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21. 发明申请

US20050129508A1 Cooled turbine blade or vane 有权
标题翻译：冷却涡轮叶片或叶片
公开(公告)号：US20050129508A1
公开(公告)日：2005-06-16
申请号：US10949521
申请日：2004-09-27
申请人： Reinhard Fried , Hans Wettstein
发明人： Reinhard Fried , Hans Wettstein
IPC分类号： F01D5/18 , F01D5/14
CPC分类号： F01D5/187 , F05D2260/607
摘要： A turbine blade or vane (1) has a shell (2), including a first side wall (8) and a second side wall (9), which are connected together at a leading edge (10) and at a trailing edge (11), which extend longitudinally from a root (7) to a tip (6) and which are connected together between leading edge (10) and trailing edge (11) by a plurality of inner ribs (13). In the inner region (12) of the turbine blade/vane (1), the ribs (13) form at least one cooling gas path (15), which guides a cooling gas flow from the root (7) to the tip (6) and, in the process, is deflected a plurality of times in serpentine shape from the outside to the inside and from the inside to the outside. In order to increase the life of the turbine blade/vane (1), at least one bypass opening (18) and/or at least one outlet opening (19) are arranged in the region of at least one rib (13), which deflects the cooling gas flow from the outside to the inside, the bypass opening (18) penetrating the rib (13) at the shell (2) and the outlet opening (19) penetrating the shell (2).
摘要翻译：涡轮叶片或叶片（1）具有壳体（2），包括第一侧壁（8）和第二侧壁（9），它们在前缘（10）和后缘（11）处连接在一起），其从根部（7）纵向延伸到尖端（6），并且通过多个内肋（13）在前缘（10）和后缘（11）之间连接在一起。在涡轮叶片/叶片（1）的内部区域（12）中，肋（13）形成至少一个冷却气体通道（15），其将冷却气体流从根部（7）引导到尖端（6）），并且在该过程中，从外部到内部以及从内部到外部以蛇形形式偏转多次。为了增加涡轮叶片/叶片（1）的寿命，至少一个旁路开口（18）和/或至少一个出口开口（19）布置在至少一个肋（13）的区域中，其中将冷却气流从外部偏转到内部，旁路开口（18）穿过壳体（2）处的肋（13）并穿过壳体（2）的出口开口（19）。

22. 发明申请

US20050084371A1 Base material with cooling air hole 失效
标题翻译：基材具有冷却空气孔
公开(公告)号：US20050084371A1
公开(公告)日：2005-04-21
申请号：US10899031
申请日：2004-07-27
申请人： Reinhard Fried , Ulrich Rathmann
发明人： Reinhard Fried , Ulrich Rathmann
IPC分类号： F01D5/18 , F01D25/12
CPC分类号： F01D5/18 , B23P2700/06 , F01D5/186 , F01D25/12 , F05D2260/201 , F05D2260/202 , F05D2260/607
摘要： A base material (2) with a cooling air hole (1) is disclosed, means being present which prevent particles (5), which are located in the cooling air (4) which flows through the cooling air hole (1) during the operation of the cooling air hole (1), from closing the cooling air hole (1). In this arrangement, the means can consist in the edge of the cooling air hole (1) being uneven or having a ridge (3) or the cooling air hole (1) being star-shaped, ellipsoidal or linear or the cooling air hole (1) being circular and having lateral slots (7).
摘要翻译：公开了一种具有冷却空气孔（1）的基材（2），用于防止在操作期间流过冷却空气孔（1）的冷却空气（4）中的颗粒（5）的装置的冷却空气孔（1）的关闭。在这种布置中，装置可以包括不均匀或具有脊（3）的冷却空气孔（1）的边缘或冷却空气孔（1）是星形，椭圆形或直线形或冷却空气孔（ 1）为圆形并具有侧向槽（7）。

