capable of preventing reduction of the mechanical strength of the thrust balance disks due to excessive heating up by bleed gas, a portion of the fuel gas F, after having passed through the diffuser, is conducted to the thrust balance disks as the bleed gas flow c.
摘要翻译：为了提供一种轴向压缩机以及其推力平衡盘的排气方法，其能够防止由于排出气体的过度加热而导致的推力平衡盘的机械强度的降低，一部分燃料气体 F在通过扩散器之后，作为排气流c被传导到推力平衡盘。

6. 发明授权

US07033138B2 Ring segment of gas turbine 有权
标题翻译：燃气轮机的环段
公开(公告)号：US07033138B2
公开(公告)日：2006-04-25
申请号：US10235825
申请日：2002-09-06
申请人： Yasuoki Tomita , Osamu Isumi , Shinichi Inoue , Friedrich Soechting , Vincent Laurello , Hiroshige Matsuoka
发明人： Yasuoki Tomita , Osamu Isumi , Shinichi Inoue , Friedrich Soechting , Vincent Laurello , Hiroshige Matsuoka
IPC分类号： F01D25/08
CPC分类号： F01D25/12 , F01D11/005 , F01D11/08 , F01D25/246 , F05D2240/55 , F05D2260/201
摘要： An object of the present invention is to provide a ring segment of a gas turbine in which the temperature is maintained low, damage due to high temperature oxidation is prevented, and high temperature deformation is prevented. In order to achieve the object, the present invention provides a ring segment of a gas turbine which comprises a blade ring, a main shaft and moving blades comprising a plurality of individual units which define an annular form by being arranged around the peripheral direction of the main shaft, and disposed so that its inner peripheral surface is maintained at a constant distance from the tips of the moving blades, wherein grooves which extend along the axial direction of the main shaft of the turbine are formed upon of the individual units so as mutually to confront one another; a seal plate which is inserted into each mutually confronting pair of the grooves so as to connect together the adjacent pair of individual units; and contact surfaces which are formed at positions more radially inward than the seal plates, which extend in the axial direction and the peripheral direction and which mutually contact one another.
摘要翻译：本发明的目的是提供一种燃气轮机的环段，其中温度保持较低，防止了由于高温氧化引起的损坏，并且防止了高温变形。为了实现该目的，本发明提供了一种燃气轮机的环形段，其包括叶片环，主轴和包括多个独立单元的活动叶片，所述多个单独的单元通过围绕主轴，并且配置成使其内周面与动叶片的前端保持恒定的距离，其中沿涡轮主轴的轴向延伸的槽形成在各个单元上，以便相互相互对抗密封板，其插入每个相互面对的一对槽中，以将相邻的一对单独的单元连接在一起; 以及形成在比轴向和周向延伸并彼此相互接触的密封板更径向向内的位置处的接触表面。

7. 发明授权

US07017349B2 Gas turbine and bleeding method thereof 有权
标题翻译：燃气轮机及其排气方法
公开(公告)号：US07017349B2
公开(公告)日：2006-03-28
申请号：US10358336
申请日：2003-02-05
申请人： Vincent Laurello , Masanori Yuri
发明人： Vincent Laurello , Masanori Yuri
IPC分类号： F02C7/12 , F02C7/18
CPC分类号： F01D5/081 , F01D11/001 , F02C7/18 , F05D2260/2212
摘要： Bleeding is operated by annularly providing plural stationary blades at an interior side of a vehicle; annularly providing plural moving blades around rotor disk adjacent to stationary blades; providing plural stage units comprising the stationary and moving blades; introducing bleed air into each stage unit from a compressor; supplying bleed air extracted from a final stage of the compressor into a first stage unit; and supplying bleed air extracted from compressed air which has not yet arrived at a final stage unit of the compressor.
摘要翻译：出血通过在车辆的内侧环形地提供多个固定叶片来操作; 环形地在与固定叶片相邻的转子盘周围提供多个活动叶片; 提供包括固定和动叶片的多级单元; 将压缩空气引入各级单元; 将从压缩机的最后阶段提取的排放空气供应到第一级单元; 并且提供从还没有到达压缩机的最后级单元的压缩空气抽出的排出空气。

8. 发明授权

US06786488B2 Seal structure, turbine having the same, and leak-preventing seal system for rotating shaft 有权
标题翻译：密封结构，具有相同的涡轮，以及用于旋转轴的防漏密封系统
公开(公告)号：US06786488B2
公开(公告)日：2004-09-07
申请号：US10197581
申请日：2002-07-18
申请人： Vincent Laurello , Masanori Yuri
发明人： Vincent Laurello , Masanori Yuri
IPC分类号： F16J1544
CPC分类号： F01D11/00 , F02C7/28
摘要： In order to decrease gas leakage and in order to restrict the friction between the brush and the rotating shaft, a seal structure for a rotating shaft comprises a stator section, a rotating shaft, a groove, a brush, a spring member, and a connecting hole induces fluid pressure which presses the ring in a direction in which the ring approaches to the rotating shaft so as to be against the spring force of the spring member and make the brush contact the inner surface of the stator, the sealing structure prevents the fluid from flowing between the rotating shaft and the stator having a clearance from the surface of the rotating shaft and flowing in an axial direction of the rotating shaft.
摘要翻译：为了减少气体泄漏并且为了限制电刷和旋转轴之间的摩擦，用于旋转轴的密封结构包括定子部分，旋转轴，凹槽，电刷，弹簧部件和连接孔引起流体压力，该压力将环沿着旋转轴接近的方向按压，以抵抗弹簧构件的弹簧力，并使刷接触定子的内表面，密封结构防止流体在旋转轴和定子之间流动，具有与旋转轴的表面间隙并沿着旋转轴的轴向流动。

9. 发明授权

US06837676B2 Gas turbine 有权
标题翻译：燃气轮机
公开(公告)号：US06837676B2
公开(公告)日：2005-01-04
申请号：US10238651
申请日：2002-09-11
申请人： Masanori Yuri , Vincent Laurello , Satoshi Hada
发明人： Masanori Yuri , Vincent Laurello , Satoshi Hada
IPC分类号： F01D11/04 , F01D5/08 , F01D11/02 , F01D25/00 , F02C7/18 , F02C7/28 , F01D5/18
CPC分类号： F01D5/082 , F01D11/02 , F02C7/18
摘要： A sealing air bypass flow path is provided in a gas turbine for supplying sealing air to a sealing air supply flow path by bypassing the flow path between each tangential on board injection (TOBI) nozzles and disk holes.

10. 发明授权

US06659716B1 Gas turbine having thermally insulating rings 有权
标题翻译：具有隔热环的燃气轮机
公开(公告)号：US06659716B1
公开(公告)日：2003-12-09
申请号：US10195103
申请日：2002-07-15
申请人： Vincent Laurello , Masanori Yuri
发明人： Vincent Laurello , Masanori Yuri
IPC分类号： F01D1124
CPC分类号： F01D11/24
摘要： A gas turbine capable of minimizing the clearance between each of the rotor blades and partition ring, uses a structure in which the upstream thermally insulating ring is installed on the downstream blade ring.
摘要翻译：能够使每个转子叶片和分隔环之间的间隙最小化的燃气轮机使用其中上游绝热环安装在下游叶片环上的结构。

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