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. 发明授权

US08353663B2 Shroud seal segments arrangement in a gas turbine 有权
标题翻译：护罩密封段布置在燃气轮机中
公开(公告)号：US08353663B2
公开(公告)日：2013-01-15
申请号：US13011203
申请日：2011-01-21
申请人： Tanguy Arzel , Thomas Heinz-Schwarzmaier , Martin Schnieder
发明人： Tanguy Arzel , Thomas Heinz-Schwarzmaier , Martin Schnieder
IPC分类号： F04D29/38
CPC分类号： F01D11/24 , F01D5/08 , F01D11/08 , F01D25/12 , F05D2240/11 , F05D2260/201 , F05D2260/202 , F05D2260/205
摘要： A gas turbine is provided that includes a rotor which is rotatable around an axis and equipped with rotor blades, and which is concentrically enclosed at a distance by a casing, which is equipped with stator blades, forming an annular hot gas passage. Rings with stator blades and rotor blades are arranged in a manner alternating in the axial direction. Between adjacent stator blades, heat shield segments are arranged, which delimit the hot gas passage on the outside in a region of the rotor blades and are cooled by impingement cooling where a cooling medium from an outer annular cavity flows into the heat shield segment.
摘要翻译：提供了一种燃气轮机，其包括能够绕轴线旋转并且配备有转子叶片的转子，并且由配置有定子叶片的壳体一定距离同心地封闭，该壳体形成环形的热气体通道。具有定子叶片和转子叶片的环以轴向交替排列。在相邻的定子叶片之间，布置有隔热板段，其在转子叶片的区域中限定外部的热气体通道，并且通过来自外部环形空腔的冷却介质流入隔热板段的冲击冷却来冷却。

2. 发明授权

US08303257B2 Shiplap arrangement 有权
标题翻译： Shiplap安排
公开(公告)号：US08303257B2
公开(公告)日：2012-11-06
申请号：US12572034
申请日：2009-10-01
申请人： Thomas Heinz-Schwarzmaier , Ulrich Rathmann , Carlos Simon-Delgado
发明人： Thomas Heinz-Schwarzmaier , Ulrich Rathmann , Carlos Simon-Delgado
IPC分类号： F01D11/02 , F01D5/22
CPC分类号： F01D11/02 , F01D11/005 , F01D11/04 , F05D2240/57
摘要： An arrangement between blade elements in a blade row in a turbine is described. Each blade element has at least one shroud element and a blade airfoil which abuts on, and is connected to, the shroud element, and essentially extends radially with regard to a principal axis of the blade row. When installed, the shroud element sides, which extend circumferentially, abut on the respectively adjacent shroud element of the respectively adjacent blade element, each forming an essentially radial gap. At least one blade element has a projection which projects into the shroud element of the abutting blade element and extends in the circumferential direction, and at least one blade element has a recess which accommodates such a projection. In the region of the projection or recess there is a stepped region of the radial gap, and the guiding of the radial gap in this stepped region is a labyrinth seal.
摘要翻译：描述了涡轮机中的叶片排中的叶片元件之间的布置。每个叶片元件具有至少一个护罩元件和叶片翼型件，其抵靠并连接到护罩元件，并且基本上相对于叶片排的主轴线径向延伸。当安装时，沿周向延伸的护罩元件侧邻接在相邻的相邻叶片元件的相邻的护罩元件上，每个形成基本上径向的间隙。至少一个叶片元件具有突出部，其突出到邻接叶片元件的护罩元件中并沿周向延伸，并且至少一个叶片元件具有容纳这种突起的凹部。在突起或凹槽的区域中，存在径向间隙的台阶区域，并且在该阶梯区域中的径向间隙的引导是迷宫式密封。

3. 发明授权

US07562934B2 Apparatus and method for configurable seating 失效
标题翻译：用于可配置座位的装置和方法
公开(公告)号：US07562934B2
公开(公告)日：2009-07-21
申请号：US11222054
申请日：2005-09-08
申请人： David Swan , Thomas Heinz-Gerd Preiss , Robert J. McMillen
发明人： David Swan , Thomas Heinz-Gerd Preiss , Robert J. McMillen
IPC分类号： A47C3/00 , A47C7/02 , A47C7/14 , A47C4/54
CPC分类号： B60N2/914 , B60N2/99
摘要： A configurable vehicle seat having at least two configurations is disclosed. The configurable vehicle seat has a seat base, a seat bottom supported by the seat base, and a seat back coupled to the seat base. The seat back or seat bottom has one or more adjustable profile members, wherein the adjustable profile members may be adjusted such that the seat is adjusted from at least a first configuration to a second configuration.
摘要翻译：公开了具有至少两种配置的可配置车辆座椅。可配置车辆座椅具有座椅底座，由座椅底座支撑的座椅底座和联接到座椅底座的座椅靠背。座椅靠背或座椅底部具有一个或多个可调节的轮廓构件，其中可调整的轮廓构件可以被调节为使得座椅从至少第一构型调整到第二构造。