23. 发明授权

US06720087B2 Temperature stable protective coating over a metallic substrate surface 失效
标题翻译：在金属基材表面上的温度稳定的保护涂层
公开(公告)号：US06720087B2
公开(公告)日：2004-04-13
申请号：US10193278
申请日：2002-07-12
申请人： Reinhard Fried , Alkan Goecmen , Abdus S. Khan
发明人： Reinhard Fried , Alkan Goecmen , Abdus S. Khan
IPC分类号： B32B1504
CPC分类号： C23C28/3215 , C23C4/02 , C23C28/3455 , C23C28/44 , Y02T50/67 , Y10T428/12451 , Y10T428/12486 , Y10T428/12493 , Y10T428/12611 , Y10T428/12931 , Y10T428/12937 , Y10T428/12944
摘要： The invention describes a temperature-stable protective coating over a metallic substrate surface (1), which coating includes at least one layer of material (4) consisting of MCrAlY, where M represents at least one of the elements selected from the group of materials consisting of Fe, Co and Ni. The invention also describes a production process for this coating. The invention is distinguished by the fact that a multiplicity of local elevations, known as rivets (3), are provided distributed directly over the area of the substrate surface (1) or distributed indirectly over the area of the substrate surface, separated from the substrate surface (1) by means of at least one interlayer (2), which rivets are fixedly joined to the substrate surface (1) or the interlayer (2), that at least one layer of material (4) consisting of MCrAlY is deposited on the substrate surface (1) or interlayer (2) in such a manner that the layer of material (4) consisting of MCrAlY completely surrounds the rivets (3), completely fills regions which lie between adjacent rivets (3) and projects above the rivets (3).
摘要翻译：本发明描述了在金属基材表面（1）上的温度稳定的保护涂层，该涂层包括由MCrAlY组成的至少一层材料（4），其中M表示选自以下的材料中的至少一种元素：的Fe，Co和Ni。本发明还描述了该涂层的生产方法。本发明的区别在于，提供了多个局部立面，称为铆钉（3），直接分布在衬底表面（1）的区域上，或间接地分布在与衬底分离的衬底表面的区域上表面（1）通过至少一个中间层（2），所述铆钉固定地接合到基底表面（1）或中间层（2），至少一层由MCrAlY组成的材料层（4）沉积在衬底表面（1）或中间层（2），使得由MCrAlY组成的材料层（4）完全包围铆钉（3），完全填充位于相邻铆钉（3）之间并突出在铆钉上方的区域（3）。

24. 发明授权

US06647624B2 Method of fitting an impingement plate 有权
标题翻译：碰撞板的安装方法
公开(公告)号：US06647624B2
公开(公告)日：2003-11-18
申请号：US10187004
申请日：2002-07-02
申请人： Reinhard Fried , Richard London , Peter Marx
发明人： Reinhard Fried , Richard London , Peter Marx
IPC分类号： B23P1500
CPC分类号： B23K11/002 , Y10T29/4932 , Y10T29/49778 , Y10T29/49895
摘要： A method of fitting an impingement plate to a platform of a guide blade of a gas turbine. The impingement plate is first fastened at individual spots by spot welds to at least one supporting surface of the platform and is then brazed at the supporting surface to the platform. The impingement plate is prefabricated with recesses and the spot welds are executed at the recesses.
摘要翻译：一种将冲击板装配到燃气轮机的引导叶片的平台上的方法。冲击板首先通过点焊在单个点处紧固到平台的至少一个支撑表面上，然后在支撑表面上钎焊到平台。冲击板预制有凹槽，点焊在凹槽处执行。

25. 发明授权

US5067986A Process for producing coarse, longitudinally oriented column crystals in an oxide-dispersion-strengthened nickel-base superalloy 失效
标题翻译：氧化物分散强化镍基超级合金中生产粗糙度，纵向取向的柱状晶体的方法
公开(公告)号：US5067986A
公开(公告)日：1991-11-26
申请号：US524273
申请日：1990-05-15
申请人： Reinhard Fried , Peter Jongenburger
发明人： Reinhard Fried , Peter Jongenburger
IPC分类号： C22C19/05 , C22C29/12 , C22C32/00 , C22F1/00 , C22F1/10
CPC分类号： C22C32/0026 , C22F1/10
摘要： A process for producing coarse, longitudinally oriented column crystals with improved temperature change resistance and ductility in the transverse direction in a workpiece of any cross-section from an oxide-dispersion-strengthened nickel-base superalloy, which exists in fine-grained form, by annealing in the temperature range between 1000.degree. and 1200.degree. C., cooling to room temperature and isothermally annealing for coarse grain in the range between 1230.degree. C. and 1280.degree. C.
摘要翻译：一种生产粗略纵向取向的柱状晶体的方法，该方法具有改善的耐温度变化性和延展性，其工作方式是从以细晶粒形式存在的氧化物分散强化的镍基超级合金的任何截面的工件中在1000〜1200℃的温度范围内进行退火，冷却至室温，并在1230℃〜1280℃的范围内对粗粒进行等温退火。

