公开(公告)号：US20160097325A1

公开(公告)日：2016-04-07

申请号：US14858535

申请日：2015-09-18

Applicant: ROLLS-ROYCE PLC

Inventor： Stephen Charles HARDING ,  Nicholas Alexander WORTH

IPC: F02C7/18 ,  F01D25/12 ,  F23R3/04

CPC classification number: F02C7/18 ,  F01D5/186 ,  F01D9/065 ,  F01D25/12 ,  F05D2250/13 ,  F05D2260/201 ,  F05D2260/202 ,  F23R3/002 ,  F23R3/04 ,  F23R3/06 ,  F23R2900/00018 ,  F23R2900/03041 ,  F23R2900/03042 ,  F23R2900/03043

Abstract: A cooled gas turbine engine component comprises a wall which has a plurality of effusion cooling apertures extending there-through from a first surface to a second surface. The apertures are arranged at an angle to the second surface and each aperture has an inlet in the first surface and an outlet in the second surface. Each aperture has a metering portion and a diffusing portion arranged in flow series and each metering portion is elongate and the width is greater than the length of the metering portion. Each diffusing portion increases in dimension in the length from the metering portion to the outlet. Each outlet has a rectangular shape in the second surface of the wall. Each inlet has an elongate shape in the first surface of the wall and the inlet in the wall is arranged substantially diagonally with respect to the outlet in the wall.

Abstract translation: 冷却的燃气涡轮发动机部件包括壁，该壁具有从第一表面延伸到第二表面的多个渗出冷却孔。 孔与第二表面成角度地布置，并且每个孔在第一表面中具有入口和在第二表面中具有出口。 每个孔具有流量系列布置的计量部分和扩散部分，每个计量部分是细长的，并且该宽度大于计量部分的长度。 每个漫射部分在从计量部分到出口的长度上增加尺寸。 每个出口在壁的第二表面中具有矩形形状。 每个入口在壁的第一表面中具有细长形状，并且壁中的入口相对于壁中的出口基本上对角地布置。

公开(公告)号：US20150241062A1

公开(公告)日：2015-08-27

申请号：US14608943

申请日：2015-01-29

Applicant: ROLLS-ROYCE PLC

Inventor： Stephen Charles HARDING

IPC: F23R3/00

CPC classification number: F23R3/002 ,  B22F3/105 ,  B22F3/1055 ,  B22F5/009 ,  B22F5/10 ,  B22F2003/1054 ,  C21B9/04 ,  F23R2900/00018 ,  F23R2900/03042 ,  Y02P10/295 ,  Y10T29/49231

Abstract: A combustion chamber wall is hollow, has a first surface and a second surface and includes a plurality of polyhedron shaped chambers defined by a matrix of integral interconnected walls. The walls of the chambers in a first layer define the first surface of the combustion chamber wall and the walls of the chambers in a third layer define the second surface of the combustion chamber wall. The chambers are fluidly interconnected by apertures extending through the integral interconnected walls of the chambers for the flow of coolant there-between. The walls of the chambers in the first layer have apertures extending there-through to supply coolant into the first layer and the walls of the chambers in the third layer have apertures extending there-through to supply coolant from the third layer into the combustion chamber. The combustion chamber wall is manufactured by additive layer manufacture.

Abstract translation: 燃烧室壁是中空的，具有第一表面和第二表面，并且包括由整体互连壁的矩阵限定的多个多面体形状的室。 在第一层中的室的壁限定燃烧室壁的第一表面，并且第三层中的室的壁限定燃烧室壁的第二表面。 腔室通过延伸通过腔室的整体互连壁的孔流体地互连，用于其间的冷却剂流。 第一层中的室的壁具有在其上延伸的孔，以将冷却剂供应到第一层中，并且第三层中的室的壁具有在其上延伸的孔，以将冷却剂从第三层供应到燃烧室中。 燃烧室壁由添加剂层制造制成。

公开(公告)号：US20160258624A1

公开(公告)日：2016-09-08

申请号：US15010800

申请日：2016-01-29

Applicant: ROLLS-ROYCE plc

Inventor： Stephen Charles HARDING ,  Paul Allan HUCKER ,  Giuseppe RALLO

IPC: F23R3/00 ,  F02C7/20

CPC classification number: F23R3/002 ,  F02C7/20 ,  F23R2900/00018 ,  F23R2900/03041 ,  F23R2900/03043 ,  F23R2900/03044

Abstract: A combustion chamber comprises an upstream ring structure, a downstream ring structure and a plurality of circumferentially arranged combustion chamber segments. Each combustion chamber segment extends the full length of the combustion chamber. Each combustion chamber segment comprises a frame structure and at least an inner wall and the frame structure and the inner wall are integral. An upstream end of each combustion chamber segment is secured to the upstream ring structure and a downstream end of each combustion chamber segment is mounted on the downstream ring structure. The combustion chamber segments are manufactured by additive layer manufacture. The combustion chamber segments have a stiff frame structure which carries the structural loads, the thermal loads, surge loads and flameout loads and the frame structure distributes loads into adjacent components.

Abstract translation: 燃烧室包括上游环结构，下游环结构和多个周向布置的燃烧室段。 每个燃烧室段延伸燃烧室的整个长度。 每个燃烧室段包括框架结构，并且至少内壁和框架结构以及内壁是一体的。 每个燃烧室段的上游端固定到上游环结构，并且每个燃烧室段的下游端安装在下游环结构上。 燃烧室段通过添加剂层制造制造。 燃烧室段具有刚性框架结构，其承载结构负载，热负荷，浪涌负载和熄火负载，并且框架结构将负载分配到相邻部件中。