4. 发明授权

US08534675B2 Strip seal and method for designing a strip seal 有权
标题翻译：带状密封和设计带状密封的方法
公开(公告)号：US08534675B2
公开(公告)日：2013-09-17
申请号：US12694765
申请日：2010-01-27
申请人： Thomas Heinz-Schwarzmaier , Ulrich Steiger , Ulrich Rathmann
发明人： Thomas Heinz-Schwarzmaier , Ulrich Steiger , Ulrich Rathmann
IPC分类号： F16J3/00
CPC分类号： F01D11/005 , F01D25/04 , F05D2240/11 , F05D2240/57 , F05D2260/96 , F05D2300/501
摘要： A strip seal and method of configuration thereof for sealing two adjacent non-rotating gas turbine hot gas components exposed to pressure pulsations. The strip seal has at least two clamping projections distributed along discrete points of the strip seal length that extend out from a pressure face of the strip seal. The location of the projections are defined by two ratios. The first ratio, of less than 25, is the strip seal length extending free of clamping projections from any one of the ends of the strip seal to a clamping projection to the ratio of strip seal thickness. The second ratio, of less than 200, is the ratio of the strip seal length extending free of clamping projections between any two projections to the thickness of the strip seal. This seal arrangement ameliorates detrimental effects of induced resonance.
摘要翻译：一种带状密封件及其构造方法，用于密封暴露于压力脉动的两个相邻的非旋转燃气轮机热气体组件。带状密封件具有沿带状密封件长度的离散点分布的至少两个夹紧突起，其从带状密封件的压力表面延伸出来。突起的位置由两个比例定义。小于25的第一比率是从带状密封件的任何一个端部延伸到没有夹紧突起的条形密封长度到夹紧突起到条形密封件厚度的比率。小于200的第二比率是在任何两个突起之间没有夹紧突起的条形密封长度与带状密封件的厚度之间的比率。该密封装置改善了诱导共振的有害影响。

5. 发明申请

US20130233424A1 LIQUID DISTRIBUTOR OF MODULAR CONSTRUCTION 审中-公开
标题翻译：模块化建筑液体分配器
公开(公告)号：US20130233424A1
公开(公告)日：2013-09-12
申请号：US13756440
申请日：2013-01-31
申请人： Markus FREY , Axel GERLACH , Thomas HEINZ , Thomas VON OLNHAUSEN
发明人： Markus FREY , Axel GERLACH , Thomas HEINZ , Thomas VON OLNHAUSEN
IPC分类号： F17D1/08
CPC分类号： F17D1/084 , F16K11/22 , F16K27/003 , F24D3/1075 , F24T10/10 , Y02E10/12 , Y10T137/86911
摘要： A geothermal plant brine distributor includes a plurality of distributor modules which are detachably connected to each other and are arranged in series behind one another forming a continuous main line. A connector module is connectable to a distributor supply line or distributor return line and also to the distributor modules. Each distributor module includes a housing of plastic material including a main line section, each end of which is surrounded by one connector flange, a pipe-shaped valve stem which branches off from the lateral surface side of the main line section and has a side opening, and a branch pipe that joins the side opening of the valve stem. A hollow cylinder valve body is rotatable in the valve stem for closing or opening fluid flow from the main line to the branch pipe.
摘要翻译：地热设备盐水分配器包括多个分配器模块，它们彼此可拆卸地连接并且彼此串联排列，形成连续主线。连接器模块可连接到分配器供应管线或分配器返回管线以及分配器模块。每个分配器模块包括塑料材料壳体，该壳体包括主线段，每个端部由一个连接器凸缘包围，管状阀杆从主线段的侧面侧分支并具有侧开口，以及连接阀杆的侧开口的分支管。中空圆柱阀体可在阀杆中旋转，用于关闭或打开从主管线到分支管道的流体流动。

