公开(公告)号：US20160084102A1

公开(公告)日：2016-03-24

申请号：US14489686

申请日：2014-09-18

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Surinder Singh PABLA ,  Luc Stephane LEBLANC ,  Donald Earl FLOYD

IPC: F01D11/12 ,  F16J15/16

CPC classification number: F01D11/122 ,  F05D2230/90 ,  F05D2250/181 ,  F05D2300/173 ,  F05D2300/2118 ,  F05D2300/608 ,  F05D2300/611 ,  F16J15/16 ,  F16J15/445 ,  Y02T50/671 ,  Y02T50/6765

Abstract: An abradable seal having a metallic substrate and a multi-layered ceramic coating on the metallic substrate. The multi-layered ceramic coating includes a base layer deposited on the metallic substrate, an abradable layer overlaying the first layer, and an abrading layer overlaying the second layer. The abrading layer is formed of an abrading material. A turbine system and a method for forming an abradable seal are also disclosed.

Abstract translation: 具有金属基底和在金属基底上的多层陶瓷涂层的耐磨密封件。 多层陶瓷涂层包括沉积在金属基底上的基底层，覆盖第一层的可磨损层和覆盖第二层的研磨层。 研磨层由研磨材料形成。 还公开了一种用于形成耐磨密封件的涡轮机系统和方法。

公开(公告)号：US20140271154A1

公开(公告)日：2014-09-18

申请号：US13828081

申请日：2013-03-14

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Donald Earl FLOYD ,  Kenneth Black

IPC: F01D25/14

CPC classification number: F01D25/14 ,  F01D11/20

Abstract: A turbine inner shell for a turbine engine includes one or more mounting grooves, each of which receives a fluid conduit. A temperature controlling fluid is circulated through fluid conduit to selectively heat or cool surrounding portions of the turbine inner shell, to thereby control the thermal growth of those portions of the turbine inner shell. This makes it possible to selectively control a clearance between the tips of rotating turbine blades and the surrounding shrouds of the turbine.

Abstract translation: 用于涡轮发动机的涡轮机内壳包括一个或多个安装槽，每个安装槽接收流体导管。 温度控制流体通过流体导管循环，以选择性地加热或冷却涡轮机内壳的周围部分，从而控制涡轮内壳的那些部分的热生长。 这使得可以选择性地控制旋转的涡轮叶片的尖端与涡轮的周围的护罩之间的间隙。