Guide vane for a turbomachine fan

Abstract

A guide vane in an outer section of a turbofan engine contains oil cooling cavities which are located on one side of a main bending axis of the vane so that the differential thermal expansions compensate for the bending deformations caused by the aerodynamic forces exerted on the outer vane surface.

Claims

1. A guide vane for a turbomachine fan, comprising two opposite ends intended to be mounted on an internal casing and an external casing, concentric with the internal casing, of the turbomachine, the vane being hollow and traversed by a main heat transfer fluid circulation conduit extending, from a fluid inlet at a first of the vane ends, into at least a height portion of the vane, the vane being composed of sections, each at a uniform position in a radial direction of the turbomachine, the sections being each composed of a central region and at least one end region on either side of a principal axis of flexural inertia of the section, the end region including a leading edge and a trailing edge of the vane, wherein, in each vane section of the height portion of the vane, the main conduit extends merely in the central region, said principal axis of flexural inertia being an axis about which the section has a quadratic moment of inertia and the vane has the lowest flexural rigidity.

2. The guide vane according to claim 1, wherein the vane is also traversed, in the height portion of the vane, by lateral fluid circulation conduits between the main conduit and, respectively, the leading edge and the trailing edge of the vane, the lateral conduits extending between a fluid outlet and a first coupling, joining the ends of the lateral conduits to an end of the main conduit.

3. The guide vane according to claim 2, wherein the lateral conduits extend, in each section of the height portion of the vane, into said end region.

4. A guide section for a turbomachine fan, comprising a stage composed of vanes according to claim 1.

5. The guide section for a turbomachine fan, comprising a stage composed of vanes according to claim 2.

6. The guide section according to claim 5, comprising an oil circulation direction inversion arrangement either in the main conduit, or in the lateral conduits.

7. A turbomachine, comprising a secondary stream and at least one guide vane according to claim 1.

8. A turbomachine, comprising a fan and the guide section according to claim 5, immediately downstream from the fan.

Description

(1) The various aspects, features and advantages of the invention will now be described in more detail by means of the following figures, which represent some preferred, but merely illustrative, embodiments thereof:

(2) FIG. 1, already described, represents a dual-flow turbomachine;

(3) FIG. 2, also described, conveys the technical problem solved by the invention;

(4) FIG. 3 represents a transverse cross-section of a vane according to the invention;

(5) FIG. 4 represents a perspective view of the vane; and

(6) FIGS. 5 and 6 each represent a schematic illustration of an alternative embodiment.

(7) Reference is made directly to FIGS. 3 and 4. The vane 15 equipped with the invention includes an internal end 20 fastened to the internal casing 3, and an external end 21 fastened to the external casing 4. An oil lubrication circuit 22 is present in the machine, for example under the internal casing 3. It comprises a supply conduit 23 whereby the oil enters the vane 15 located downstream from a lubricated device where the oil has been exposed to friction and contact with hot solids (bearings for example); the oil is then hot, and suitable for transferring greater heat to the vane 15, and producing a greater local thermal expansion therein. The circuit further comprises an outlet circuit 24 whereby the oil comes out of the vane 15; the oil, which has then been cooled by passing in the vane 15, is less suitable for transferring heat, and produces smaller local thermal expansions. The supply conduit 23 is extended into the vane 15 via a cavity referred to as central conduit 25, wherein the oil rises in the radial direction R or height of the vane 15 before reaching a so-called upper coupling 26 (according to the orientation of FIG. 3, where “upper” is equivalent to “closer to the external casing 4”) where the oil flow is dispersed before falling into lateral conduits 27 and 28, parallel with the central conduit 25 and the cooled oil travels in the opposite direction, towards the internal end 20, before joining the outlet conduit 24 which returns the oil to the lubricated device. The conduits 25, 27 and 28 extend over a height portion 29 of the vane 15 which may encompass the entire height or almost of the vane 15, and it is in any case advantageous that they extend via a main portion, encompassing the mid-height line 30 (at radial mid-distance from the casings 3 and 4) and optionally comprising about half the height of the vane 15 between said casings 3 and 4. The upper coupling 26 may be close to the external end 21, but this condition is not essential. In further possible embodiments of the invention, the lubrication circuit 22 could extend into the external casing 4, and the general arrangement of the conduits 25, 27 and 28 would then be inverted. In further possible embodiments, the lateral conduits 27 and 28 could be omitted, as well as the upper coupling 26, and the supply conduit 23 and the outlet conduit 24 would then both branch at opposite ends of the central conduit 25 extending into the internal casing 3 for one, into the external casing 4 for the other.

