专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明专利

JP2013072316A Transition piece of combustor, gas turbine having the same, and method for manufacturing transition piece 有权
标题翻译：燃气轮机的过渡部件，具有其的燃气轮机，以及制造过渡部件的方法
公开(公告)号：JP2013072316A
公开(公告)日：2013-04-22
申请号：JP2011210710
申请日：2011-09-27
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： HANEDA SATORU , NAKAMURA SOSUKE , TANAKA KATSUNORI , AKAGI KOICHI , KONISHI SATORU , SHIBATA HIROKI
IPC分类号： F02C7/18 , F01D25/12 , F02C7/00 , F23R3/42
CPC分类号： F01D9/023 , F23R3/002 , F23R3/005 , F23R3/60 , F23R2900/00017 , F23R2900/00018 , F23R2900/03043
摘要： PROBLEM TO BE SOLVED: To provide a transition piece of combustor capable of enduring conditions with a more severe thermal environment.SOLUTION: The transition piece 20 of combustor includes: a tubular trunk body 21; a tubular outlet trunk 32 which is joined to the downstream end of the trunk body and which forms a trunk B in cooperation with the trunk body; and an inner flange 36 which extends from the downstream end of the outlet trunk toward the outer peripheral side of the outlet trunk. The outlet trunk 32 and the inner flange 36 are formed as an integrated member. In the outlet trunk 32, a groove 35 is formed on the upstream side of the inner flange at a position along the inner flange, being recessed from the outer peripheral side to the inner peripheral side and extending in the circumferential direction. Further, in the outlet trunk 32, a cooling fluid path 33 is formed, extending along an axis Ac of the trunk B, and opening to the groove.
摘要翻译：要解决的问题：提供一种能够具有更严格的热环境的耐久条件的燃烧器的过渡片。解决方案：燃烧器的过渡件20包括：管状主体21; 管状出口主干32，其与躯干主体的下游端连接并与躯干主体配合形成躯干B. 以及从出口主干的下游端向出口主干的外周侧延伸的内凸缘36。出口主干32和内凸缘36形成为一体的构件。在出口主干32中，在内凸缘的上游侧，沿着内凸缘的位置，在外周侧向内周侧凹陷并沿圆周方向延伸形成有槽35。此外，在出口主干32中，形成有沿着树干B的轴线Ac延伸并且向槽开口的冷却流体路径33。版权所有（C）2013，JPO＆INPIT

2. 发明专利

JP2010261318A Method of manufacturing plate-shaped body, plate-shaped body, gas turbine combustor, and gas turbine 有权
标题翻译：制造板形体，板形体，气体涡轮机和气体涡轮机的方法
公开(公告)号：JP2010261318A
公开(公告)日：2010-11-18
申请号：JP2009110510
申请日：2009-04-30
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： MORIMOTO HITOSHI , KAMIYOSHI SHUSUKE , ISHIGURO TATSUO , SHIBATA HIROKI , KONISHI SATORU , SATO KENJI
IPC分类号： F02C7/18 , B23K26/20 , F01D25/00 , F01D25/12 , F02C7/00 , F23R3/10 , F23R3/42
CPC分类号： B23K26/30 , B23K1/0018 , B23K2201/001 , F01D9/023 , F23R3/005 , F23R3/42 , F23R2900/00017 , F23R2900/00018 , Y02T50/67 , Y02T50/675 , Y10T29/49826 , Y10T29/49893 , Y10T428/12493
摘要： PROBLEM TO BE SOLVED: To provide a manufacturing method of a plate-shaped body, the plate-shaped body, a gas turbine combustor and a gas turbine, capable of preventing the deterioration in a work environment, by shortening time required for manufacturing the gas turbine combustor, by restraining reduction in cooling performance. SOLUTION: This manufacturing method of the plate-shaped body 33 comprises a process of laminating a plurality of plates 41 and 42 and forming the plate-shaped bodies 33U and 33R of juxtaposing a plurality of flow passages 51 and 52 for flowing a cooling medium between the plurality of plates 41 and 42, and a process of juxtaposing a plurality of plate-like bodies 33U and 33R in the juxtaposed direction of the flow passages 51 and 52, butting and arranging the plurality of plate-shaped bodies 33U and 33R and welding in butting parts 63 and 63, and is characterized in that the flow passage 52 adjacent to the butting parts 63 and 63 extends along the butting parts 63, and is longer in a dimension in the juxtaposed direction of the flow passages 51 and 52 than the flow passage 51 except for that. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：为了提供能够防止工作环境恶化的板状体，板状体，燃气轮机燃烧器和燃气轮机的制造方法，通过缩短所需的时间通过抑制冷却性能的降低来制造燃气轮机燃烧器。解决方案：板状体33的这种制造方法包括层叠多个板41和42并且形成并排多个流动通道51和52的板状体33U和33R以使流动的板状体多个板41和42之间的冷却介质，以及沿着流动通道51和52的并置方向并置多个板状体33U和33R的工序，将多个板状体33U和 33R，并且在对接部63,63中进行焊接，其特征在于，与对接部63,63相邻的流路52沿着对接部63延伸，并且在流路51的并列方向上的尺寸更长， 52除了流路51以外。版权所有（C）2011，JPO＆INPIT

