公开(公告)号：EP3077729A4

公开(公告)日：2017-01-11

申请号：EP14867187

申请日：2014-08-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BANGERTER JAMES P ,  RUSSO THOMAS R ,  HANSON RUSSELL B ,  LOW KEVIN J

IPC: F23R3/42 ,  F02C3/14 ,  F02C7/24 ,  F02K1/82 ,  F23M5/04 ,  F23R3/00 ,  F23R3/06 ,  F23R3/60

CPC classification number: F23R3/60 ,  F02C3/04 ,  F02C7/24 ,  F02K1/822 ,  F05D2260/30 ,  F23M5/04 ,  F23R3/002 ,  F23R3/06 ,  F23R2900/00018 ,  F23R2900/03042 ,  Y02T50/675

Abstract: A wall assembly is provided for a gas turbine engine. This wall assembly includes a support shell with a contoured region; and a multiple of liner panels mounted to the support shell. At least one of the multiple of liner panels includes an end rail. The contoured region is deformable to selectively contact at least a portion of the end rail. A method of assembling a wall assembly within a gas turbine engine is also provided. This method includes locating a stud that extends from a cold side of a liner panel through a support shell; and attaching a fastener onto the stud to at least partially close a gap defined between the panel and shell.

Abstract translation: 为燃气涡轮发动机提供壁组件。 该壁组件包括具有轮廓区域的支撑壳; 以及安装到支撑壳体上的多个衬板。 多个衬板中的至少一个包括端轨。 轮廓区域可变形以选择性地接触端轨的至少一部分。 还提供了组装在燃气涡轮发动机内的壁组件的方法。 该方法包括定位从衬板的冷侧延伸穿过支撑壳的螺柱; 以及将紧固件附接到所述螺柱上以至少部分地闭合限定在所述面板和壳体之间的间隙。