IP Library Granted Patent US 7,856,828
Granted Patent B2
US 7,856,828 · App. 11/693,177 · Granted Dec 28, 2010

Flameholder arm for an afterburner

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Quick Facts
Patent No.
US 7,856,828
App. No.
11/693,177
Granted
Dec 28, 2010
Kind
B2
Abstract

A flameholder arm for an afterburner of a turbomachine, particularly a jet engine, is disclosed. The arm includes a ventilation duct which is centered and immobilized inside the arm independent of the heatshield. The duct also includes a transverse lip which includes an orifice for centering and guiding a fuel injection harness. The transverse lip prevents the harness from being positioned in any way incorrectly in the arm.

Claims (26)

1. A flameholder arm for an afterburner, comprising:

a body in the form of an open dihedron, the body including a base disposed at a radially innermost end of the body and an orifice which is disposed in the base of the body;

a ventilation duct which extends inside the body and includes a centering finger at a radially innermost end of the ventilation duct which is engaged in the orifice disposed in the base of the body and a transverse lip which extends inside the body of the arm towards an open face of the dihedron;

a fuel injection harness which extends inside the body along the ventilation duct, and

a heatshield fixed to the body and which closes the open face of the dihedron,

wherein the ventilation duct is immobilized in the body of the arm independent of the heatshield,

wherein the transverse lip includes a guide orifice which centers the fuel injection harness, and

wherein a space is provided between the transverse lip and the heatshield.

2. The arm as claimed in claim 1 , wherein the ventilation duct centering finger passes through the orifice in the body and immobilizes the duct on the body of the arm.

3. The arm as claimed in claim 1 , wherein the centering finger comprises an annular shoulder of the centering finger abuts against the edge of the orifice in the body of the arm on the inside of the arm.

4. The arm as claimed in claim 2 , wherein the radially innermost end of the finger which extends externally from the arm retains the centering finger in the orifice.

5. The arm as claimed in claim 4 , wherein an annular component is fixed by brazing or welding to the radially innermost end of the centering finger.

6. The arm as claimed in claim 5 , wherein a shoulder of the centering finger is pressed against the arm by the annular component fixed to the radially innermost end of the centering finger.

7. The arm as claimed in claim 5 , wherein the annular component comprises at least one flat which cooperates with a corresponding element of the arm in order to prevent the finger from rotating in the orifice.

8. The arm as claimed in claim 1 , wherein the transverse lip of the duct occupies almost all of the available space inside the arm so as to prevent the fuel injection harness from being fitted incorrectly.

9. The arm as claimed in claim 1 , wherein the ventilation duct is formed as a single piece with the finger and the transverse lip.

10. A ventilation duct of a flameholder arm comprising:

a first end which is open; and

a second end opposite the first end formed with a substantially axial finger; and

a transverse lip including a through-orifice with an axis substantially parallel to an axis of the duct,

wherein the finger includes an annular shoulder which bears against a support, and

wherein the axial finger is circular, and

wherein a space is provided between the transverse lip and a heatshield disposed in the flameholder arm.

11. A turbomachine, such as an airplane jet engine, and which comprises at least one flameholder arm as claimed in claim 1 .

12. The arm as claimed in claim 1 , wherein the orifice is formed in an end wall of a small indentation in the base of the body, and the end wall is perpendicular to an axis of the ventilation duct.

13. The arm as claimed in claim 1 , wherein the traverse lip is an angular sector and a space is provided between side walls of the traverse lip and side walls of the body of the arm.

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 29, 2007
From: BUNEL, JACQUES MARCEL ARTHUR; GIRARD, NICOLAS PIERRE-MARIE
To: SNECMA
Reel/Frame 019086/0185 →