Engine aft section structure

Patent metadata

Field	Value
Publication number	US-10830180-B2
Application number	US-201715671788-A
Country	US
Kind code	B2
Filing date	Aug 8, 2017
Priority date	Jun 16, 2015
Publication date	Nov 10, 2020
Grant date	Nov 10, 2020

Abstract

An aft section structure of a jet engine with an axis is comprised of a casing defining a duct around the axis and opened axially fore and aft; a cone tapering aftward at a first angle with the axis and having a pointed end; guide vanes, each of the vanes radially extending from the cone to the casing and comprising a pressure side at a second angle with a plane containing the axis; spray bars, each of the spray bars extending radially within the duct and comprising trailing sides, each of the trailing sides being directed aftward at a third angle with a plane containing the axis; and flame holders, each of the flame holders extending radially within the duct and comprising one or more interior sides, each of the interior sides being directed aftward at a fourth angle with a plane containing the axis.

First claim

What is claimed is:

1. An aft section structure of a jet engine having an axis, comprising:
a casing defining a duct around the axis and opened axially fore and aft;
a cone tapering aftward at a first angle with the axis and having a pointed end;
one or more guide vanes, each of the one or more guide vanes radially extending from the cone to the casing and comprising a pressure side at a second angle with the plane containing the axis;
one or more spray bars, each of the one or more spray bars extending radially within the duct and comprising one or more trailing sides, each of the one or more trailing sides being directed aftward at a third angle with the plane containing the axis; and
one or more flame holders, each of the one or more flame holders extending radially within the duct and comprising one or more interior sides, each of the one or more interior sides being directed aftward at a fourth angle with plane containing the axis,
wherein any of the first, the second, the third, and the fourth angles is between 0 and 45 degrees, and
wherein the first, the second, the third, and the fourth angles are identical.

2. The aft section structure of claim 1 , wherein, when viewed from an axially back, the one or more spray bars expose only the one or more trailing sides and the one or more flame holders expose only the one or more interior sides.

Assignees

• Ihi Corp

Inventors

• Tanaka Shinji
• Takahashi Katsuyoshi
• Hosoi Jun

Classifications

• F23R3/18 Primary

  Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants · CPC title

• F02K3/10 Primary

  by after-burners (F02K3/105 takes precedence) · CPC title

• F02K1/78

  Other construction of jet pipes · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title