IP Library Granted Patent US 8,307,658
Granted Patent B2
US 8,307,658 · App. 12/394,570 · Granted Nov 13, 2012

Flame holder for an afterburner duct of a jet engine with a spacer shoe, afterburner duct, and jet engine comprising an afterburner duct

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Quick Facts
Patent No.
US 8,307,658
App. No.
12/394,570
Granted
Nov 13, 2012
Kind
B2
Abstract

A flame holder for an afterburner duct of a jet engine, including an arm in the form of a gutter forming a cavity, a shield for protecting the cavity of the arm from heat, and an air supply baffle housed in the cavity, is disclosed. The arm, the protective shield, and the air supply baffle are held together by a one-piece spacer shoe.

Claims (20)

1. A flame holder for an afterburner duct of a jet engine, comprising:

an arm in the form of a gutter forming a cavity;

a shield for protecting the cavity of the arm from heat; and

an air supply baffle housed in the cavity,

wherein the arm, the protective shield and the air supply baffle are held together by a one-piece spacer shoe comprising a central branch, at least one lateral branch extending axially from the central branch, and at least one spacer lug disposed at an end of the at least one lateral branch designed to form a gap between the protective heat shield and at least one wall of the arm, the spacer lug including a fastening orifice, and a stud passes through the at least one wall of the arm, the fastening orifice, and the protective heat shield.

2. The flame holder as claimed in claim 1 , wherein the shoe comprises a means for retaining the air supply baffle.

3. The flame holder as claimed in claim 1 , wherein a fuel injector is placed inside said cavity of the arm.

4. The flame holder as claimed in claim 3 , wherein the shoe comprises a means for centering the injector.

5. The flame holder as claimed in claim 4 , wherein the shoe comprises a means for retaining the air supply baffle.

6. The flame holder as claimed in claim 1 , wherein the shoe is welded to the air supply baffle.

7. A jet engine afterburner duct comprising at least one flame holder as claimed in claim 1 .

8. A jet engine comprising an afterburner duct as claimed in claim 7 .

9. The flame holder as claimed in claim 1 , wherein a thickness of the at least one lateral branch is less than a thickness of the central branch.

10. A flame holder for an afterburner duct of a jet engine, comprising:

an arm in the form of a gutter forming a cavity;

a shield for protecting the cavity of the arm from heat; and

an air supply baffle housed in the cavity,

wherein the arm, the protective shield and the air supply baffle are held together by a one-piece spacer shoe comprising at least one spacer lug designed to form a gap between the protective heat shield and at least one wall of the arm, and

wherein the shoe takes the form of a Y defining a central branch and two lateral branches, the central branch comprising a through orifice for retaining the air supply baffle.

11. The flame holder as claimed in claim 10 , wherein a fuel injector is placed inside said cavity of the arm, the central branch comprising a through orifice for centering the injector.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 2, 2009
From: BUNEL, JACQUES MARCEL ARTHUR; VUILLEMENOT, YANN FRANCOIS JEAN-CLAUDE
To: SNECMA
Reel/Frame 022329/0481 →