Flow mixer with a changing thickness

Abstract

The invention relates to a concentric gas flow mixer in a multiple-flow turbomachine, comprising a nominally cylindrical upstream part and a downstream part having outer and inner lobes distributed peripherally around the tower of said mixer, characterised in that it comprises at least one modified lobe having a wall thickness, in at least one area, which is different from the other lobes, so as to modify the vibratory response of said mixer.

Claims

1. A mixer for concentric gas flows in a multi-flow turbomachine, including a nominally cylindrical upstream portion and a downstream portion having outer lobes and inner lobes distributed circumferentially over the perimeter of said mixer, characterized in that it includes at least one modified lobe disposed in an aperiodic angular pattern and having, at least at one area, a wall thickness of a material of the at least one area different from other of the outer lobes or the inner lobes, so as to modify the vibratory response of said mixer.

2. The mixer as defined in claim 1, characterized in that the at least one of the modified lobe has the wall thickness that varies between 110% and 300% of a wall thickness of the other of the outer lobes or the inner lobes.

3. The mixer as defined in claim 1, characterized in that the at least one of the modified lobe has the wall thickness of 1.5 mm.

4. The mixer as defined in claim 1, characterized in that the at least one of the modified lobe has the wall thickness that varies between 50% and 90% of the a wall thickness of the other of the outer lobes or the inner lobes.

5. The mixer as defined in claim 1, characterized in that the at least one modified lobe includes at least two modified lobes.

6. The mixer as defined in claim 1, characterized in that an addition or removal of material extends over an entire area including a first inner half lobe, the outer lobe and a second inner half-lobe.

7. The mixer as defined in claim 1, characterized in that two of the at least one modified lobe disposed in an aperiodic angular pattern have a different wall thickness.

8. A turbomachine including the mixer as defined in claim 1.

Description

PRESENTATION OF THE FIGURES

(1) Other characteristics and advantages of the invention will appear from the following description, which is purely illustrative and non-limiting, and should be read with reference to the appended figures in which:

(2) FIG. 1a is a graphical representation of a Campbell diagram highlighting the matching of a pure diameter natural mode of the type 0Φ of the mixer with the vibrations caused by the turbojet engine during stabilized operating speeds, FIG. 1b being a histogram representation of the distribution of the deformations encountered in one of the natural modes highlighted in the Campbell diagram in FIG. 1a;

(3) FIG. 2a is a graphical representation of a Campbell diagram highlighting the matching of a pure diameter natural mode of type 1Φ of the mixer with the vibrations caused by the turbojet engine during stabilized operating speeds, FIG. 2b being a histogram representation of the distribution of the deformations encountered in one of the natural modes highlighted in the Campbell diagram in FIG. 2a;

(4) FIG. 3 represents a schematized sectional view of a turbojet engine seen in profile and the elements constituting it;

(5) FIGS. 4a, 4b and 4c are 3D modeling of the flow mixer from different viewing angles;

(6) FIGS. 5a and 5b represent the localization and the type of the deformations on a modeling of the mixer for said 0Φ pure diameter mode;

(7) FIGS. 6a and 6b represent the amplitude and the location of the deformations of a complex vibration mode on a mixer;

(8) FIGS. 7a and 7b represent a 3D modeling of the mixer highlighting the modifications received in order to modify its vibratory response.

DESCRIPTION OF ONE OR SEVERAL MODES OF IMPLEMENTATION AND EMBODIMENTS

(9) Overviews

(10) With reference to FIG. 3, a dual-flow turbojet engine T, whose general operation considered as known will not be explained, has conventionally from upstream to downstream, a fan propelling an air flow which will be divided into a primary flow Fp and a secondary flow Fs.

(11) The primary flow flows in a low-pressure compressor, a high-pressure compressor, a combustion chamber, a high-pressure turbine Thp and joins the secondary flow Fs downstream of a mixer 1.

(12) The secondary flow F flows, for its part, concentrically with the primary flow Fp around the inner casing Ci and inside the outer casing Ce.

(13) The function of the mixer 1 is to optimize the mixing of the primary Fp and secondary Fs flows at the outlet of the turbojet engine T.

(14) The mixing of the primary Fp and secondary Fs flows downstream of the turbojet engine T bringing many advantages both in terms of performances and environmental disturbances, new solutions are continuously explored to optimize the homogeneity of the mixture.

(15) Flow Mixer

(16) With reference to FIGS. 4a, 4b and 4c, a daisy wheel-type lobed mixer 1 has a nominally cylindrical upstream portion 2 and a corrugated downstream portion 3.

(17) The indications concerning the radial, axial and tangential directions correspond to the axis of the mixer, which is also that of the turbojet engine. The upstream and downstream concepts follow the flow direction of gases in the turbojet engine.

