-
1.
公开(公告)号:US20050181231A1
公开(公告)日:2005-08-18
申请号:US10708205
申请日:2004-02-16
IPC分类号: B23K1/00 , B23K35/32 , B23K35/40 , B23P6/00 , C22C19/07 , F01D5/28 , F01D25/00 , F02C7/00 , B32B15/00 , B23P19/04
CPC分类号: B23P6/005 , B23K1/0008 , Y10T29/301 , Y10T29/302 , Y10T29/49318 , Y10T29/49721 , Y10T29/49723 , Y10T29/49726 , Y10T29/49728 , Y10T29/49732 , Y10T29/49734 , Y10T29/49737 , Y10T29/49742 , Y10T29/49746 , Y10T428/12861
摘要: A process for refurbishing a worn surface of a shroud support component of a turbomachine, as well as a shroud support component refurbished with the process. The process generally entails removing a surface region of the worn surface so as to define a repair surface on the component. A braze tape formed from a slurry to comprise a braze material and a wear-resistant alloy is then applied to the repair surface, followed by a heat treatment to cause the braze tape to diffusion bond to the repair surface so as to define a built-up surface. The built-up surface is then machined to define a wear-resistant coating on the component.
摘要翻译: 用于翻新涡轮机的护罩支撑部件的磨损表面的过程以及用该过程翻新的护罩支撑部件。 该方法通常需要去除磨损表面的表面区域,以便在部件上限定修复表面。 然后将由钎焊材料和耐磨合金制成的浆料形成的钎焊带施加到修复表面上,随后进行热处理,使得钎焊带扩散到修复表面上, 上表面。 然后,加工表面被加工以在部件上限定耐磨涂层。
-
公开(公告)号:US06892931B2
公开(公告)日:2005-05-17
申请号:US10330420
申请日:2002-12-27
CPC分类号: B23P6/005 , F01D9/042 , F01D25/246 , F05D2220/32 , F05D2230/80 , Y02T50/67 , Y10T29/49316 , Y10T29/49742
摘要: A method facilitates replacing a portion of a gas turbine engine turbine support. The turbine support includes a body including a forward leg, an aft leg, and a mounting flange that each extend radially outwardly from the body. The forward leg is axially upstream from the aft leg and the mounting flange. The mounting flange is substantially axially aligned with respect to the aft leg. The method comprises cutting through at least one of the body, the aft leg, and the mounting flange, removing the forward leg and at least a portion of the body that is upstream from the cut from the engine, and coupling a replacement spad to the portion of the turbine support that is downstream from the cut.
摘要翻译: 一种方法有助于更换燃气涡轮发动机涡轮机支架的一部分。 涡轮机支撑件包括主体,其包括前腿,后腿和安装凸缘,每个从主体径向向外延伸。 前腿从后腿和安装法兰轴向上游。 安装法兰相对于后腿基本上轴向对准。 该方法包括切割主体,后腿和安装凸缘中的至少一个,从发动机上拆下前腿和身体上游的至少一部分,并将替换螺钉与 在切割下游的涡轮支架的一部分。
-
公开(公告)号:US20060257244A1
公开(公告)日:2006-11-16
申请号:US11224655
申请日:2005-09-12
IPC分类号: F03B11/00
CPC分类号: F01D5/005 , B23P6/005 , F01D9/06 , F05D2230/237 , F05D2240/12 , Y02T50/671 , Y10T29/49243
摘要: A gas turbine engine plenum cover is repaired using a prefabricated repair cover SPAD. The SPAD repair cover has a spoolie boss that is aligned and attached to the body of the repair plenum cover prior to attachment to a plenum casting to form a repaired plenum chamber. Preattachment of the spoolie boss by brazing methods, as well as optional machining of a borescope hole prior to or after attachment of the repair cover, greatly simplifies the repair process, thereby reducing the time required and cost of repair.
摘要翻译: 燃气涡轮发动机增压罩使用预制的修理盖SPAD进行修理。 SPAD修理盖具有一个卷轴凸台,其在连接到增压室铸件之前对准并附接到修理增压罩的主体,以形成修复的增压室。 通过钎焊方法来推动卷轴凸台,以及在安装维修盖之前或之后可选地加工孔眼镜孔,这大大简化了维修过程,从而减少了所需的时间和维修成本。
-
-