公开(公告)号：US20150047360A1

公开(公告)日：2015-02-19

申请号：US13965657

申请日：2013-08-13

Applicant: General Electric Company

Inventor： Abinash Baruah ,  Gilbert Otto Kraemer ,  Predrag Popovic ,  William Francis Carnell, JR.

IPC: F23R3/28

CPC classification number: F23R3/34 ,  F23R3/28 ,  F23R3/346

Abstract: A system for injecting a liquid fuel into a combustion gas flow field includes an annular liner that defines a combustion gas flow path. The annular liner includes an inner wall, an outer wall and a fuel injector opening that extends through the inner wall and the outer wall. The system further includes a gas fuel injector that is coaxially aligned with the fuel injector opening. The gas fuel injector includes an upstream end and a downstream end. The downstream end terminates substantially adjacent to the inner wall. A dilution air passage is at least partially defined by the gas fuel injector. A liquid fuel injector extends partially through the dilution air passage. The liquid fuel injector includes an injection end that terminates upstream from the inner wall.

Abstract translation: 用于将液体燃料喷射到燃烧气体流场中的系统包括限定燃烧气体流动路径的环形衬套。 环形衬套包括延伸穿过内壁和外壁的内壁，外壁和燃料喷射器开口。 该系统还包括与燃料喷射器开口同轴对准的气体燃料喷射器。 气体燃料喷射器包括上游端和下游端。 下游端基本上靠近内壁终止。 稀释空气通道至少部分地由气体燃料喷射器限定。 液体燃料喷射器部分地延伸穿过稀释空气通道。 液体燃料喷射器包括从内壁的上游终止的喷射端。

公开(公告)号：US20170184310A1

公开(公告)日：2017-06-29

申请号：US15458545

申请日：2017-03-14

Applicant: General Electric Company

Inventor： Abinash Baruah ,  Gilbert Otto Kraemer ,  Predrag Popovic ,  William Francis Carnell, JR.

IPC: F23R3/34

CPC classification number: F23R3/34 ,  F23R3/28 ,  F23R3/346

Abstract: A system for injecting a liquid fuel into a combustion gas flow field includes an annular liner that defines a combustion gas flow path. The annular liner includes an inner wall, an outer wall and a fuel injector opening that extends through the inner wall and the outer wall. The system further includes a gas fuel injector that is coaxially aligned with the fuel injector opening. The gas fuel injector includes an upstream end and a downstream end. The downstream end terminates substantially adjacent to the inner wall. A dilution air passage is at least partially defined by the gas fuel injector. A liquid fuel injector extends partially through the dilution air passage. The liquid fuel injector includes an injection end that terminates upstream from the inner wall.

公开(公告)号：US20140260302A1

公开(公告)日：2014-09-18

申请号：US13804199

申请日：2013-03-14

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Arvind Venugopal Menon ,  Gilbert Otto Kraemer ,  Predrag Popovic ,  Abinash Baruah

IPC: F23R3/36 ,  F23R3/14

CPC classification number: F23R3/36 ,  F23R3/14

Abstract: The present application and the resultant patent provide a diffusion combustor fuel nozzle for a gas turbine engine. The fuel nozzle may include one or more gas fuel passages for one or more flows of gas fuel, a swirler surrounding the one or more gas fuel passages and positioned about a downstream face of the fuel nozzle, a number of swirler gas fuel ports defined in the swirler, and a number of downstream face gas fuel ports defined in the downstream face of the fuel nozzle. The swirler may include a number of swirl vanes and a number of air chambers defined between adjacent swirl vanes. The present application and the resultant patent further provide a method of operating a diffusion combustor fuel nozzle of a gas turbine engine.

Abstract translation: 本申请和所得专利提供了一种用于燃气涡轮发动机的扩散燃烧器燃料喷嘴。 燃料喷嘴可以包括用于一个或多个气体燃料流的一个或多个气体燃料通道，围绕一个或多个气体燃料通道并围绕燃料喷嘴的下游侧定位的旋流器，多个旋流器气体燃料端口限定在 旋流器和限定在燃料喷嘴的下游面中的多个下游面气体燃料端口。 旋流器可以包括多个旋流叶片和限定在相邻旋流叶片之间的多个空气室。 本申请和所得到的专利还提供了一种操作燃气轮机的扩散燃烧器燃料喷嘴的方法。