Mixer for an engine manufactured from at least one composite material, manufacturing method and manufacturing device

Abstract

It is provided a mixer for an engine, that for the mixing of fluid flows from a primary flow channel and a secondary flow channel of the engine, respectively has multiple first and second guide elements that alternate along a circumferential direction and extend along a central axis, wherein the first guide elements are formed in a diffusor-like manner with at least one radially outwardly extending section, and the second guide elements are formed in a nozzle-like manner with at least one radially inwardly extending section, and the mixer is made of a composite material with at least two separate material layers. The at least two material layers are arranged with their edges along the central axis in an overlapping manner and/or edge to edge, and namely in an area of the mixer in which the first and second guide elements are provided.

Claims

1. A method for manufacturing a mixer for an engine for mixing fluid flows from a primary flow channel and a secondary flow channel, comprising: forming the mixer from a composite material including at least two material layers that respectively contain fibers, wherein each of the at least two material layers include edges, and wherein the mixer includes: a plurality of first guide elements, each including at least one radially outwardly extending section with respect to a central axis of the mixer; a plurality at second guide elements respectively positioned adjacent to the first guide elements, wherein each second guide element includes at least one radially inwardly extending section, and wherein the first guide elements and the second guide elements alternate along a circumferential direction of the mixer and extend axially with respect to the central axis of the mixer; a common side wall shared by adjacent ones at the first guide elements and the second guide elements, wherein the common side wall extends between a radially outermost section of the first guide element and a radially innermost section of the second guide element; wherein the edges of the at least two material layers are arranged along the central axis of the mixer in at least one of an overlapping manner for at least a local stiffening of a structure of the mixer and edge to edge for at least a local reduction in stiffness of the structure of the mixer; and wherein the edges of the at least two material layers are arranged along the central axis of the mixer at the common side wall in an overlapping manner to form a local thickening of a portion of the common side wall extending axially, wherein the local thickening locally stiffens the structure of the mixer, and wherein the edges of the at least two material layers extend in the axial direction, the circumferential direction, and the radial direction, and wherein the edges of the at least two material layers extend in a curved manner with respect to at least two spatial axes that are perpendicular to each other.

2. The method according to claim 1, further comprising forming the mixer with a manufacturing tool that predefines a contour of the mixer, wherein the at least two material layers are flexible, wherein the at least two material layers are arranged at the manufacturing tool, and wherein the at least two material layers are submitted to a curing process at the manufacturing tool.

3. The method according to claim 2, wherein the curing procedure includes one chosen from an infusion method, an autoclaving process, and an injection method.

4. The method according to claim 2, wherein the manufacturing tool extends along a longitudinal axis that coincides with the central axis of the mixer, wherein the manufacturing tool includes radially outwardly protruding radial arms to define the first guide element and the second guide element, wherein the manufacturing tool includes an outer contour, and wherein the at least two material layers are arranged at the outer contour.

5. The method according to claim 2, wherein the manufacturing tool extends along a longitudinal axis that coincides with the central axis of the mixer, wherein the manufacturing tool includes radially inwardly extending radial arms and an inner contour, wherein the manufacturing tool surrounds a hollow space in the shape of a circular ring, into which the radially inwardly extending radial arms protrude to define the first guide element and the second guide element, and wherein the at least two material layers are arranged at the inner contour.

6. The method according to claim 1, wherein the at least two material layers are formed by one chosen from pre-impregnated batts and batts that are impregnated after having been arranged at a manufacturing tool that predefines a contour of the mixer.

7. The method according to claim 1, wherein the at least two material layers are cut out from a material surface, wherein the at least two material layers are provided for forming a segment of the mixer, the at least two material layers include geometries that are determined in an automated manner, with at least one design parameter being prescribed, and the at least two material layers are cut out from the material surface wherein a specification of an arrangement of sectional lines for the at least two material layers at the material surface is performed in an automated manner.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The accompanying Figures illustrate possible embodiment variants of the solution according to the invention by way of example.

(2) FIG. 1 shows a perspective view of an embodiment variant of a mixer according to the invention with a blossom-shaped or meander-shaped contour.

(3) FIG. 2 shows, by sections, a cross-section of the mixer of FIG. 1, also rendering individual material layers that are arranged edge to edge.

(4) FIGS. 2A-2B show enlarged sections of the sectional view of FIG. 2.

(5) FIG. 3 shows, in a perspective view, a segment of the mixer of FIG. 1 that is comprised of multiple individual material layers, with material layers that are arranged axially edge to edge.

