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1.发明授权Single crystal turbine components made using a moving zone transient liquid phase bonded sandwich construction 有权使用移动区域瞬态液相粘结夹层结构制造的单晶涡轮机组件公开(公告)号：US06193141B1
公开(公告)日：2001-02-27
申请号：US09558131
申请日：2000-04-25
申请人： Michael A. Burke , Paul J. Zombo
发明人： Michael A. Burke , Paul J. Zombo
IPC分类号： B23K3102
CPC分类号： F01D5/005 , B23K20/023 , B23K20/16 , B23K35/004 , B23K35/3033 , B23K2101/001 , B23P15/04 , Y10T29/4932 , Y10T29/49336
摘要： A method of bonding together at least two long, metal alloy segments, of turbine components, such as turbine blade segments (18, 19, 20 and 21) by: putting a melting point depressant between the segments at bond planes (34) between contracting segments; forming a heated zone across the segments and a heated front (32); where melt pools (36) form in a molten zone (38) at the heated front which front (32), pools (36) and zone (38) continuously move and pass along the bond planes (34); where crystal re-growth (35) occurs along the bonding planes to form bonds (34) between the individual segments (18, 19, 20 and 21) behind the moving molten zone (38).
摘要翻译： 一种通过以下方式将至少两个长的金属合金段结合在一起的涡轮机部件，例如涡轮机叶片段（18,19,20和21）：通过在接合平面（34）处的段之间放置熔点降低剂 段; 跨越所述段和加热的前部（32）形成加热区; 其中熔融池（36）在加热的前部形成在熔融区域（38）中，前部（32），池（36）和区域（38）连续地移动并沿着粘合平面（34）移动; 其中晶体再生长（35）沿着接合平面发生，以在移动熔融区（38）后面的各个段（18,19,20和21）之间形成接合（34）。
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2.发明授权On-line monitor for detecting excessive temperatures of critical components of a turbine 有权用于检测涡轮机关键部件温度过高的在线监视器
公开(公告)号：US6062811A
公开(公告)日：2000-05-16
申请号：US129905
申请日：1998-08-06
摘要： A monitor for detecting overheating of a critical component in a combustion turbine is provided. The monitor, when used in conjunction with a closed-loop cooling system, comprises a coating comprising an indicator material having an activation temperature. The coating is situated on the internal cooling passages of the critical component. The monitor further comprises a sensor connected to an outlet conduit of the cooling system for determining the amount of degradation of indicator material by monitoring the cooling fluid flowing through the outlet conduit. Embodiments further comprising "sniffer" tubes for use with open-loop air cooling systems also are provided.
摘要翻译： 提供了一种用于检测燃气轮机中的关键部件的过热的监视器。 当与闭环冷却系统结合使用时，监测器包括包含具有活化温度的指示剂材料的涂层。 涂层位于关键部件的内部冷却通道上。 显示器还包括连接到冷却系统的出口导管的传感器，用于通过监测流经出口导管的冷却流体来确定指示剂材料的劣化量。 还提供了还包括用于开环空气冷却系统的“嗅探”管的实施例。
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3.发明授权On-line monitor for detecting excessive temperatures of critical components of a turbine 有权用于检测涡轮机关键部件温度过高的在线监视器公开(公告)号：US06200088B1
公开(公告)日：2001-03-13
申请号：US09566572
申请日：2000-05-08
IPC分类号： F01D518
摘要： A monitor for detecting overheating of a critical component in a combustion turbine is provided. The monitor, when used in conjunction with a closed-loop cooling system, comprises a coating comprising an indicator material having an activation temperature. The coating is situated on the internal cooling passages of the critical component. The monitor further comprises a sensor connected to an outlet conduit of the cooling system for determining the amount of degradation of indicator material by monitoring the cooling fluid flowing through the outlet conduit. Embodiments further comprising “sniffer” tubes for use with open-loop air cooling systems also are provided. In alternative embodiments, auxiliary cooling systems for supplying auxiliary cooling to critical components at certain activation temperatures also are provided.
