公开(公告)号：US20040072014A1

公开(公告)日：2004-04-15

申请号：US10271098

申请日：2002-10-15

Applicant: General Electric Company

Inventor： Wayne Charles Hasz ,  Nesim Abuaf ,  Robert Alan Johnson ,  Ching-Pang Lee

IPC: B32B001/06 ,  B32B001/08 ,  B32B015/02

CPC classification number: F28F13/18 ,  B23K35/30 ,  F01D5/147 ,  F01D5/186 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2230/10 ,  F05D2230/21 ,  F05D2230/22 ,  F05D2230/23 ,  F05D2230/40 ,  F05D2260/202 ,  F05D2260/2212 ,  F05D2260/22141 ,  F05D2300/132 ,  F05D2300/172 ,  F05D2300/222 ,  Y02T50/67 ,  Y02T50/676 ,  Y10T428/12993

Abstract: A method of providing turbulation on the inner surface of a passage hole (e.g., a turbine cooling hole) is described. The turbulation is first applied to a substrate which can eventually be inserted into the passage hole. The substrate is often a bar or tube, formed of a sacrificial material. After the turbulation is applied to the substrate, the substrate is inserted into the passage hole. The turbulation material is then fused to the inner surface, using a conventional heating technique. The sacrificial substrate can then be removed from the hole by various techniques. Related articles are also described.

Abstract translation: 描述了在通道孔（例如，涡轮机冷却孔）的内表面上提供紊流的方法。 首先将该紊乱施加到最终可以插入通道孔中的基底。 基板通常是由牺牲材料形成的棒或管。 在对基板施加了混浊之后，将基板插入到通孔中。 然后使用常规的加热技术将紊乱材料熔合到内表面。 然后可以通过各种技术从孔中去除牺牲衬底。 还描述了相关文章。

公开(公告)号：US20030106215A1

公开(公告)日：2003-06-12

申请号：US10014696

申请日：2001-12-11

Applicant: General Electric Company

Inventor： John Peter Heyward ,  Gregory Alan White ,  Michael Philip Hagle ,  Ching-Pang Lee

IPC: B23P006/00

CPC classification number: B23P6/002 ,  F01D5/005 ,  Y02T50/67 ,  Y02T50/673 ,  Y10T29/49318

Abstract: The present invention provides a method of repairing a turbine nozzle segment having one or more vanes disposed between outer and inner bands. The method includes separating at least one of the outer and inner bands from the vanes. The vanes are cut through in close proximity to the band being replaced. A newly manufactured replacement band including protruding vane stubs is provided for each one of the original bands being replaced. The replacement band is attached to the vanes by welding.

Abstract translation: 本发明提供了一种修复涡轮喷嘴段的方法，其具有设置在外带和内带之间的一个或多个叶片。 该方法包括从叶片分离外带和内带中的至少一个。 叶片在被更换的带子附近切割。 为更换的每个原始频带提供新制造的包括突出的叶片短截线的替换带。 替代带通过焊接附接到叶片。

公开(公告)号：US20030173213A1

公开(公告)日：2003-09-18

申请号：US10063087

申请日：2002-03-18

Applicant: General Electric Company

Inventor： Ching-Pang Lee ,  Robert Alan Johnson ,  Bin Wei ,  Hsin-Pang Wang ,  Lawrence Bernard Kool

IPC: B23H003/06

CPC classification number: B23H9/16 ,  B23H9/10

Abstract: An electrode for rejuvenating a cooling passage within an airfoil, the electrode including a tip, an end, a conductive core extending between the tip and the end, and an insulating coating disposed on the conductive core. The insulating coating exposes a number of conductive strips of the conductive core extending between the tip and the end. The insulating coating forms a number of insulating portions and further exposes a number of spacer portions of the conductive core longitudinally positioned between the insulating portions. The insulating portions substantially span a distance between the tip and the end and are positioned between the conductive strips.

Abstract translation: 一种用于振动翼型内的冷却通道的电极，所述电极包括尖端，端部，在尖端和端部之间延伸的导电芯，以及设置在导电芯上的绝缘涂层。 绝缘涂层暴露出在尖端和端部之间延伸的多个导电芯的导电条。 绝缘涂层形成多个绝缘部分，并进一步暴露导体芯的多个间隔部分纵向定位在绝缘部分之间。 绝缘部分基本上跨越尖端和端部之间的距离并且位于导电条之间。

公开(公告)号：US20030209589A1

公开(公告)日：2003-11-13

申请号：US10139659

申请日：2002-05-07

Applicant: General Electric Company

Inventor： Wayne Charles Hasz ,  Venkat S. Venkataramani ,  Ching-Pang Lee

IPC: B23K031/02

CPC classification number: B23P15/008 ,  B81B1/00 ,  C23C4/01 ,  C23C4/18 ,  C23C26/00 ,  C23C26/02 ,  C23C28/3215 ,  C23C28/3455 ,  F01D5/18 ,  F01D5/288 ,  F02K9/64 ,  F23R3/002 ,  F23R3/005 ,  Y02T50/67 ,  Y10T29/49321 ,  Y10T29/49341 ,  Y10T29/49812

Abstract: A method for forming a channel within a coated, metal-based substrate is described. In one technique, a channel-forming material is first deposited on the substrate, followed by the deposition of a bonding agent, such as a braze. One or more coatings can then be applied over the substrate. In one embodiment, the channel is formed when the channel-forming material is subsequently removed. In another embodiment, the channel is formed due to the lack of adhesion between particular channel-forming materials and the overlying bonding agent. Related articles are also described, e.g., gas turbine components which include protective coatings and a pattern of cooling channels.

Abstract translation: 描述了在涂覆的金属基底中形成通道的方法。 在一种技术中，首先在基底上沉积通道形成材料，然后沉积粘合剂，例如钎焊。 然后可以在衬底上施加一个或多个涂层。 在一个实施例中，当通道形成材料随后被去除时，形成通道。 在另一个实施方案中，由于在特定的通道形成材料和上覆粘合剂之间缺乏粘合而形成通道。 还描述了相关文章，例如包括保护涂层和冷却通道图案的燃气涡轮机部件。