IP Library Granted Patent US 9,188,338
Granted Patent B2
US 9,188,338 · App. 13/522,511 · Granted Nov 17, 2015

Injector device and combustion chamber for a turbomachine provided with such injector device

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Quick Facts
Patent No.
US 9,188,338
App. No.
13/522,511
Granted
Nov 17, 2015
Kind
B2
Abstract

A low-cost combustion chamber injector device that has sturdier construction and is safer for use. Parts are configured specifically to be nested, to dispense with welding between the cellular parts. The device for injecting a fuel-air mix includes, centered on a single axis, a swirl chamber including at least two annular air suction parts, a centering guide, and a retainer ring. The annular parts have cellular conduits connecting to axial inner and outer Venturi tubes. The parts are coaxially mounted, the inner part being configured to be self-centered in the outer part by engagement of the axial and radial walls and then, after assembly, the outer part is welded to the retainer ring and to the inner part in a single radial plane.

Claims (16)

1. A fuel-air mix injector device comprising, centered on a same axis:

a swirl chamber including at least an external annular air suction part and an internal annular air suction part;

a centering guide; and

a retainer ring;

wherein the annular parts present cellular conduits opening into external and internal coaxial Venturi tubes formed by internal axial walls, and the parts are coaxially mounted,

the internal part is configured to be self-centered in the external part by contacting axial and radial walls, and

the retainer ring, the external part, and the internal part are welded together in a same radial plane along opposite radial faces, the retainer ring capping the centering guide so as to hold it in a radial housing.

2. The injector device according to claim 1 , wherein air conduits of the external part are cylindrical and regularly distributed on two crowns orthogonally to the axis, the conduits of one crown being oriented according to an angle of an opposed direction compared to one of the conduits of the other crown with respect to a radius from the axis.

3. The injector device according to claim 1 , wherein angles of opposed directions formed between the conduits and radii pass through the symmetry axis and the center of the conduits in the periphery of the injector device are between ±20° ands 40°.

4. The injector device according to claim 1 , wherein the conduits of the internal part are arranged in an extension of the conduits of one crown of the external part and open into an internal Venturi tube, the conduits of the other crown of the external part opening into a space formed between the internal and external Venturi tubes.

5. The injector device according to claim 4 , wherein the conduits of the internal part are realized in an extension of the conduits of one crown of the external part after centering the internal part in the external part and welding with the retainer ring.

6. The injector device according to claim 2 , wherein the conduits are of a section having substantially a same dimension in at least two perpendicular directions.

7. The injector device according to claim 2 , wherein a number of conduits of one crown is equal to that of the other crown and the crowns are offset by half a pitch on a periphery of the external part.

8. The injector device according to claim 1 , wherein the retainer ring presents a bevelled edge configured to make positioning of the internal part on the external part easier.

9. The injector device according to claim 1 , wherein the centering guide includes a collar and is adaptable in position into a radial housing made between a radial wall of the retainer ring and a radial wall of the internal part through an adapted dimensioning of the retainer ring and/or the collar of the centering guide.

10. A combustion chamber comprising an injector device according to claim 1 , comprising an annular wall and a bottom wall, fastening means for the injector device being arranged in the chamber bottom wall presenting a passage opening for a fuel injection nozzle being coupled to the centering guide of the injector device.

Assignments (2)
CHANGE OF NAME Recorded May 11, 2018
From: TURBOMECA
To: SAFRAN HELICOPTER ENGINES
Reel/Frame 046127/0021 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 23, 2012
From: BERTEAU, PATRICK; CARRERE, BERNARD JOSEPH JEAN-PIERRE; HERNANDEZ, LORENZO HUACAN; NAUDOT, LUDOVIC ANDRE JOEL
To: TURBOMECA
Reel/Frame 028611/0693 →