摘要翻译： 提供了一种用于检测燃气轮机中的关键部件的过热的监视器。 当与闭环冷却系统结合使用时，监测器包括包含具有活化温度的指示剂材料的涂层。 涂层位于关键部件的内部冷却通道上。 显示器还包括连接到冷却系统的出口导管的传感器，用于通过监测流经出口导管的冷却流体来确定指示剂材料的劣化量。 还提供了还包括用于开环空气冷却系统的“嗅探”管的实施例。 在替代实施例中，还提供用于在某些激活温度下向关键部件提供辅助冷却的辅助冷却系统。
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4.发明授权公开(公告)号：US06733907B2
公开(公告)日：2004-05-11
申请号：US09963278
申请日：2001-09-26
IPC分类号： B32B900
CPC分类号： C04B35/10 , B32B18/00 , C04B28/34 , C04B35/803 , C04B35/806 , C04B37/001 , C04B37/005 , C04B38/007 , C04B2111/28 , C04B2235/5224 , C04B2235/5228 , C04B2235/77 , C04B2235/96 , C04B2235/9607 , C04B2237/06 , C04B2237/062 , C04B2237/34 , C04B2237/341 , C04B2237/343 , C04B2237/345 , C04B2237/346 , C04B2237/348 , C04B2237/36 , C04B2237/361 , C04B2237/365 , C04B2237/366 , C04B2237/368 , C04B2237/38 , C04B2237/584 , C04B2237/62 , C04B2237/704 , F01D5/288 , F05D2230/90 , F05D2300/21 , F05D2300/6033 , F05D2300/611 , Y02T50/67 , Y02T50/672 , Y10T428/2495 , Y10T428/30 , C04B35/00
摘要： A hybrid ceramic structure (10), for use in high temperature environments such as in gas turbines, is made from an insulating layer (12) of porous ceramic that is thermally stable at temperatures up to 1700° C. bonded to a high mechanical strength structural layer (8) of denser ceramic that is thermally stable at temperatures up to 1200° C., where optional high temperature resistant adhesive (9) can bond the layers together, where optional cooling ducts (11) can be present in the structural layer and where hot gas (14) can contact the insulating layer (12) and cold gas (15) can contact the structural layer (8).
摘要翻译： 用于高温环境例如燃气轮机的混合陶瓷结构（10）由多孔陶瓷的绝缘层（12）制成，其在高达1700℃的温度下是热稳定的，结合到高机械强度 结构层（8），其在高达1200℃的温度下是热稳定的，其中任选的耐高温粘合剂（9）可以将层粘合在一起，其中可选的冷却管道（11）可以存在于结构层 并且其中热气体（14）可以接触绝缘层（12）并且冷气体（15）可接触结构层（8）。
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5.发明授权
公开(公告)号：US4402905A
公开(公告)日：1983-09-06
申请号：US355071
申请日：1982-03-05
申请人： Michael A. Burke , Robert E. Gainer
发明人： Michael A. Burke , Robert E. Gainer
IPC分类号： B22F3/14 , C04B35/645 , C22C29/18 , B22F1/00 , B22F9/04
CPC分类号： C22C29/18 , B22F3/14 , C04B35/645
摘要： The present invention is directed to a process for preparing a body of polycrystalline silicon doped with aluminum comprising melting a mixture of silicon powder and aluminum powder, rapidly quenching the melt, grinding the solidified silicon-aluminum alloy and hot pressing to form a compact.
摘要翻译： 本发明涉及一种制备掺杂有铝的多晶硅体的方法，包括熔融硅粉和铝粉的混合物，快速淬火熔体，研磨固化的硅铝合金并热压成型。
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公开(公告)号：US07311790B2
公开(公告)日：2007-12-25
申请号：US10767013
申请日：2004-01-29
CPC分类号： B28B19/0053 , B28B21/42 , F05D2300/6033 , F23R3/007
摘要： A hybrid structure (50) and method of manufacturing the same including a structural ceramic matrix composite (CMC) material (42) coated with a layer of ceramic insulating tiles (24). Individual ceramic tiles are attached to a surface (22) of a mold (20). The exterior surface (32) of the tiles may be subjected to a mechanical process such as machining with the mold in place to provide mechanical support for the tiles. A layer of CMC material is then applied to bond the tiles and the CMC material together into a hybrid structure. The mold may include a fugitive material portion (26) to facilitate removal of the mold when the hybrid structure has a complex shape. Tiles located in different regions of the structure may have different compositions and/or dimensions. The gaps between adjacent tiles may be filled from the outside before the CMC material is applied or from the inside after the mold is removed.
摘要翻译： 一种混合结构（50）及其制造方法，包括涂覆有陶瓷绝缘砖（24）层的结构陶瓷基复合材料（CMC）材料（42）。 单个陶瓷砖附接到模具（20）的表面（22）。 瓦片的外表面（32）可以经受机械加工，例如用模具进行机械加工，以为瓦片提供机械支撑。 然后施加一层CMC材料以将瓷砖和CMC材料结合在一起成为混合结构。 当混合结构具有复杂的形状时，模具可以包括短片材料部分（26），以便于去除模具。 位于结构的不同区域的瓷砖可以具有不同的组成和/或尺寸。 相邻瓦片之间的间隙可以在CMC材料施加之前从外部填充，或者在模具移除之后从内部填充。
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公开(公告)号：US06508000B2
公开(公告)日：2003-01-21
申请号：US09779208
申请日：2001-02-08
IPC分类号： B23P1500
CPC分类号： B23P6/005 , B23K2101/001 , F01D5/005 , Y10T29/49318 , Y10T29/49336 , Y10T29/49721
摘要： A method of repairing gas turbine engine components is provided. The method includes removing the damaged portion and fabricating an insert to match the removed portion. The insert is precision machined and crystallographically matched to the original component, and then bonded to this component using transient liquid phase bonding techniques and suitable heat treatment.