3. 发明专利

JP2012189495A Sensor attaching structure 有权
标题翻译：传感器连接结构
公开(公告)号：JP2012189495A
公开(公告)日：2012-10-04
申请号：JP2011054237
申请日：2011-03-11
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： HARUTA HIDEKI , SHIBATA HIROKI , IZUTSU NOBUYUKI
IPC分类号： G01L19/00
摘要： PROBLEM TO BE SOLVED: To provide a sensor attaching structure capable of fixing sensor means in an optimum fixing state, preventing looseness of the sensor means and preventing fastening between the sensor means and a sensor attaching wall part.SOLUTION: A sensor attaching structure A includes: a sensor insertion hole 20 pierced through a sensor attaching wall part 17 and having a diameter reduction part 21 whose inner diameter is reduced from the outside to the inside on its intermediate part; a sensor holder 30 inserted from the outside into the sensor insertion hole 20, abutting on the diameter reduction part 21 and positioned in an axial direction to fix sensor means 15 on a sensor holding hole 37 formed on its shaft center part; and a pressing sleeve 50 for pressing only the sensor holder 30 in the axial direction by being screwed into the sensor insertion hole 20 following the sensor holder 30 and pressing the sensor holder 30 against the diameter reduction part 21 of the sensor insertion hole 20. The sensor means 15 is screwed into the sensor holding hole 37 in optimum fastening torque and looseness of the sensor means 15 is prevented by a detent member 60.
摘要翻译：要解决的问题：提供一种能够将传感器装置固定在最佳固定状态的传感器安装结构，防止传感器装置的松动，并防止传感器装置与传感器安装壁部之间的紧固。传感器安装结构A包括：穿过传感器安装壁部17的传感器插入孔20，并且在其中间部分具有内径从外部减小到内部的直径减小部21; 传感器保持件30从外部插入到传感器插入孔20中，抵接在直径减小部21上并沿轴向定位，以将传感器装置15固定在形成在其轴心部分上的传感器保持孔37上; 以及按压套筒50，用于按照传感器保持器30旋入到传感器插入孔20中，并且将传感器保持器30按压在传感器插入孔20的直径减小部分21上，从而沿轴向仅按压传感器保持器30。传感器装置15以最佳的紧固扭矩拧入传感器保持孔37中，传感器装置15的松动由止动构件60阻止。（C）2013，JPO＆INPIT

4. 发明专利

JP2004301115A Sealing construction and sealing device of turbine tail pipe 有权
公开(公告)号：JP2004301115A
公开(公告)日：2004-10-28
申请号：JP2003327636
申请日：2003-09-19
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： SHIBATA HIROKI , TANAKA KATSUNORI , NAKANE HIDEHIKO
IPC分类号： F01D25/00 , F01D25/24 , F02C7/28 , F16J15/08 , F23R3/42
摘要： PROBLEM TO BE SOLVED: To provide the sealing construction of a turbine tail pipe and a sealing device for general purpose which are markedly excellent in sealing performance.
SOLUTION: In the sealing structure of the turbine tail pipe, clearance between turbine tail pipes is blocked with an edge surface of the sealing device 10, in which a plurality of long quadrilateral thin plates are laminated to bundle and fix the other long side. The clearance between a turbine tail pipe 5 and a shroud 6 is blocked with the thin plate flat surface of the sealing device 10, in which a plurality of long quadrilateral thin plates are laminated to bundle and fix the other long side.
COPYRIGHT: (C)2005,JPO&NCIPI

5. 发明专利

JP2961089B2 Gas turbine 1-stage vane seal structure 失效
公开(公告)号：JP2961089B2
公开(公告)日：1999-10-12
申请号：JP14773597
申请日：1997-06-05
申请人：三菱重工業株式会社
发明人： TANAKA MIKI , ICHANAGI TAKU , AKAGI KOICHI , SHIBATA HIROKI , SAKAGUCHI TADAKAZU
IPC分类号： F01D9/04 , F01D9/02 , F01D11/00 , F01D11/04 , F02C7/18 , F02C7/28
CPC分类号： F01D9/02 , F01D11/005 , F02C7/18 , Y02T50/675

6. 发明专利

JPH10339108A GAS TURBINE FIRST STAGE STATIONARY BLADE SEAL STRUCTURE 失效
公开(公告)号：JPH10339108A
公开(公告)日：1998-12-22
申请号：JP14773597
申请日：1997-06-05
申请人： MITSUBISHI HEAVY IND LTD
发明人： TANAKA MIKI , ICHIYANAGI TAKU , AKAGI KOICHI , SHIBATA HIROKI , SAKAGUCHI TADAKAZU
IPC分类号： F01D9/04 , F01D9/02 , F01D11/00 , F01D11/04 , F02C7/18 , F02C7/28
摘要： PROBLEM TO BE SOLVED: To prevent leakage of sealing air from the inside of a first stage stationary blade by notching a part contacting with a stationary blade support ring in a straight line shape in both lower end parts of a circular arc shape of a flange, and notching a part contacting with a flange side surface in a straight line shape in a circumferential end part of the stationary blade support ring. SOLUTION: A recess part 24 is formed on the circumferential end part of a circular stationary blade support ring 23 by respectively notching a part with which a rear flange 22 of a stationary blade 31 comes into contact. A recess 25 is also respectively formed in the rear flange 22. That is, the recess part 25 is formed in the rear flange 22 of the stationary blade 31, and a seal structure by combining this rear flange 22 and the stationary blade support ring 23 having the recessed part 24 is adopted. Therefore, even if blades relatively fall down in a first stage stationary blade 31 by thermal stress, a seal surface can be reliably held without generating a clearance on a contact surface, and leakage of sealing air from the inside can be prevented.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式