公开(公告)号：WO2014171997A2

公开(公告)日：2014-10-23

申请号：PCT/US2014014593

申请日：2014-02-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LUTJEN PAUL M ,  BRUSKOTTER MICHAEL J

CPC classification number: F01D11/12 ,  F01D9/041 ,  F01D11/08 ,  F01D25/12 ,  F05D2220/32 ,  F05D2240/11 ,  F05D2240/12 ,  F05D2250/711 ,  F05D2250/712 ,  F05D2260/202

Abstract: A blade outer air seal (BOAS) segment according to an exemplary aspect of the present disclosure includes, among other things, a seal body having a radially inner face that circumferentially extend between a first mate face and a second mate face and axially extend between a leading edge face and a trailing edge face, wherein a radial position of the radially inner face varies at a given axial position.

Abstract translation: 根据本公开的示例性方面的叶片外部空气密封（BOAS）段包括其中具有径向内表面的密封体，所述径向内表面在第一配合面和第二配合面之间周向延伸并且在 前缘面和后缘面，其中径向内表面的径向位置在给定的轴向位置处变化。

公开(公告)号：EP2961940A4

公开(公告)日：2016-06-15

申请号：EP14785115

申请日：2014-02-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LUTJEN PAUL M ,  BRUSKOTTER MICHAEL J

IPC: F01D11/08 ,  F02C7/28

CPC classification number: F01D11/12 ,  F01D9/041 ,  F01D11/08 ,  F01D25/12 ,  F05D2220/32 ,  F05D2240/11 ,  F05D2240/12 ,  F05D2250/711 ,  F05D2250/712 ,  F05D2260/202

Abstract: A blade outer air seal (BOAS) segment according to an exemplary aspect of the present disclosure includes, among other things, a seal body having a radially inner face that circumferentially extend between a first mate face and a second mate face and axially extend between a leading edge face and a trailing edge face, wherein a radial position of the radially inner face varies at a given axial position.

公开(公告)号：EP3052787A4

公开(公告)日：2017-05-31

申请号：EP14851155

申请日：2014-09-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： STROCK CHRISTOPHER W ,  LUTJEN PAUL M ,  BRUSKOTTER MICHAEL J

IPC: F01D11/12

CPC classification number: F01D11/122 ,  C23C4/129 ,  C23C4/134 ,  C23C4/18 ,  C23C28/32 ,  C23C28/3455 ,  F01D11/02 ,  F05D2220/32 ,  F05D2230/312 ,  F05D2240/11 ,  F05D2240/55 ,  F16J15/40

Abstract: An air seal system for a rotor blade assembly of a gas turbine engine includes a substrate. An optional ceramic interlayer may be disposed on an optional bond coat deposited on the substrate. An erosion resistant thermal barrier coating (E-TBC) layer is disposed on the ceramic interlayer (if present) or on the bond coat, or on the substrate. An abradable layer is disposed on the erosion resistant thermal barrier coating (E-TBC) layer.

Abstract translation: 用于燃气涡轮发动机的转子叶片组件的气封系统包括基板。 可选的陶瓷夹层可以设置在沉积在基底上的可选粘合涂层上。 在陶瓷夹层（如果存在的话）上或在粘合涂层上或在基材上设置抗侵蚀热障涂层（E-TBC）层。 耐磨热障涂层（E-TBC）上设置耐磨层。