(18) The corrugations of the downstream portion form together a plurality of radially outer 4 and inner 5 lobes distributed circumferentially about the longitudinal axis of the mixer 1.

(19) The mixer has the particularity that at least one of its lobes has in at least one area an addition or a withdrawal of material configured to modify the vibratory response of said mixer.

(20) This addition or withdrawal is chosen to shift the frequencies of its natural modes in order to avoid a matching with the vibration frequencies generated by a stabilized operating speed of the turbojet engine.

(21) In particular, in order to reduce the vibratory response, as illustrated later, the modifications made to the mixer 1 are intended to promote the appearance of complex modes composed of a sum of pure modes.

(22) Embodiments of the Mixer

(23) With reference to FIG. 5a, a retained solution includes two lobes having a modified thickness 14. Indeed, in order to minimize the mass increase, the best compromise between mass increase and vibratory response modification is sought.

(24) A modified lobe 14 is therefore an outer lobe 44 which has a thicker surface portion, this portion extending between the vertices of the two inner lobes 5 that border it as observable in FIG. 5b.

(25) The two lobes 14 mentioned above have a wall thickness different from the other lobes 13. In a retained solution, the mixer 1 includes 16 regular lobes 13 with a wall thickness of 1 mm and 2 particular lobes 14 with a wall thickness of 1.5 mm.

(26) The thickening rate of the retained wall also takes into account manufacturing constraints, in order to ensure that, on a finished product, a thick lobe 14 having a minimum thickness in its tolerance area is substantially different from a regular lobe 13 having a maximum thickness in its tolerance area to ensure a substantially constant gain in performances for all mixers 1.

(27) The thickness of a modified lobe 14 can be 110% to 300% of the thickness of a regular lobe.

(28) For example, a modified lobe 14 may have a thickness representing 150% of the thickness of a regular lobe 13.

(29) A marked difference allows an obvious visual differentiation during manufacture, the mixer 1 being manufactured by assembling half-lobes juxtaposed and welded together.

(30) During assembly, two different types of parts make it possible to produce the mixer 1: a first type being a regular lobe 13 including an outer lobe framed by two inner half-lobes, this type of part composing mostly the mixer; a second type being a modified lobe 14 having the same general geometry as a regular lobe except for the thickness of its wall, and in the case of the solution represented in FIG. 5a, two modified complete lobes are included in the mixer 1.

(31) The parts are juxtaposed and welded to form the lobes of the mixer.

(32) The contact profile between a modified lobe 14 and a conventional lobe 13 is not smoothed, and therefore includes a “step” at the contact, related to the difference in thickness between a modified lobe and a regular lobe.

(33) Another method for manufacturing a mixer is described in document FR2912469.

(34) In other embodiments of the invention, it is also envisaged to reduce the thickness of a lobe to generate the same effects, a modified lobe 14 having in this embodiment a thickness that can represent 25% to 90% of the thickness of a regular lobe.

(35) A modified lobe 14 may for example have a thickness representing 50% of the thickness of a regular lobe 13.

(36) An occasional modification of the thickness of one or several lobe(s) is also a possibility, such as an addition of material or a local extra-thickness, as well as a removal of material such as a bore or a groove made on one or several lobe(s).

(37) The relative position of the modified lobes 14 also affects the vibratory response of the mixer 1. Indeed, the angular periodicity (periodicity along a rotation about the axis of the mixer) of the pattern formed by the position of the modified lobes 14 promotes the appearance of natural modes. One of the solutions envisaged is therefore, in the case of a thickening of several lobes, to arrange them so as to avoid creating a pattern forming an angular repetition.

(38) With reference to FIG. 5b, the thickened area of a modified lobe 14 thus relates to an outer lobe 4.

(39) The adopted configuration therefore makes it possible to promote the appearance of complex vibratory modes, less damaging to the mixer 1, in addition to drastically reducing the number of modes with diameters considered to be pure.

(40) Desired Vibratory Mode

(41) With reference to FIG. 6b, it is possible to observe the mapping of the deformations in a pure deformation mode, here a mode 0Φ. The deflected shape is generally uniform for a given radius, the largest deformation being achieved at the smallest diameter of the part, at the crest of the inner lobes 5.

(42) With reference to FIG. 7b, it can be noticed that the represented critical mode consists of a sum of modes with radial deformation at diameters Φ3, Φ12, Φ14, Φ15, Φ16, Φ17, Φ18, Φ19, Φ20 and Φ21, modes with tangential deformation at diameters Φ0, Φ3 and Φ6, and modes with axial deformation at diameters Φ18 and Φ21. The distribution of the deformations is less uniform, in addition to having smaller amplitude.