6. 发明申请

US20120097586A1 Device for filtering and deaeration of fuel oil with return changeover valve 审中-公开
标题翻译：具有返回切换阀的燃油过滤和脱气装置
公开(公告)号：US20120097586A1
公开(公告)日：2012-04-26
申请号：US13277949
申请日：2011-10-20
申请人： Thomas HEINZ , Eugen Mayer
发明人： Thomas HEINZ , Eugen Mayer
IPC分类号： B01D35/02 , B01D35/147 , B01D29/90
CPC分类号： B01D29/885 , B01D35/147 , B01D35/153 , B01D2201/165 , F23K5/147 , F23K5/18
摘要： In a device (1) for filtering and deaeration of liquid fuel, in particular fuel oil, comprising a tank connection (2) for connection to an oil tank, a feed connection (3) for connection to an oil burner feed, a return connection (4) for connection to an oil burner fuel return, a feed line (5) connecting the tank connection (2) to the feed connection (3), an oil filter (6) disposed in the feed line (5), and a return line (8) connecting the return connection (4) to the feed line (5), in accordance with the invention, the return line (8) is connected to the feed line (5) by means of a return changeover valve (14) that can be switched between two valve positions and connects the return line (8) to the feed line (5) in one of the valve positions upstream of the oil filter (6) and connects the return line (9) to the feed line (5) in the other valve position downstream of the oil filter (6).
摘要翻译：在用于液体燃料，特别是燃料油的过滤和脱气的装置（1）中，包括用于连接到油箱的罐连接件（2），用于连接到油燃烧器进料的进料连接件（3），回流连接（4），用于连接油燃烧器燃油回路，将油箱连接件（2）连接到进料连接件（3）的进料管线（5），设置在进料管线（5）中的油过滤器（6）根据本发明，将返回连接件（4）连接到进料管线（5）的返回管线（8），返回管线（8）通过回流切换阀（14）连接到进料管线），其可以在两个阀位置之间切换，并且在油过滤器（6）上游的阀位置之一处将返回管线（8）连接到进料管线（5），并将返回管线（9）连接到进料管线（5）位于机油滤清器（6）下游的另一阀位。

7. 发明授权

US08043050B2 Gap seal in blades of a turbomachine 有权
标题翻译：涡轮机刀片间隙密封
公开(公告)号：US08043050B2
公开(公告)日：2011-10-25
申请号：US12057506
申请日：2008-03-28
申请人： Thomas Heinz-Schwarzmaier , Sven Olmes , Ronald Wifling
发明人： Thomas Heinz-Schwarzmaier , Sven Olmes , Ronald Wifling
IPC分类号： F01D1/00
CPC分类号： F01D11/008
摘要： A gap seal (9) radially seals a gap (8) which extends axially and radially between two blades (1, 2) of a turbomachine which are adjacent in the circumferential direction (3). The two blades (1, 2) have, in each case, an axially extending longitudinal slot (10, 11), which is open towards the gap (8), on its respective blade root (6, 7). A band-form or strip-form sealing element (12) engages with its longitudinal sides (13, 14) in the two longitudinal slots (10, 11) and bridges the gap (8). The one blade (1) has a projection (15) on its blade root (6), which projects from the blade root (6) in the circumferential direction (3) and extends in the circumferential direction (3) and radially, at least in the region of the respective longitudinal slot (10), and bridges an axial longitudinal end of the gap (8) in the process. The other blade (2) has a step-shaped recess (16) on its blade root (7), complementary to the projection (15) of the one blade (1) and in which the projection engages. The projection (15) has a transverse slot (17) which extends in the circumferential direction (3) and is open towards the gap (8). The sealing element (12) engages with an end face (18) in the transverse slot (17).
摘要翻译：间隙密封件（9）径向密封在圆周方向（3）上相邻的涡轮机的两个叶片（1,2）之间轴向和径向延伸的间隙（8）。在每种情况下，两个叶片（1,2）在其相应的叶片根部（6,7）上具有朝向间隙（8）开口的轴向延伸的纵向槽（10,11）。带状或带状密封元件（12）与两个纵向狭槽（10,11）中的纵向侧面（13,14）接合并桥接间隙（8）。一个叶片（1）在其叶片根部（6）上具有在叶片根部（6）沿圆周方向（3）突出并且在周向（3）上径向延伸的突起（15），至少在相应的纵向狭槽（10）的区域中，并且在该过程中桥接间隙（8）的轴向纵向端部。另一个叶片（2）在其叶片根部（7）上具有与所述一个叶片（1）的突出部（15）互补并且突起接合的台阶形凹部（16）。突起（15）具有沿圆周方向（3）延伸并且朝向间隙（8）打开的横向槽（17）。密封元件（12）与横向槽（17）中的端面（18）接合。