(8) It is recommended, at least for the height portion 29 of the vane 15, that the central conduit 25 extend into the central region 40 and therefore between the central portion of the extrados face 16 and the principal axis of inertia Iz, so that the greatest thermal expansions produced by the heat transferred by the oil benefit the regions of the vane 15 subject to the greatest compression produced by the aerodynamic loads. The lateral conduits 27 and 28, being traversed by the oil already cooled, apply less substantial thermal expansions: it is therefore stated that these expansions are located at locations of the vane 15 which, being on average closer to the main axis Iz, or on the opposite side of this axis, are subject to less compression produced by aerodynamic bending or are subjected on the contrary to an extension. For this reason, it is advantageous that the lateral conduits 27 and 28 extend into the end regions 41 and 42. The principal axis of inertia Iz for which the quadratic moment of inertia of the section is minimal, and the strength of the vane 15 in respect of bending and at this section is also minimal, therefore perfectly separates the central conduit 25 from the lateral heat transfer fluid return conduits 27 and 28. Advantageously, the central conduit 25 occupies the greatest portion of the surface area of the central region 40; and the lateral conduits 27 and 28 may occupy the greatest portion of the surface areas of the respective end regions 41 and 42.

(9) Relatively thin partitions of uniform thickness delimit the vane 15 and separate the conduits 25, 27 and 28. One of these partitions 43 separates the central conduit 25 from the lateral conduit 27 located around the leading edge 17, the other of these partitions 44 separates the central conduit 25 from the other lateral conduit 28, located around the trailing edge 18. The partitions 42 and 43 extend, in this embodiment, somewhat extending from one another and at the location of the principal axis Iz. This, the central conduit 25 extends exclusively in the side of the vane 15 subject to compression. In this embodiment, the lateral conduits 27 and 28 extend on the other side of the axis Iz. They could thus occupy a portion of the central region 40.

(10) The various conduits 25, 27 and 28 could all be divided into several parallel conduits. In the embodiment shown, they are all rectilinear, which is not essential. The wall thicknesses of the vane 15 are identical on the extrados 16 side and the intrados 19 side for the various conduits 25, 26 and 27, which is likewise not essential, and the central conduit 25 could for example be closer to the extrados 16.

(11) It is seen that the technical effect of the invention is produced above all by the central conduit 25, the lateral conduits 27 and 28 not being essential (or suitable for being left empty of oil). A slightly more complex arrangement, represented in FIGS. 5 and 6, may then be proposed, to produce a different operating mode as desired, wherein the differential thermal expansion is not used. With reference to FIGS. 5 and 6, the preceding oil circuit is supplemented by a by-pass 31, connecting to the upper coupling 26 one of the supply 23 and outlet conduits 24 by a first valve 32; a lower coupling 33 between the conduits 25, 27 and 28, at the opposite end to the upper coupling 26 is added; and a second valve 34, fitted on the same supply 23 or outlet conduit 24 as the first valve 32, is disposed at the junction of the conduit extending into the vane 15 (herein the central conduit 25) of the lower coupling 33. Herein also, “upper” and “lower” refer to the orientation of FIGS. 3, 5 and 6, and are equivalent to “closer to the external casing 4” and “closer to the internal casing 3”, respectively.

(12) As shown in FIG. 5, the first valve 32 closes the by-pass 31 and the second valve 34 closes the communication between the central conduit 25 and the lower coupling 33: the operation is the same as above, with reverse oil circulations between the central conduit 25 and the lateral conduits 27 and 28, the valves 32 and 34 enabling circulation from the supply conduit 23 to the central conduit 25. However, as shown in FIG. 6 where the two valves 32 and 34 are switched, the hot oil is sent into the by-pass 31, then into the upper coupling 26, before flowing in the same direction, towards the bottom of the figure, in the three conduits 25, 27 and 28. The second valve 34 then enables communication between the central conduit 25 and the lower coupling 33, which enables the oil having traversed the central conduit 25 to reach the outlet conduit 24 directly.

(13) The invention has been described in relation to an oil lubrication circuit. It could be implemented with other heat transfer fluids, without changing the shape of the vane 15, which would offer the same heat exchange relationship.