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1. 发明专利

JP2014020331A Turbine 有权
标题翻译：涡轮
公开(公告)号：JP2014020331A
公开(公告)日：2014-02-03
申请号：JP2012162098
申请日：2012-07-20
申请人： Toshiba Corp , 株式会社東芝
发明人： OKAMURA NAOYUKI , OKISONO NOBUHIRO , SATO IWATARO , TSURUTA KAZUTAKA , ONODA AKIHIRO
IPC分类号： F01K25/10 , F01D9/02 , F01D11/00 , F01D25/00 , F01D25/12
CPC分类号： F02C3/00 , F01D25/12 , F02C3/34 , F02C7/10 , F02C7/18 , F05D2210/12
摘要： PROBLEM TO BE SOLVED: To improve energy efficiency of a turbine.SOLUTION: The turbine of an embodiment, uses COas a working fluid and a refrigerant, and includes a working fluid transfer channel, a refrigerant transfer channel and a refrigerant recovery channel. The working fluid transfer channel allows the working fluid to be transferred from an upstream side toward a downstream side with respect to plural steps respectively composed of a pair of a stator vane and a rotor vane. The refrigerant transfer channel allows the refrigerant to be transferred from the upstream side toward the downstream side while passing through the inside of the stator vanes of every steps. The refrigerant recovery channel allows the refrigerant passing through the inside of the stator vane of a prescribed step to be recovered, and allows the recovered refrigerant to join the working fluid transfer channel at a step at the upstream side with respect to the prescribed step.
摘要翻译：要解决的问题：提高涡轮机的能源效率。实施例的涡轮机使用工作流体和制冷剂，并且包括工作流体输送通道，制冷剂输送通道和制冷剂回收通道。工作流体传递通道允许工作流体相对于分别由一对定子叶片和转子叶片构成的多个步骤从上游侧向下游侧传递。制冷剂输送通道允许制冷剂从上游侧向下游侧传递，同时通过每个步骤的定子叶片的内部。制冷剂回收通道允许通过规定步骤的定子叶片内部的制冷剂回收，并且允许回收的制冷剂在相对于规定步骤的上游侧的台阶处接合工作流体输送通道。

2. 发明专利

JP2015045246A ガスタービン設備有权
标题翻译：气体涡轮安装
公开(公告)号：JP2015045246A
公开(公告)日：2015-03-12
申请号：JP2013175933
申请日：2013-08-27
申请人：株式会社東芝 , Toshiba Corp
发明人： ITO MASAO , OKISONO NOBUHIRO , MAEDA HIDEYUKI , IWAI YASUNORI
IPC分类号： F02C3/30 , F01K25/00 , F02C3/05 , F02C3/34 , F02C7/00 , F02C9/40 , F23R3/00
CPC分类号： F02C3/34 , F01K19/10 , F02C1/08 , F02C3/04 , F02C6/18 , Y02E20/16 , Y02E20/322
摘要：【課題】タービン負荷が変化したときでも、燃焼器噴出速度を適正な範囲に維持し火炎安定が図れるガスタービン設備を提供する。【解決手段】実施形態のガスタービン設備10は、燃料と酸化剤を燃焼させる燃焼器20と、燃焼器20からの燃焼ガスで回動するタービン21と、燃焼ガスを冷却する熱交換器23と、熱交換器23を通過した燃焼ガスから水蒸気を除去してドライ作動ガスとする熱交換器24と、ドライ作動ガスを超臨界流体となるまで昇圧する圧縮機25とを備える。また、圧縮機25からのドライ作動ガスの一部を、熱交換器23を通して燃焼器20に導く配管42と、熱交換器23よりも上流側の配管42から分岐し、ドライ作動ガスの一部を外部に排出する配管44と、圧縮機25から排出されたドライ作動ガスの残部をタービン21の出口と熱交換器23の入口とを連結する配管40内に導入する配管45とを備える。【選択図】図1
摘要翻译：要解决的问题：提供能够将燃烧室喷射速度保持在适当范围内的燃气轮机装置，即使随着涡轮机负荷的变化也能实现火焰稳定性。解决方案：根据实施例的燃气轮机装置10包括：燃烧室20 燃烧燃料和氧化剂; 与来自燃烧室20的燃烧气体一起旋转的涡轮机21; 冷却燃烧气体的热交换器23; 热交换器24，其从通过热交换器23的燃烧气体除去蒸气，生成干燥工作气体; 以及增加干燥工作气体的压力以产生超临界流体的压缩机25。燃气轮机装置10还包括：管42，通过热交换器23将来自压缩机25的干燥工作气体的一部分引入燃烧室20; 从热交换器23上游的管42分支的管44，将一部分干燥工作气体排出到外部; 以及从压缩机25排出的干燥工作气体的其余部分的导管45连接到将涡轮机21的出口与热交换器23的入口连接的管道40中。