(6) FIG. 4 shows a variant of the segment of FIG. 3 with an alternative edge-side arrangement of individual material layers.

(7) FIG. 5 shows, in a view corresponding to FIG. 2, a sectional view with an alternative structure of the material layers.

(8) FIG. 5A shows a schematic sectional view of the material layers of FIG. 5 in an unfolded state and in an alternative layering.

(9) FIG. 6 shows, in perspective view, a segment of the mixer with two material layers that are overlapping axially along a lobe of the mixer and at the edge side.

(10) FIG. 7 shows, in a perspective rendering, a segment of the mixer with four material layers that respectively axially overlap in pairs along a gully of the mixer and at the edge side.

(11) FIG. 8 shows, by sections, a cross-sectional rendering of a mixer with three material layers corresponding to a further embodiment variant.

(12) FIG. 9 shows, by sections, a sectional view of a manufacturing tool for manufacturing a mixer corresponding to FIG. 8.

(13) FIG. 10 shows a section of the mixer of FIG. 1 with different mixer segments from material layers overlapping each other at the edge side along a spline.

(14) FIGS. 10A-10B show differently constructed mixer segments for the section of FIG. 10.

(15) FIG. 11 shows, by sections and in a schematic manner, a sectional view of the section of FIG. 10.

(16) FIG. 12 shows, by sections and in a perspective view, a segment of the mixer with an illustration of areas of different stiffness.

(17) FIGS. 13A to 13E show, in different views, an embodiment variant of a manufacturing tool according to the invention as a positive mold for a mixer of FIG. 1 that is to be manufactured.

(18) FIGS. 14 to 19 show an illustration of a variant of a method according to the invention for manufacturing a mixer corresponding to FIG. 1, in which multiple material layers for a single segment of the mixer are cut out in a computer-aided and automated manner from a material surface of a fiber roll for the subsequent arrangement at a manufacturing tool.

(19) FIGS. 20 to 23 show a schematic rendering of possible methods for carrying out a curing in the manufacturing of the mixer.

(20) FIGS. 24 to 24A show a schematic illustration of a variant of a manufacturing method according to the invention using a positive mold corresponding to FIGS. 13A to 13E.

(21) FIGS. 25 to 25A show a SCHEMATIC illustration of a variant of a manufacturing method according to the invention using a manufacturing tool as a negative mold for the mixer.

(22) FIGS. 26 to 26A show a schematic illustration of a further embodiment variant of a manufacturing method according to the invention, in which an injection method is used as part of the curing.

(23) FIG. 27 shows a cross-sectional view of a turbofan engine according to the invention with a mixer in the area of an exhaust of the turbofan engine.

(24) FIG. 28 shows a section of a manufacturing tool with a channel system integrated therein.

DETAILED DESCRIPTION

(25) FIG. 27 illustrates, in a schematic manner and in sectional view, a (turbofan) engine T in which the individual engine components are arranged in succession along a rotational axis or central axis M. At an inlet or intake E of the engine T, air is sucked in along an entry direction R by means of a fan F. This fan F, which is arranged in a fan housing FC, is driven via a rotor shaft RS that is set into rotation by a turbine TT of the engine T. Here, the turbine TT connects to a compressor V, which for example has a low-pressure compressor 11, and a high-pressure compressor 12, as well as possibly also a medium-pressure compressor. The fan F supplies air to the compressor V, on the one hand, as well as, on the other hand, to the secondary flow channel or bypass channel B in order to create the thrust. Here, the bypass channel B extends about a core engine that comprises the compressor V and the turbine TT as well as a primary flow channel for the air that is supplied to the core engine by the fan F.

(26) The air that is conveyed via the compressor V into the primary flow channel reaches a combustion chamber section BK of the core engine, where the driving power for driving the turbine TT is generated. For this purpose, the turbine TT has a high-pressure turbine 13, a medium-pressure turbine 14, and a low-pressure turbine 15. Here, the turbine TT drives the rotor shaft RS and thus the fan F by means of the energy released during combustion in order to create the required thrust by means of the air that is conveyed into the bypass channel B. The air from the bypass channel B as well as the exhausts from the primary flow channel of the core engine flow out via an exhaust A at the end of the engine T. Here, the exhaust A usually has a thrust nozzle with a centrally arranged outlet cone C.

