Annular assembly for a turbomachine

Abstract

The invention relates to an annular assembly for a dual-flow turbomachine having a longitudinal axis (A) and comprising a casing (12) with an annular shell (14), one face of which supports a piece of annular equipment, a plurality of means of attachment (18) for attaching the equipment to the annular shell (14) being distributed around the longitudinal axis (A) and allowing the equipment (16) a degree of freedom in the tangential direction relative to the annular shell (14), characterised in that each means of attachment (18) comprises a rail (20) integral with the annular equipment (16) and arranged radially between a first radially internal plate (22) and a second, radially external plate (24) and capable of sliding in the tangential direction between the first plate (22) and the second plate (24), and in that a removable support element (56) is securely connected to the annular shell and to the first plate (22) and second plate (24).

Claims

1. An annular assembly for a dual-flow turbomachine having a longitudinal axis and comprising a casing with an annular shell, one face of which supports a piece of annular equipment, a plurality of means of attachment for attaching the equipment to the annular shell being distributed around the longitudinal axis and allowing the equipment a degree of freedom in the tangential direction relative to the annular shell, characterised in that each means of attachment comprises a rail integral with the annular equipment and arranged radially between a first radially internal plate and a second radially external plate and capable of sliding in the tangential direction between the first plate and the second plate, and in that a removable support element is securely connected to the annular shell and to the first plate and second plate, wherein the annular shell is an external annular shell of an annular flow path of a secondary air stream, the equipment being carried by a radially internal face of the external shell and wherein the equipment is a heat exchanger made of a material having a coefficient of thermal expansion greater than that of a material of the casing shell.

2. An assembly according to claim 1, in which the rail comprises an opening with a closed outline delimited internally by at least two edges which are substantially tangential in relation to each other in the longitudinal direction of first two tangential faces of the first plate or of the second plate and ensuring the guiding of the rail in the tangential direction.

3. An assembly according to claim 2, wherein said two first tangential faces are each formed on the first plate and are connected to two second tangential retaining faces radially inward of the rail, the two first tangential faces forming, with the two second tangential faces, an L-shaped section.

4. An assembly according to claim 2, wherein the two first tangential faces and/or the two second tangential faces are formed on the first plate.

5. An assembly according to claim 3, wherein the two first tangential faces and/or the two second tangential faces are formed on the first plate.

6. An assembly according to claim 1, wherein the first plate comprises a central tubular portion tightly engaged in an orifice of the second plate.

7. An assembly according to claim 2, wherein the first plate comprises a central tubular portion tightly engaged in an orifice of the second plate.

8. An assembly according to claim 3, wherein the first plate comprises a central tubular portion tightly engaged in an orifice of the second plate.

9. An assembly according to claim 4, wherein the first plate comprises a central tubular portion tightly engaged in an orifice of the second plate.

10. An assembly according to claim 1, wherein the removable support element comprises at least one rod integral with the first plate.

11. An assembly according to claim 2, wherein the removable support element comprises at least one rod integral with the first plate.

12. An assembly according to claim 3, wherein the removable support element comprises at least one rod integral with the first plate.

13. An assembly according to claim 10, wherein the said rod is a threaded rod screwed into the first plate and comprising a flat bearing on a face of the annular shell opposite that carrying the equipment.

14. An assembly according to claim 1, in which elastic means are elastically constrained in the radial direction between the first plate and the rail.

15. An assembly according to claim 14, wherein the first plate comprises a housing for receiving elastic means, such as for example a wave washer.

16. An assembly according to claim 2, wherein the outline comprises a convex edge delimiting a part of the rail serving for the radial support of the elastic means.

17. An assembly according to claim 14, wherein the outline comprises a convex edge delimiting a part of the rail serving for the radial support of the elastic means.

18. An assembly according to claim 1, wherein the heat exchanger made of aluminium and the casing shell is made of titanium.

19. Method for mounting the assembly according to claim 1, in which: for each of the first means of attachment, the rail is arranged between the first plate and the second plate fastened to each other, the rail being made integral with a radially external face of the heat exchanger, then the assembly carried out in the preceding step is presented opposite the radially internal face of the annular shell and the support elements are secured to one of the first plate and the second plate.

Description

BRIEF DESCRIPTION OF THE FIGURES

(1) FIG. 1, already described above, is a schematic perspective view of a turbomachine according to the prior art;

(2) FIG. 2, already described above, is a schematic perspective view of a portion of an annular heat exchanger mounted in the turbomachine of FIG. 1;

(3) FIG. 3 is a schematic perspective view of a heat exchanger according to the invention comprising means of attachment with a degree of freedom in the tangential direction;

(4) FIG. 4A is a schematic perspective view of the main element of the means of attachment according to the invention;

(5) FIG. 4B is a schematic perspective view of the main element of the means of attachment according to the invention;

(6) FIG. 5 is a schematic sectional view of the means of attachment, the heat exchanger and an annular shell of a casing according to the sectional plane W of FIG. 4A (shown on 3 or 4A of the sectional plane);

(7) FIG. 6 is a schematic view, in perspective, of a turbine engine blade Performance according to the invention.