26. 发明授权

US4474009A Control apparatus for an air throttle valve in the intake manifold of an internal combustion engine 失效
标题翻译：内燃机的进气歧管中的空气节流阀的控制装置
公开(公告)号：US4474009A
公开(公告)日：1984-10-02
申请号：US204859
申请日：1980-11-07
申请人： Reinhard Fried , Heimo Hubner
发明人： Reinhard Fried , Heimo Hubner
IPC分类号： F02D9/04 , F02B33/42 , F02B37/00
CPC分类号： F02B33/42
摘要： The invention discloses an apparatus for adjusting or actuating an air throttle valve positioned in the intake manifold of an internal combustion engine which is supplied by air under pressure. The air throttle valve is held in a closed position by a spring when the engine is in the cold starting phase. Air is supplied to the engine through a by-pass valve when the air throttle valve is closed. The air throttle valve is opened against the force of the spring in response to a predetermined pressure or vacuum in the intake manifold at the end of the cold starting phase. The air throttle valve is held in an open position by an electro-magnetic structure which is effective when an ignition circuit of the vehicle is energized or by a detent structure which is effective when the engine or exhaust temperatures are at predetermined levels.
摘要翻译：本发明公开了一种用于调节或致动位于内燃机的进气歧管内的空气节流阀的装置，其由在压力下的空气供应。当发动机处于冷启动阶段时，空气节流阀由弹簧保持在关闭位置。当节气门关闭时，空气通过旁路阀供给发动机。在冷起动阶段结束时，响应于进气歧管中的预定压力或真空，克服弹簧的力打开空气节流阀。空气节流阀通过电磁结构保持在打开位置，该电磁结构在车辆的点火电路通电时或通过当发动机或排气温度处于预定水平时有效的止动结构有效。

27. 发明授权

US4298028A Starting valve and mounting therefor 失效
标题翻译：起动阀和安装
公开(公告)号：US4298028A
公开(公告)日：1981-11-03
申请号：US115131
申请日：1980-01-24
申请人： Reinhard Fried , Andreas Mayer , Ambrogio Perego
发明人： Reinhard Fried , Andreas Mayer , Ambrogio Perego
IPC分类号： F02B39/00 , F02B33/00 , F02B33/42 , F02B37/16 , F02N99/00 , F16K1/226 , F16K11/14 , F16K1/22
CPC分类号： F16K1/2268 , F02B33/42 , Y10S384/908 , Y10T137/87692 , Y10T137/87756 , Y10T137/8778
摘要： A starting valve is disclosed having a starter choke valve and a poppet valve which is kept closed by the starter choke valve when the choke valve is in an open position. For mounting the starter choke valve there is provided a choke shaft and a bushing set screw which interact with a plurality of tapered bushes. The arrangement provides for an axial and a radial compression of the bushes to prevent foreign matter from fouling the movement of the choke. Also a compensation for the varying tolerances between the component parts is accomplished by providing a plurality of rubber-elastic components.
摘要翻译：公开了一种起动阀，其具有起动阻流阀和提升阀，当止回阀处于打开位置时，该提升阀由起动阻流阀保持关闭。为了安装起动器节流阀，设置有与多个锥形衬套相互作用的阻塞轴和衬套固定螺钉。该布置提供了衬套的轴向和径向压缩，以防止异物污染扼流圈的运动。还通过提供多个橡胶弹性部件来实现组件之间的不同公差的补偿。

28. 发明授权

US4154060A Method for starting a pressure-charged internal-combustion engine and apparatus for implementing the method 失效
标题翻译：用于启动加压内燃机的方法和用于实施该方法的装置
公开(公告)号：US4154060A
公开(公告)日：1979-05-15
申请号：US751098
申请日：1976-12-16
申请人： Alain Deprez , Reinhard Fried
发明人： Alain Deprez , Reinhard Fried
IPC分类号： F02D23/00 , F02B33/42 , F02B33/44 , F02B37/00
CPC分类号： F02B33/446 , F02B33/42
摘要： A starting arrangement for a pressure-charged internal-combustion engine in which at the beginning of the starting phase combustion air is delivered to the engine by way of a bypass valve and a throttle valve in the charge-air line from the pressure-charging device is closed. Two mutually independent variables are used for controlling the opening of the throttle valve. At the end of the starting phase a command variable typical of the process e.g., charge air pressure is used to initiate an opening of the throttle valve and an engine-dependent operating variable e.g., engine lubricating oil pressure is then used to actually move the throttle valve to its open position, the throttle valve then remaining in the open position so long as the engine-dependent operating variable does not fall below a specified minimum value.
摘要翻译：一种起动装置，其特征在于，在起动阶段开始时，燃料空气通过旁通阀和来自加压装置的增压空气管路中的节气门被输送到发动机关闭了。两个相互独立的变量用于控制节流阀的开度。在起动阶段结束时，典型的过程的命令变量例如是使用增压空气压力来启动节流阀的开启和发动机相关的操作变量，例如，然后使用发动机润滑油压力来实际地移动油门只要发动机相关的操作变量不低于指定的最小值，节气门就处于打开位置。