(27) In particular for the purpose of noise reduction, a mixer 20 is provided in the area of the exhaust A as part of a mixer assembly group 2. A first fluid flow f1 from the primary flow channel that is discharged form the core engine behind the low-pressure turbine 15 and a second fluid flow f2 from the bypass channel B are intermixed by this mixer assembly group 2 and its mixer 20. For this purpose, parts of the first (primary) fluid flow f1 from the core engine are alternatingly guided outwards and the second (secondary) fluid flow f2 from the bypass channel B is guided inwards via a blossom-shaped or meander-shaped contour of the mixer 20. In this manner, segments of hot and cold flow zones are created, and an intermixing of the two fluid flows f1 and f2 is achieved. Due to turbulences occurring during intermixing, low-frequency noise is reduced and high-frequency noise is amplified, so that the audible nose range is reduced as a result.

(28) In the present case, the mixer 20 is preferably manufactured from a fiber reinforced composite, in particular a ceramic matrix composite, and thus for example as a CMC mixer. In the embodiment variants that will be explained in more detail in the following, the mixer has guide elements 210, 220 that define the meander-shaped contour of the mixer 20 and are formed in the manner of alternating lobes and gullies about a mixer opening O. Via these guide elements 210, 220, the first and second fluid flows f1 and f2 from the primary flow channel of the core engine and the bypass channel B are alternatingly guided outwards and inwards to obtain the desired intermixing of the fluid flows f1 and f2.

(29) FIG. 1 shows the mixer 20 in perspective detail view. It extends in a longitudinal axis that coincides with the central axis M in a longitudinal direction L, which in the mounted state of the mixer 20 points in the direction of the exhaust A, and thus in the flow direction of the fluid flow f1 and f2. The different guide elements 210 and 220 of the mixer 20 extend in longitudinal direction L, starting from a front mixer edge 200 via which the fixation of the mixer 20 at the interface 21 is realized. The guide elements 210 and 220 are arranged alternatingly along a circumferential direction U and are alternatingly arched in a convex (in the case of the first guide elements 210) and a concave manner (in the case of the second guide elements 220).

(30) Here, the first guide elements 210 are embodied so as to be respectively pointing radially outwards and thus in a diffusor-like manner, while the second guide elements 220 are formed so as to be pointing radially inwards and thus in a nozzle-like manner. Correspondingly, the fluid flow f1 from the core engine is guided radially outwards via the first guide elements 210, while the fluid flow f2 from the bypass channel B is guided radially inwards via the second guide elements 210, if the mixer 20 is mounted at the engine T according to the intended use.

(31) Each first guide element 210 shares respectively one side wall 231, 232, 233 or 234 with an adjacent second guide element 220. Thus, a side wall 231-234 extends between a radially outermost section of a first guide element 210, i.e. up to a convex outer curvature 2100 of the first guide element 210, and a radially innermost section of a second guide element 220, i.e. up to a concave inner curvature 2200 of the second guide element. Due to the radially converging second guide elements 220 and axially diverging first guide elements 210, the radial extension of each side wall 231-234 (with respect to the longitudinal direction L of the mixer 20) is increased, starting from the mixer edge 200 in the direction of the exhaust-side end of the mixer 20.

(32) In the present case, the mixer 20 that is manufactured from a fiber-reinforced composite is formed from multiple batts with ceramic filaments and a matrix that possibly also contains ceramics as the CMC structural component. The mixer 20 has a multi-layered structure, and in a first embodiment variant is e.g. comprised of different material layers a1 to a5, b1 to b4, c1 to c4, and d1 to d5. This is illustrated in particular for the first embodiment variant based on FIGS. 2, 2A and 2B.

(33) At their edges that are positioned in the circumferential direction U, multiple single material layers a1 to a5; d1 to d 5 and b1 to b4; c1 to c4 that are formed of batts are arranged in pairs edge to edge in the axial direction. As for the material layers a1 to a5 and d1 to d5 as well as b1 to b4 and c1 to c4, that are arranged edge to edge and are thus butted together, a gap l1 to l9 that is possibly only a few m wide is present between each pair of material layers which are arranged edge to edge. Thus, a reduced stiffness is provided in a targeted manner in a joint area S1-S5 of the respective gaps l1 to l9, which is associated with a greater elastic deformability of the mixer structure. Hence, a targeted stiffness reduction is obtained through the arrangement of the material layers a1 to d5 via the joint areas S1 to S5 at the convex outer curvatures 2100 and the concave inner curvatures 2200, without the wall thickness of the mixer 20 having to be reduced in a large planar area.

