公开(公告)号：US20170003030A1

公开(公告)日：2017-01-05

申请号：US15107282

申请日：2014-12-23

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Michael Anthony BENJAMIN ,  Joshua Tyler MOOK ,  Sean James HENDERSON ,  Ramon MARTINEZ

IPC: F23R3/28 ,  F23R3/14

CPC classification number: F23R3/283 ,  F23D11/386 ,  F23D2209/30 ,  F23R3/14 ,  F23R3/286 ,  F23R3/34 ,  F23R3/346 ,  F23R2900/00004

Abstract: A fuel nozzle includes an outer body extending parallel to a centerline axis, having a generally cylindrical exterior surface, forward and aft ends, and a plurality of openings through the exterior surface. The fuel nozzle further includes an inner body inside the outer body, cooperating with the outer body to define an annular space, and a main injection ring inside the annular space, the main injection ring including fuel posts extending therefrom. Each fuel post is aligned with one of the openings and separated from the opening by a perimeter gap which communicates with the annular space. There is a circumferential main fuel gallery in the main injection ring, and a plurality of main fuel orifices, wherein each orifice communicates with the main fuel gallery and extends through one of the fuel posts.

Abstract translation: 燃料喷嘴包括平行于中心线延伸的外体，具有大致圆柱形的外表面，前端和后端以及穿过外表面的多个开口。 燃料喷嘴还包括在外体内的内体，与外体配合以限定环形空间，以及环形空间内的主注射环，主注射环包括从其延伸的燃料柱。 每个燃料柱与其中一个开口对准并且与开口分隔开与环形空间连通的周边间隙。 在主注射环中存在周向主燃料流道和多个主燃料孔，其中每个孔与主燃料通道连通并且延伸穿过其中一个燃料柱。

公开(公告)号：US20190056113A1

公开(公告)日：2019-02-21

申请号：US16059474

申请日：2018-08-09

Applicant: General Electric Company

Inventor： Joshua Tyler MOOK ,  Michael Anthony BENJAMIN ,  David Richard BARNHART ,  Sean James HENDERSON ,  Ramon MARTINEZ ,  Neerav Atul PATEL ,  Mark Richard SHAW

IPC: F23R3/28 ,  F02C7/18 ,  F23R3/14 ,  B23P15/00 ,  B23P6/00

Abstract: An aft heat shield for a fuel nozzle tip includes: an annular shield wall; an annular shield flange extending radially outward from an aft end of the shield wall; an annular baffle flange surrounding the conical section, and disposed such that an axial gap is defined between the shield flange and the baffle flange, the baffle flange including a radially outer rim extending axially forward therefrom; and a plurality of impingement cooling holes passing through the baffle flange and oriented to as to direct air flow towards the shield wall.