29. 发明授权

US07293962B2 Cooled turbine blade or vane 有权
标题翻译：冷却涡轮叶片或叶片
公开(公告)号：US07293962B2
公开(公告)日：2007-11-13
申请号：US10949521
申请日：2004-09-27
申请人： Reinhard Fried , Hans Wettstein
发明人： Reinhard Fried , Hans Wettstein
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2260/607
摘要： A turbine blade or vane (1) has a shell (2), including a first side wall (8) and a second side wall (9), which are connected together at a leading edge (10) and at a trailing edge (11), which extend longitudinally from a root (7) to a tip (6) and which are connected together between leading edge (10) and trailing edge (11) by a plurality of inner ribs (13). In the inner region (12) of the turbine blade/vane (1), the ribs (13) form at least one cooling gas path (15), which guides a cooling gas flow from the root (7) to the tip (6) and, in the process, is deflected a plurality of times in serpentine shape from the outside to the inside and from the inside to the outside. In order to increase the life of the turbine blade/vane (1), at least one bypass opening (18) and/or at least one outlet opening (19) are arranged in the region of at least one rib (13), which deflects the cooling gas flow from the outside to the inside, the bypass opening (18) penetrating the rib (13) at the shell (2) and the outlet opening (19) penetrating the shell (2).
摘要翻译：涡轮叶片或叶片（1）具有壳体（2），包括第一侧壁（8）和第二侧壁（9），它们在前缘（10）和后缘（11）处连接在一起），其从根部（7）纵向延伸到尖端（6），并且通过多个内肋（13）在前缘（10）和后缘（11）之间连接在一起。在涡轮叶片/叶片（1）的内部区域（12）中，肋（13）形成至少一个冷却气体通道（15），其将冷却气体流从根部（7）引导到尖端（6）），并且在该过程中，从外部到内部以及从内部到外部以蛇形形式偏转多次。为了增加涡轮叶片/叶片（1）的寿命，至少一个旁路开口（18）和/或至少一个出口开口（19）布置在至少一个肋（13）的区域中，其中将冷却气流从外部偏转到内部，旁路开口（18）穿过壳体（2）处的肋（13）并穿过壳体（2）的出口开口（19）。

30. 发明授权

US06895650B2 Process for producing a spatially shaped carrier layer 失效
标题翻译：用于制造空间形载体层的方法
公开(公告)号：US06895650B2
公开(公告)日：2005-05-24
申请号：US10173258
申请日：2002-06-18
申请人： Reinhard Fried , Alkan Goecmen
发明人： Reinhard Fried , Alkan Goecmen
IPC分类号： C23C2/00 , C23C4/00 , C23C4/18 , C23C24/00 , B23P25/00
CPC分类号： C23C4/00 , C23C2/00 , C23C4/185 , C23C24/00 , Y02T50/67 , Y10T29/49885 , Y10T29/4998 , Y10T29/49982 , Y10T428/1234 , Y10T428/24149
摘要： A process for producing a spatially shaped carrier layer (3) which is of foil-like design from hard brittle material includes: providing a basic mold (1) having a spatially shaped surface, depositing a material which is in the gas or liquid phase on the spatially shaped surface, solidifying the material which has been deposited on the spatially shaped surface to form a hard brittle material layer (3), and separating the hard brittle material layer (3) from the spatially shaped surface in order to obtain the carrier layer (3) which consists of hard brittle material.
摘要翻译：用于生产由硬脆性材料制成箔状设计的空间形状载体层（3）的方法包括：提供具有空间形状表面的基本模具（1），将处于气相或液相的材料沉积在在空间形状的表面上固化已经沉积在空间形状表面上的材料以形成硬脆性材料层（3），并将硬脆性材料层（3）与空间形状表面分离，以获得载体层（3）由硬脆材料组成。

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