8. 发明申请

US20110186879A1 MULTIFUNCTIONAL TAPE 有权
标题翻译：多功能胶带
公开(公告)号：US20110186879A1
公开(公告)日：2011-08-04
申请号：US13084877
申请日：2011-04-12
申请人： Thomas Heinz-Helmut ALTEBAEUMER , Stephen Day , Jonathan Heffernan
发明人： Thomas Heinz-Helmut ALTEBAEUMER , Stephen Day , Jonathan Heffernan
IPC分类号： H01L33/00
CPC分类号： H01L29/76 , B82Y10/00 , H01L27/15 , H01L29/0665 , H01L29/0673 , H01L29/0676 , H01L29/068 , H01L29/42392 , H01L29/66439 , H01L29/775 , H01L29/78642 , H01L29/78696 , H01L33/08 , H01L33/20 , H01L2924/0002 , H01L2924/00
摘要： A method comprises forming elongate structures (5) on a first substrate (3), such that the material composition of each elongate structure (7) varies along its length so as to define first and second physically different sections in the elongate structures. First and second physically different devices (1,2) are then defined in the elongate structures. Alternatively, the first and second physically different sections may be defined in the elongate structures after they have been fabricated. The elongate structures may be encapsulated and transferred to a second substrate (7). The invention provides an improved method for the formation of a circuit structure that requires first and second physically different devices (1,2) to be provided on a common substrate. In particular, only one transfer step is necessary.
摘要翻译：一种方法包括在第一基板（3）上形成细长结构（5），使得每个细长结构（7）的材料组成沿其长度变化，从而在细长结构中限定第一和第二物理上不同的部分。然后在细长结构中限定第一和第二物理上不同的装置（1,2）。或者，第一和第二物理上不同的部分可以在它们被制造之后在细长结构中限定。细长结构可以被封装并转移到第二衬底（7）。本发明提供了一种用于形成电路结构的改进方法，其需要在公共基板上提供第一和第二物理上不同的装置（1,2）。特别地，仅需要一个转移步骤。

9. 发明申请

US20110171039A1 BLADE ARRANGEMENT OF A GAS TURBINE 审中-公开
标题翻译：气体涡轮叶片布置
公开(公告)号：US20110171039A1
公开(公告)日：2011-07-14
申请号：US13024545
申请日：2011-02-10
申请人： Thomas HEINZ-SCHWARZMAIER , Thomas DUDA , Alexander SCHNELL
发明人： Thomas HEINZ-SCHWARZMAIER , Thomas DUDA , Alexander SCHNELL
IPC分类号： F01D5/18
CPC分类号： F01D11/122 , F01D5/288 , F01D11/14
摘要： A blade arrangement of a gas turbine, with at least one blade which in the radial direction projects into a hot gas passage arranged concentrically to an axis, and terminates in a blade tip which with a clearance lies opposite a heat shield which delimits the hot gas passage. The blade and the heat shield are movable in relation to each other in the circumferential direction, and the blade tip and the heat shield are covered with coatings, which enable a directed cutting of the blade tip into the heat shield. By such a blade arrangement, a reduction of the clearance as a result of cutting in is simply achieved by the heat shield having a porous thermal barrier coating as an outer, abradable coating, and by the blade tip being provided with a homogenous, metallic cover coating.
摘要翻译：一种燃气轮机的叶片装置，其具有至少一个叶片，其沿径向突出到与轴线同心设置的热气体通道中，并且终止于叶片尖端，其间隙与限定热气体的隔热罩相对通道。叶片和隔热罩可在圆周方向上相对移动，并且叶片尖端和隔热罩覆盖有涂层，从而能够将叶片尖端定向切割成隔热层。通过这样的叶片装置，通过具有作为外部可磨损涂层的多孔隔热涂层的隔热罩简单地实现由于切割而导致的间隙减小，并且通过叶片尖端设置有均匀的金属盖涂层。

10. 发明申请

US20110171013A1 SHROUD SEAL SEGMENTS ARRANGEMENT IN A GAS TURBINE 有权
标题翻译： SHROUD在气体涡轮机中的密封部分安装
公开(公告)号：US20110171013A1
公开(公告)日：2011-07-14
申请号：US13011203
申请日：2011-01-21
申请人： Tanguy ARZEL , Thomas HEINZ-SCHWARZMAIER , Martin SCHNIEDER
发明人： Tanguy ARZEL , Thomas HEINZ-SCHWARZMAIER , Martin SCHNIEDER
IPC分类号： F01D5/08
CPC分类号： F01D11/24 , F01D5/08 , F01D11/08 , F01D25/12 , F05D2240/11 , F05D2260/201 , F05D2260/202 , F05D2260/205
摘要： A gas turbine is provided that includes a rotor which is rotatable around an axis and equipped with rotor blades, and which is concentrically enclosed at a distance by a casing, which is equipped with stator blades, forming an annular hot gas passage. Rings with stator blades and rotor blades are arranged in a manner alternating in the axial direction. Between adjacent stator blades, heat shield segments are arranged, which delimit the hot gas passage on the outside in a region of the rotor blades and are cooled by impingement cooling where a cooling medium from an outer annular cavity flows into the heat shield segment.
摘要翻译：提供了一种燃气轮机，其包括能够绕轴线旋转并且配备有转子叶片的转子，并且由配置有定子叶片的壳体一定距离同心地封闭，该壳体形成环形的热气体通道。具有定子叶片和转子叶片的环以轴向交替排列。在相邻的定子叶片之间，布置有隔热板段，其在转子叶片的区域中限定外部的热气体通道，并且通过来自外部环形空腔的冷却介质流入隔热板段的冲击冷却来冷却。

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