3. 发明专利

JP2014020327A Labyrinth seal part and turbine 有权
标题翻译： LABYRINTH密封件和涡轮
公开(公告)号：JP2014020327A
公开(公告)日：2014-02-03
申请号：JP2012161943
申请日：2012-07-20
申请人： Toshiba Corp , 株式会社東芝
发明人： MAEDA HIDEYUKI , WADA KUNIHIKO , OKISONO NOBUHIRO , SATO IWATARO , TSURUTA KAZUTAKA , OKAMURA NAOYUKI
IPC分类号： F01D11/02 , C23C4/08 , C23C4/18 , F01D11/08 , F01D25/00 , F01D25/08 , F02C7/00 , F02C7/28 , F16J15/453
摘要： PROBLEM TO BE SOLVED: To reduce a leak of working fluid between facing components in a turbine and prevent a leak increase caused by thinning damage.SOLUTION: A labyrinth seal part has a member including fins which are attached to a base material of a stationary part provided by facing a rotary part of a turbine and composed of ceramic material, the fins extending toward the rotary part.
摘要翻译：要解决的问题：减少涡轮机的面对部件之间的工作流体的泄漏，并防止由变薄的损伤引起的泄漏增加。解决方案：迷宫式密封部件具有包括翅片的构件，翅片附接到固定部件的基材通过面对涡轮机的旋转部分并由陶瓷材料构成，翅片朝向旋转部分延伸。

4. 发明专利

JP2014020329A Co2 turbine, method of manufacturing co2 turbine, and power generation system 有权
标题翻译：二氧化碳涡轮机，制造二氧化碳涡轮机的方法和发电系统
公开(公告)号：JP2014020329A
公开(公告)日：2014-02-03
申请号：JP2012162096
申请日：2012-07-20
申请人： Toshiba Corp , 株式会社東芝
发明人： WADA KUNIHIKO , KUBOTANI SATORU , SAITO DAIZO , OKISONO NOBUHIRO , SATO IWATARO , TSURUTA KAZUTAKA
IPC分类号： F01D11/08 , C23C28/00 , F01D11/02 , F01D25/00 , F01K25/10 , F02C3/22 , F02C7/00 , F02C7/28 , F16J15/453
摘要： PROBLEM TO BE SOLVED: To provide a COturbine which is superior in reliability on a seal part and improved in performance.SOLUTION: A COturbine includes a stationary part, a rotary part, and a seal part for reducing a combustion gas leaking from a gap between opposite parts of the stationary part and rotary part, and rotates the rotary part with a combustion gas produced by burning a fuel including mixed CO. The seal part has a ceramic layer, having lower thermal conductivity than a formed member as one member selected between the stationary part and rotary part and also having its surface made uneven, formed on the formed member, and has a structure in which the formed member and the opposite member as the other member never come into contact with each other, or a structure in which a surface of the opposite member is lower in hardness than the ceramic layer and preferentially ground in contacting.
摘要翻译：要解决的问题：提供一种在密封部件上的可靠性优异并且性能提高的混合机。解决方案：一种涡轮机包括固定部件，旋转部件和密封部件，用于减少从第二固定部分和旋转部分的相对部分，并且通过燃烧包含混合CO的燃料产生的燃烧气体旋转旋转部分。密封部分具有陶瓷层，其具有比成形部件低的热导率，固定部分和旋转部分，并且其表面形成不均匀，形成在成形构件上，并且具有其中成形构件和作为另一个构件的相对构件彼此不会接触的结构，或者其中相对构件的表面的硬度低于陶瓷层，并优先接地。

5. 发明专利

JP2004245460A Tail pipe for gas turbine combustor 审中-公开
公开(公告)号：JP2004245460A
公开(公告)日：2004-09-02
申请号：JP2003033908
申请日：2003-02-12
申请人： Toshiba Corp , 株式会社東芝
发明人： ITO HIROYUKI , SUZUKI NOBUHISA , OKAMOTO HIROAKI , OKISONO NOBUHIRO
IPC分类号： F23R3/42 , F02C7/18
摘要： PROBLEM TO BE SOLVED: To provide a tail pipe for a gas turbine combustor easy to disassemble/reassemble when assembling, inspecting or repairing an outer tube of the tail pipe for the gas turbine combustor.
SOLUTION: The tail pipe for the gas turbine combustor for guiding combustion gas from a combustor liner through an inner tube to a gas turbine has a double tube structure of covering the inner tube via a cooling passage with the outer tube. The outer tube is divided into a plurality of parts to form outer tube divided pieces in the shape of holding the inner tube between both sides. Fixing members are provided near mating portions of the outer tube divided pieces, joint members are mounted between the fixing members, and the fixing members and the joint members are fixed together to make the outer tube divided pieces into one unit.
COPYRIGHT: (C)2004,JPO&NCIPI

