公开(公告)号：US20170009995A1

公开(公告)日：2017-01-12

申请号：US15185596

申请日：2016-06-17

Applicant: ROLLS-ROYCE plc

Inventor： Frederic WITHAM ,  Steven P JONES ,  Jonathan M GREGORY ,  Timothy MINCHIN ,  David CLARKE ,  David STEELE

IPC: F23R3/28 ,  F23R3/14 ,  F02C3/00

CPC classification number: F23R3/286 ,  F02C3/00 ,  F23D11/24 ,  F23D11/383 ,  F23D2900/11101 ,  F23R3/14 ,  F23R3/30 ,  F23R2900/00012

Abstract: A fuel spray nozzle comprises a fuel passage (1) having at least one inlet and at least one outlet. The outlet is configured for accelerating fuel exiting the fuel passage into a jet. An air swirler (3) is arranged outboard of the fuel passage and converges to a single outlet chamber (5) adjacent the fuel passage outlet(s). The air swirler (3) can be nominally concentrically arranged but have some freedom to move axially or radially or change its angular position. The fuel passage outlets may be arranged symmetrically in an annular configuration. An air passage may be arranged axially within the annular array of fuel passage outlets.

Abstract translation: 燃料喷嘴包括具有至少一个入口和至少一个出口的燃料通道（1）。 出口构造成将从燃料通道排出的燃料加速成射流。 空气旋流器（3）布置在燃料通道的外侧并且会聚到与燃料通道出口相邻的单个出口室（5）。 空气旋流器（3）可以名义上同心地布置，但是具有沿轴向或径向移动或改变其角位置的一些自由度。 燃料通道出口可以对称地布置在环形构造中。 空气通道可以轴向布置在燃料通道出口的环形阵列内。

公开(公告)号：US20170067641A1

公开(公告)日：2017-03-09

申请号：US15245035

申请日：2016-08-23

Applicant: ROLLS-ROYCE plc

Inventor： Frederic WITHAM ,  Pierre HILT ,  Steven P. JONES ,  Jonathan M. GREGORY ,  Timothy MINCHIN

IPC: F23R3/58 ,  F02C3/04

Abstract: An annular air swirler configured to receive a fuel injector in a central bore. The swirler has one or more annular channels, defined by radially facing channel walls and having an inlet for receiving compressed air and an axially distal outlet. The channel walls converge inwardly towards the outlet and swirl vanes extend between opposing faces of the walls. The swirler turns incoming air to create a vortex at the channel outlet. An annular cooling apparatus associated with the air swirler is arranged axially adjacently downstream of the channel outlet(s), and includes a skirt portion radially spaced from a converging portion of the outermost channel wall defining a converging portion of a bowed coolant channel. A radially outwardly extending wall connects with the outermost channel wall and, with a face of the skirt portion, defines a radially outwardly extending portion of the bowed coolant channel adapted for increased heat exchange.

Abstract translation: 环形空气旋流器，其构造成在中心孔中接收燃料喷射器。 旋流器具有由径向面对的通道壁限定的一个或多个环形通道，并且具有用于接收压缩空气和轴向远端出口的入口。 通道壁向内朝向出口汇合，并且涡流叶片在壁的相对面之间延伸。 旋流器使进入的空气在通道出口处产生涡流。 与空气旋流器相关联的环形冷却装置在通道出口的下游轴向相邻地布置，并且包括与限定弯曲冷却剂通道的会聚部分的最外通道壁的会聚部分径向间隔开的裙部。 径向向外延伸的壁与最外面的通道壁连接，并且裙部的一个表面限定了适合于增加热交换的弯曲冷却剂通道的径向向外延伸的部分。