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公开(公告)号：US4599506A
公开(公告)日：1986-07-08
申请号：US678523
申请日：1984-12-05
申请人： Michael A. Burke , Israel Stol
发明人： Michael A. Burke , Israel Stol
CPC分类号： B23K9/095
摘要： A visual observation system for monitoring a welding operation being performed in a welding region by a welding torch, the torch having a longitudinal axis and including a housing. The system is composed of a closed light conducting channel supported by the torch and having a first end directed toward the welding region and a second end remote from the first end, and image generating device disposed at the second end of the channel for receiving light entering the channel via the first end in order to generate an image of the scene in front of the first end, a transpatent plate disposed in, and blocking, the light conducting channel for protecting the image generating device against soiling by particles produced by the welding operation, and elements for producing a flow of inert gas past the side of the transparent plate directed toward the first end for opposing the deposition of such particles on the plate. The a light conducting channel is dimensioned such that in at least one direction transverse to the longitudinal axis of the torch, the channel does not project beyond the torch housing.
摘要翻译： 一种用于监视焊接操作的目视观察系统，其通过焊炬在焊接区域中进行，所述焊炬具有纵向轴线并且包括壳体。 该系统由一个由割炬支撑的闭合导光通道组成，具有朝向焊接区域的第一端和远离第一端的第二端，以及设置在通道的第二端处的图像产生装置，用于接收光线 所述通道经由所述第一端以在所述第一端的前方产生场景的图像，设置在所述导光通道中并且阻挡所述导光通道的变色板，用于保护所述图像生成装置免受由所述焊接操作产生的颗粒的污染 以及用于产生朝向第一端的透明板侧的惰性气体流的元件，用于使这种颗粒沉积在板上。 导光通道的尺寸使得在至少一个横向于割炬的纵向轴线的方向上，通道不会突出超过割炬壳体。
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9.发明授权
公开(公告)号：US4540038A
公开(公告)日：1985-09-10
申请号：US617458
申请日：1984-06-05
申请人： Michael A. Burke
发明人： Michael A. Burke
CPC分类号： B22D27/045
摘要： This is a process of fabricating directionally solidified turbine blades for combustion turbines. It is an improvement to the type of process where a mold containing molten metal is cooled in a controlled fashion such that solidification occurs slow enough to allow directional solidification beginning at the airfoil end. In the improved process solidification is monitored and magnetic mixing of the remaining molten metal is started at approximately the beginning of solidification of said root section and the rate of cooling of said blade is increased to a rate faster than at which directional solidification occurs. A blade is produced with a directionally solidified airfoil section and a fine grained root section and without a substantially inhomogeneous portion at the interface between the airfoil and root sections.
摘要翻译： 这是制造用于燃烧涡轮机的定向凝固涡轮机叶片的过程。 对于其中含有熔融金属的模具以受控的方式冷却的过程类型是一种改进，使得固化发生得足够缓慢以允许从翼型端开始定向凝固。 在改进的方法中，监测固化，并且在所述根部部分的凝固开始时大约开始固化时开始剩余熔融金属的磁性混合，并且所述叶片的冷却速率增加到比发生定向凝固的速度更快的速率。 叶片产生有定向凝固的翼型部分和细粒根部，并且在翼型和根部之间的界面处没有基本上不均匀的部分。
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公开(公告)号：US07351364B2
公开(公告)日：2008-04-01
申请号：US10767012
申请日：2004-01-29
CPC分类号： B28B7/342 , B28B11/08 , B28B19/00 , C04B2235/6028 , F05D2300/6033 , Y10S264/44
摘要： A method of manufacturing a hybrid structure (100) having a layer of CMC material (28) defining an interior passageway (24) and a layer of ceramic insulating material (18) lining the passageway. The method includes the step of casting the insulating material to a first thickness required for effective casting but in excess of a desired second thickness for use of the hybrid structure. An inner mold (14) defining a net shape desired for the passageway remains in place after the casting step to mechanically support the insulating material during a machining process used to reduce the thickness of the insulating material from the as-cast first thickness to the desired second thickness. The inner mold also provides support as the CMC material is deposited onto the insulating material. The inner mold may include a fugitive material portion (20) to facilitate its removal after the CMC material is formed.
摘要翻译： 一种制造具有限定内部通道（24）的CMC材料层（28）和衬套通道的陶瓷绝缘材料层（18）的混合结构（100）的方法。 该方法包括将绝缘材料浇铸到有效铸造所需的第一厚度但超过所需的第二厚度以用于混合结构的步骤。 限定通道所需的净形状的内模（14）在铸造步骤之后保持就位，以在用于将绝缘材料的厚度从铸造第一厚度减小到期望的机械加工过程期间机械地支撑绝缘材料 第二厚度。 当CMC材料沉积到绝缘材料上时，内模还提供支撑。 内部模具可以包括短暂材料部分（20），以便在形成CMC材料之后便于其移除。
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