公开(公告)号：US20180065185A1

公开(公告)日：2018-03-08

申请号：US15695650

申请日：2017-09-05

Applicant: ROLLS-ROYCE plc ,  TWI LIMITED

Inventor： John H. BOSWELL ,  Jeffrey ALLEN ,  Carl HAUSER ,  Neil PREECE

IPC: B22F5/00 ,  B22F3/24 ,  B22F3/115 ,  F01D25/24

CPC classification number: B22F5/009 ,  B22F3/115 ,  B22F3/24 ,  B22F7/08 ,  B22F2003/1058 ,  B22F2003/248 ,  B22F2999/00 ,  B23P15/00 ,  F01D25/24 ,  F01D25/243 ,  F05D2230/30 ,  Y02T50/671 ,  B22F3/1115 ,  B22F2005/005

Abstract: A method of attaching a projection to a thin walled component, the thin walled component having a first surface and an opposite second surface, the method comprises the steps of: (i) providing a thin walled component; (ii) identifying a first position on the first surface of the thin walled component; (iii) building a hollow thin walled lattice structure on the second surface at a second position using a liquid metal deposition process, the second position corresponding to the first position; and (iv) building a projection on the first surface at the first position using a liquid metal deposition process.

公开(公告)号：US20160097295A1

公开(公告)日：2016-04-07

申请号：US14852032

申请日：2015-09-11

Applicant: ROLLS-ROYCE PLC

Inventor： Jeffrey ALLEN ,  Adrian WRIGHT ,  Anthony GRASSBY ,  Barry LOWE ,  Kevin O'SULLIVAN ,  Philip CARROLL ,  Philip Gordon MINION

IPC: F01D11/12 ,  F01D25/12 ,  B23K26/342 ,  F16J15/44

CPC classification number: F01D11/12 ,  B23K26/342 ,  F01D11/122 ,  F01D11/127 ,  F01D25/12 ,  F05D2220/32 ,  F05D2230/234 ,  F05D2230/30 ,  F05D2240/55 ,  F16J15/44

Abstract: A sealing element for positioning radially outwardly of aerofoil blades of a gas turbine engine is provided. A radially inner surface region of the sealing element includes a seal structure having one or more inwardly projecting walls formed by additive layer, powder fed, laser weld deposition. The walls form a plurality of curved profile shapes which are arranged in a repeating pattern across the radially inner surface region. None of the walls intersects with any other wall. The curved profile shapes have no radii of curvature less than 0.5 mm.

Abstract translation: 提供了一种用于定位在燃气涡轮发动机的翼型叶片的径向外侧的密封元件。 密封元件的径向内表面区域包括密封结构，该密封结构具有由添加层，粉末进料，激光焊接沉积形成的一个或多个向内突出的壁。 壁形成多个弯曲轮廓形状，其以跨过径向内表面区域的重复图案布置。 没有一个墙壁与任何其他墙壁相交。 弯曲的轮廓形状没有小于0.5mm的曲率半径。

公开(公告)号：US20140161520A1

公开(公告)日：2014-06-12

申请号：US14087670

申请日：2013-11-22

Applicant: ROLLS-ROYCE PLC

Inventor： Daniel CLARK ,  Ian Colin Deuchar CARE ,  Jeffrey ALLEN

IPC: F16B17/00

CPC classification number: B29C65/64 ,  B29C65/4835 ,  B29C65/54 ,  B29C65/565 ,  B29C66/1122 ,  B29C66/21 ,  B29C66/30321 ,  B29C66/41 ,  B29C66/45 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29C66/73753 ,  B29C66/73755 ,  B29C66/7394 ,  B29C66/742 ,  B29C66/7428 ,  B29L2031/08 ,  B29L2031/3085 ,  F16B2200/30 ,  Y10T156/10 ,  B29K2307/04 ,  B29K2063/00

Abstract: The invention relates to a joint including a substrate, optionally a metal substrate, and a body of material joined to the substrate, the body of material typically having a composite portion. An outer surface of the substrate is provided with a fastening projection for fastening the substrate to body of material, wherein the fastening projection has a stem and a plurality of branches having dendritic geometry projecting into the material of the body.

Abstract translation: 本发明涉及包括基底，可选地金属基底和连接到基底的材料体的接头，该材料体通常具有复合部分。 衬底的外表面设置有用于将衬底紧固到材料体的紧固突起，其中紧固突起具有杆和具有突出到身体的材料中的树枝状几何的多个分支。