6. 发明专利

JP2014066145A Component for turbine, turbine, and method for manufacturing component for turbine 有权
标题翻译：涡轮机组件，涡轮机及其制造方法
公开(公告)号：JP2014066145A
公开(公告)日：2014-04-17
申请号：JP2012210495
申请日：2012-09-25
申请人： Toshiba Corp , 株式会社東芝
发明人： SAITO DAIZO , WADA KUNIHIKO , OKISONO NOBUHIRO , SATO IWATARO , TSURUTA KAZUTAKA , OKITA NOBUO
IPC分类号： F01D25/00 , F01D5/02 , F01D5/28 , F01D9/02 , F01D25/24 , F02C7/00
摘要： PROBLEM TO BE SOLVED: To provide a component for a turbine whose surface is restrained from deterioration.SOLUTION: A component for a turbine in an embodiment is a constituting component for a turbine. The component for a turbine in an embodiment has a component body, and an oxidation protective film provided on a surface of the component body. The component body is made of an Ni-group superalloy, a Co-group superalloy, or an Fe-group superalloy. The oxidation protective film is provided on at least one surface selected from an outer surface and an inner surface of the component body. Also, the oxidation protective film is formed by oxidizing the surface of the component body.
摘要翻译：要解决的问题：提供一种表面被抑制劣化的涡轮机的部件。解决方案：一个实施例中的涡轮机部件是涡轮机的组成部件。在一个实施例中的涡轮机的部件具有组件主体和设置在组件主体的表面上的氧化保护膜。组件主体由Ni基超合金，Co族超合金或Fe族超合金制成。氧化保护膜设置在选自组件主体的外表面和内表面的至少一个表面上。而且，通过氧化组分体的表面形成氧化保护膜。

7. 发明专利

JP2014020330A Turbine 有权
标题翻译：涡轮
公开(公告)号：JP2014020330A
公开(公告)日：2014-02-03
申请号：JP2012162097
申请日：2012-07-20
申请人： Toshiba Corp , 株式会社東芝
发明人： TSURUTA KAZUTAKA , OKISONO NOBUHIRO , SATO IWATARO , MAEDA HIDEYUKI , OKAMURA NAOYUKI
IPC分类号： F02C7/28 , F01D11/04 , F01D25/00 , F01D25/16 , F02C7/18 , F16J15/36 , F16J15/447
摘要： PROBLEM TO BE SOLVED: To provide a turbine capable of reducing leakage of a cooling medium from an end portion of a casing at low costs.SOLUTION: The turbine using a working medium for rotating a turbine rotor, and COas a cooling medium, has a casing and a mechanical seal. The casing has a first cooling chamber to which COfor cooling or sealing, to cool or seal the turbine, is injected at a prescribed temperature and a prescribed pressure, a second cooling chamber which is decompressed with respect to a pressure of the first cooling chamber and to which the cooling medium is injected, and a through hole for making the turbine rotor penetrate to the external through the second cooling chamber. The mechanical seal seals a clearance gap between the turbine rotor penetrating through the through hole and an opening portion to the external, of the through hole of the casing while permitting rotation of the turbine rotor.
摘要翻译：要解决的问题：提供一种能够以低成本从壳体的端部减少冷却介质的泄漏的涡轮机。解决方案：使用用于旋转涡轮机转子的工作介质的涡轮机，以及COas冷却介质，具有套管和机械密封。壳体具有第一冷却室，用于冷却或密封的CO，用于冷却或密封涡轮，在规定的温度和规定的压力下被注入，第二冷却室相对于第一冷却室的压力被减压，喷射冷却介质的通孔和用于使涡轮机转子通过第二冷却室渗透到外部的通孔。机械密封件密封涡轮机转子穿过通孔和壳体的通孔的外部的开口部分之间的间隙，同时允许涡轮转子旋转。