DETAILED DESCRIPTION

(8) FIG. 3 shows an annular equipment for the turbomachine. This equipment 16 is a heat exchanger and the invention will be described below in relation to this specific piece of equipment but is also applicable to other equipment.

(9) The body of the heat exchanger 16 is usually made by extrusion of a good heat-conducting material such as aluminium. With such a process, it is thus possible to make the ducts in the thickness of the exchanger 16. Only a portion of the angular sector of exchanger 16 is shown in FIG. 3. This heat exchanger 16 comprises internal ducts for the circulation of oil to be cooled. The circumferential ends of the exchanger 16 have inserts that allow oil recirculation.

(10) The exchanger 16 comprises a plurality of means of attachment 18 for attaching the exchanger 16 to the external annular shell 14 which is shown in FIG. 5. It should be noted immediately that the exchanger 16 can be attached to an internal annular casing shell without the need for a new description so that it is understood that what applies to the external annular shell 14 also applies to an internal annular shell.

(11) The means of attachment 18 of the heat exchanger 16 are distributed around the circumference of the heat exchanger 16, i.e. around the longitudinal axis A of the turbomachine. FIG. 3 shows two annular rows of means of attachment 18.

(12) As will be explained in the following, each means of attachment 18 allows a connection with one degree of freedom in the tangential direction of the heat exchanger 16 with the external annular shell 14. Thus, each means of attachment 18 comprises a rail 20 integral with the heat exchanger 16 and inserted radially between a first plate 22 and a second plate 24.

(13) The rail 20 has a substantially rectangular shape with an internal opening 26 which is closed in outline. This rail 20 thus comprises two rectilinear uprights 28 which are oriented in a tangential direction and are connected to each other by a first end section 30 and a second end section 32. The first end section 30 and the second end section 32 each comprise an orifice 34 for a fastening screw 36 to secure the rail 20 to radially external bosses 38 of the heat exchanger 16 (FIG. 5). The first end section 32 of the rail 20 also comprises a section 40 forming a tongue extending inwardly into the opening 26. More specifically, the outline of the opening 26 is delimited by two tangential parallel edges 26a, 26b of which a first edge 26a is formed on a first straight upright 28 and a second edge 26b is formed on a second straight upright 28, by a longitudinal edge 26c and by a convex curved edge 26d tangentially opposite the longitudinal edge 26c. This convex edge 26d is connected to the ends of the longitudinal edges 26a, 26b and, together with these, delimit two slots 42 with the external outline of the tongue 40.

(14) The first plate 22 also has an approximately rectangular shape. It has a central tubular portion 44 passing through the opening 26 of the rail 20. This tubular portion 44 is tightly engaged in an orifice 46 of the second plate 24. The first plate 22 comprises two parts extending tangentially to an L-shaped section 48 formed on either side of the tubular portion 44 and each formed by a first tangential face 48a and a second tangential face 48b. The first tangential faces 48a are longitudinally opposed to the first 26a and second 26b edges of the outline of the opening 26 of the rail 20 so as to allow tangential guiding of the rail 20. The second tangential faces 48b provide a radially inward retention of the rail 20 on the first plate 22.

(15) As can be seen in FIG. 4B, the first plate 22 comprises an end portion with a concave curved edge 50 facing the convex curved edge of the tongue 40 of the rail 20. The end portions of the concave curved edge 50 are designed to fit into the above-mentioned slots 42 of the rail 20, thus improving the compactness of each means of attachment 18. One tangential end of the first plate 22 comprises a housing 52 in which are mounted elastic means 54 capable of elastic deformation in the radial direction. These elastic means 54 are for example a wave washer as shown in FIG. 6. They can be elastically prestressed during the mounting between the first plate 22 and rail 20, here more specifically the tongue 40 of the rail 20.

(16) Note that the first plate 22 has a longitudinal dimension greater than the longitudinal dimension of the opening of the rail 20 (FIGS. 4A and 4B). More specifically, the rectilinear uprights 28 of the rail 20 are able to slide on the second plate 24 on either side of its orifice 46 for mounting the tubular portion 44 of the first plate 22.

(17) Although not shown, the first 48a tangential sliding guide faces of the first 26a and second 26b edges of the rail 20 could be formed on the second plate 24.

(18) As can be seen in FIG. 5, a removable support element 56 is mounted on the annular shell 14 and comprises a flat 56a bearing on the radially external face of the external annular shell 14 and a rod 56b screwed into the tubular portion 44 of the first plate 22. When so mounted, the first plate 22 and the second plate 24 are fastened integrally to the external annular shell 14.

(19) Each of the means of attachments 18 with a tangential degree of freedom 18 is mounted as follows: the rail 20 is arranged between the first plate 22 and the second plate 24 fastened to each other, the rail 20 being made integral with a radially external face of the heat exchanger 16, then the assembly carried out in the previous step is presented opposite the radially internal face of the external annular shell 14 and the support elements 56 are secured to one of the first plate 22 and the second plate 24.

(20) With such an assembly, each means of attachment is pre-assembled at heat exchanger 16, which simplifies the mounting of heat exchanger 16 on the external annular shell 14. In addition, the elastic means 54 prevent the untimely movements of the first 22 and second 24 plates since the first plate 22, which is attached to the second plate 24, is blocked on the rail 20.