IP Library Granted Patent US 9,410,703
Granted Patent B2
US 9,410,703 · App. 13/836,510 · Granted Aug 9, 2016

Device for injecting a mixture of air and fuel into a turbine engine combustion chamber

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Quick Facts
Patent No.
US 9,410,703
App. No.
13/836,510
Granted
Aug 9, 2016
Kind
B2
Abstract

A device for injecting a mixture of air and fuel into a turbine engine combustion chamber, the device including a mechanism for centering a fuel injector, which mechanism is movable radially in a support mechanism fastened to a wall of the chamber, the support mechanism carrying a retaining mechanism for axially retaining the centering mechanism on a side opposite from the chamber wall, the retaining mechanism being fastened in releasable manner to the support mechanism.

Claims (12)

1. A device for injecting a mixture of air and fuel into a turbine engine combustion chamber, the device comprising:

support means;

centering means for centering a fuel injector, said centering means being movable radially in the support means for fastening to a wall of the chamber, the support means carrying retaining means for axially retaining the centering means on a side opposite from the chamber wall, the retaining means are fastened in releasable manner to the support means,

wherein the retaining means comprise at least one peg carried by the support means, a latch engaged on the peg and holding the centering means against the support means, and a pin having one end portion engaged and prevented from moving in a housing of the peg and having an opposite end portion bearing against the latch to prevent the pin from moving relative to the peg.

2. A device according to claim 1 , wherein the support means comprise at least one radially outer wall or tab for guiding or bearing against the centering means, and wherein the retaining means are releasably fastened to said wall or tab.

3. A device according to claim 2 , wherein the support means comprise two diametrically opposite tabs extending radially outwards.

4. A device according to claim 3 , wherein the centering means comprise two radially outer tabs that are diametrically opposite and that are held against the tabs of the support means by the retaining means that pass through orifices or notches in the tabs of the centering means with circumferential and radial clearance.

5. A device according to claim 4 , wherein the tabs of the centering means are held against the tabs of the support means by two mutually independent retaining means.

6. A device according to claim 5 , wherein the latch includes a groove into which the end portion of the pin remote from the peg is folded down by plastic deformation.

7. A device according to claim 6 , wherein the housing in the peg is L-shaped and includes a transverse passage receiving one end of the pin and a longitudinal slot connecting the transverse passage to one end of the peg.

8. A device according to claim 7 , wherein an axis of elongation (D) of the slot in the peg is in alignment on a longitudinal axis (C) of the peg or is parallel to said axis and spaced apart therefrom.

9. A device according to claim 8 , wherein the peg is engaged in an orifice of the support means and includes an annular shoulder bearing axially against the support means, the shoulder including a substantially planar portion configured to engage with a complementary shape of the support means.

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 Jun 27, 2013
From: BUNEL, JACQUES MARCEL ARTHUR; ULRYCK, GILLES
To: SNECMA
Reel/Frame 030702/0160 →