8. 发明专利

JP2014020326A Turbine and method for cooling turbine 有权
标题翻译：用于冷却涡轮的涡轮机和方法
公开(公告)号：JP2014020326A
公开(公告)日：2014-02-03
申请号：JP2012161942
申请日：2012-07-20
申请人： Toshiba Corp , 株式会社東芝
发明人： MAEDA HIDEYUKI , OKISONO NOBUHIRO , SATO IWATARO , TSURUTA KAZUTAKA , OKAMURA NAOYUKI
IPC分类号： F02C7/18 , F01D25/12 , F01D25/24 , F01K25/10 , F02C7/16
摘要： PROBLEM TO BE SOLVED: To allow a turbine to be driven efficiently.SOLUTION: The turbine that uses COas a cooling fluid comprises: a casing constituting a stationary part of the turbine; and a stationary blade mounted to the casing and having a cooling passage inside which the cooling fluid flows. The stationary blade includes an extension part having a cooling passage inside which the cooling fluid flows and provided with a feature as a shroud segment. The stationary blade is configured so that at least part of the cooling fluid flowing through the cooling passage of the stationary blade flows into the cooling passage of the extension part.
摘要翻译：要解决的问题：为了有效地驱动涡轮机。解决方案：使用COas冷却流体的涡轮包括：构成涡轮的静止部分的壳体; 以及固定刀片，其安装在所述壳体上，并具有冷却流体流过所述冷却通道。固定叶片包括具有冷却通道的延伸部分，冷却流体流过冷却通道，并且具有作为护罩段的特征。固定叶片被构造成使得流过静止叶片的冷却通道的冷却流体的至少一部分流入延伸部分的冷却通道。

9. 发明专利

JP2014020325A Turbine and method for operating turbine 有权
标题翻译：用于运行涡轮机的涡轮机和方法
公开(公告)号：JP2014020325A
公开(公告)日：2014-02-03
申请号：JP2012161941
申请日：2012-07-20
申请人： Toshiba Corp , 株式会社東芝
发明人： MAEDA HIDEYUKI , TAJIMA TSUGUHISA , IWAI SHOGO , OKISONO NOBUHIRO , SATO IWATARO , TSURUTA KAZUTAKA , OKAMURA NAOYUKI
IPC分类号： F01D3/04 , F01D11/04 , F01K9/00 , F01K25/10
CPC分类号： F01D3/04 , F01D11/04 , F01D25/168 , F01D25/26 , F02C1/08 , F02C3/34 , F05D2260/61
摘要： PROBLEM TO BE SOLVED: To operate a turbine efficiently by a simple configuration.SOLUTION: A single-flow type turbine using COas a working fluid includes a balance piston part that optimizes an axial load of a rotor with respect to a bearing by using a fluid that has a lower temperature than that of the working fluid introduced into the turbine. The turbine is provided with a flow pass that extracts at least part of the fluid passing through the balance piston part from the middle of the part and allows at least part of the extracted fluid to flow into the middle of a passage through which the working fluid passes, and which comprises a plurality of stages of moving blades.
摘要翻译：要解决的问题：通过简单的结构有效地运行涡轮机。解决方案：使用COas工作流体的单流型涡轮机包括平衡活塞部件，其通过使用流体优化转子相对于轴承的轴向载荷其温度低于引入涡轮机的工作流体的温度。涡轮机设置有流道，其从部件的中间抽取通过平衡活塞部件的至少一部分流体，并允许至少部分提取的流体流入通道的中间，通过该通道中的工作流体通过，并且其包括多级的动叶片。

10. 发明专利

JPS5943928A Gas turbine generator 失效
标题翻译：气体涡轮发电机
公开(公告)号：JPS5943928A
公开(公告)日：1984-03-12
申请号：JP15253482
申请日：1982-09-03
申请人： Toshiba Corp
发明人： OKISONO NOBUHIRO
IPC分类号： F02C6/00 , F02C3/22 , F02C7/00
CPC分类号： F02C3/22
摘要： PURPOSE:To improve the total efficiency by coupling a gas turbine using liquidized gas as fuel, Rankine cycle turbine and a small generator through a clutch while condensing the exhaust gas from Rankine cycle turbine through liquidized gas. CONSTITUTION:LNG fed from LNG tank 1 and boosted by a pump 2 will enter into a condenser 3 to condense the exhaust gas from Rankine cycle turbine A employing low boiling point intermediate medium. LNG from a control valve 4 is evaporated in LNG evaporator 8 and enter into a combustor 5. While the condensed intermediate medium is boosted by a pump 9 and enter into a turbine A to perform a work. Upon start of turbine the clutch 17 is coupled while upon completion of start the clutch 11 is coupled. Consequently a starter is not required while the cooling heat of LNG can be utilized effectively.
摘要翻译：目的：通过使用作为燃料的液化气体的燃气轮机，兰金循环涡轮机和通过离合器的小型发电机连接来提高总效率，同时通过液化气体浓缩来自兰金循环涡轮机的废气。构成：从LNG罐1供给并由泵2加压的LNG将进入冷凝器3，以冷凝来自使用低沸点中间介质的兰金循环涡轮机A的废气。来自控制阀4的LNG在LNG蒸发器8中蒸发并进入燃烧器5.当冷凝的中间介质被泵9升压并进入涡轮机A进行作业时。在涡轮机启动时，离合器17联接，而在启动完成时，离合器11联接。因此，不需要起动器，而可以有效利用LNG的冷却热。

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