公开(公告)号：US20160116169A1

公开(公告)日：2016-04-28

申请号：US14869410

申请日：2015-09-29

Applicant: United Technologies Corporation

Inventor： David J. Hyland

IPC: F23R3/28 ,  F23R3/60 ,  F23R3/00

CPC classification number: F23R3/286 ,  F23R3/14 ,  F23R3/283 ,  F23R2900/00017 ,  F23R2900/00018 ,  F23R2900/00019

Abstract: Aspects of the disclosure are directed to methods and systems associated with a gas turbine engine of an aircraft. In some embodiments, a surface of a liner of the gas turbine engine is coupled to a fuel/air mixer, and a surface of a panel of the engine is coupled to the mixer such that a portion of the mixer is disposed between the liner surface and the panel surface.

Abstract translation: 本公开的方面涉及与飞行器的燃气涡轮发动机相关联的方法和系统。 在一些实施例中，燃气涡轮发动机的衬套的表面联接到燃料/空气混合器，并且发动机的面板的表面耦合到混合器，使得混合器的一部分设置在衬套表面 和面板表面。