(34) In the present case, the corresponding joint areas S1 to S5 are respectively provided in the area of the convex outer curvature 2100 and the concave inner curvatures 2200 of the first and second guide elements 210 and 220. Here, respectively multiple material layers are arranged in pairs edge to edge, wherein at the same time respectively multiple additional material layers extend beyond a corresponding gap l1 to l9 of two adjoining material layers, thus covering them. Thus, in the radial direction, for example material layers a1, b1, a2, b2, a3, b3, a4, b4, a5 alternate in pairs, of which respectively only every other material layer b1 to b4 is arranged, in the area of a convex outer curvature 2100 of a first guide element 210, edge to edge to a material layer c1 to c4 connecting to the same in the circumferential direction U. In contrast, the material layers a1 to a5 that adjoin thereto in the radial direction extend up to the next concave inner curvature 2200 of a second guide element 2200, only here adjoining an edge of a further material layer d1-d5. Thus, the material layers a1 to d5, although respectively extending with the same length in the circumferential direction U in the present case, are offset by layers with respect to one another in the circumferential direction U, so that material layers a1 to d5 adjoining each other in the radial direction end at different first and second guide elements 210, 220.

(35) For example, the first material layers a1 to a5 between the joint areas S3 and S5 respectively completely span a first and second side wall 233, 231 as well as a convex outer curvature 2100 of a first guide element 210, and thus extend between two concave inner curvatures 2200 of two adjoining second guide elements 220. In contrast, the material layers b1 to b4 or c1 to c4, which are layered together with them, end in the joint area S4 of the convex outer curvature 2100 of the first guide element 210, and are butted together here. In contrast, in the circumferential direction U, these material layers b1 to b4 and c1 to c4 respectively span, starting from the joint area S4 at the convex outer curvature, the second guide element 220 that adjoins in the clockwise direction or the other second guide element 220 that adjoins in the counterclockwise direction as well as the respectively associated concave inner curvature 2200 at the joint area S3 or S5.

(36) Based on FIGS. 3 and 4, the material layers 20a to 20g, which are respectively formed by a batt, are illustrated. While in the variant of FIG. 3 individual batts 20a to 20c respectively define one single second guide element 220 and are arranged edge to edge to each other in the area of a convex outer curvature 2100 of adjoining first guide elements 210, the batts 20d to 20g of FIG. 4 form the individual guide elements 210 completely and are arranged edge to edge to each other in the area of the concave inner curvatures of second guide elements 220 adjoining thereto. Thus, if in the variant of FIG. 3 the joint areas S2 and S4 are provided in the flow direction and thus along the longitudinal direction L at the first guide elements that are arched in a convex manner and extended radially outwards, the joint areas S1, S3 and S5 are located at the concave inner curvatures 2200 of the second guide elements 220 and thus run radially inwards along the longitudinal direction L in the variant of FIG. 4. In both cases, a piece-by-piece construction of the mixer 20 can be carried out, in which areas of deliberately reduced stiffness are provided in a targeted way and in a manner evenly distributed across the circumference by means of a corresponding segmentation and thus formation of individual guide elements 210 and 220 that extend radially outwards or radially inwards.

(37) In contrast, in the variant of FIGS. 5, 5A, 6 and 7, a targeted stiffening and thickening of the mixer structure is provided in the area of the convex outer curvatures 2100 and the concave inner curvatures 2200 by material layers that are overlapping at the edge side.

(38) Here, material layer bondings L1-L8 are arranged so as to overlap in the axial direction at the edge side. However, in the present case respectively only one part of the material layers that are present here ends in the area of the respective arch 2100, 2200, so that also only that part overlaps at the edge side in the area of an arch 2100 or 2200. For example, the continuous wall of the mixer 20 is constructed from a total of m plus n material layers. Here, respectively m material layers are assigned to a first material layer bonding L1, L3, L5 or L7 z, while n material layers are assigned to a further material bonding L2, L4, L6 or L8. Then, the individual material layers of these material layer bondings L1 to L8 are present in a manner stacked on top of each other in the radial direction at each side wall 231-234. Respectively only two material layer bondings L1/L3, L2/L4, L3/L5, L4/L6, L5/L7 or L6/L8 end at an arch 2100 or 2200, with their material layers overlapping at the edge side, while a third material layer bonding L2, L3, L4, L5 or L6 with multiple material layers extends beyond the respective arch 2100 or 2200.

(39) Correspondingly, overlapping areas OL13, OL24, OL35, OL46, OL57 and OL68 are respectively present in the area of the arches 2100 and 2200. In these overlapping areas OL13, OL24, OL35, OL46, OL57 and OL68, the structure of the mixer 20 is locally stiffened and thickened due to these material layers of a pair of material layer bondings L1/L3, L2/L4, L3/L5, L4/L6, L5/L7 or L6/L8 that overlap at the edge side, while at the same time material layers of a third material layer bonding L2, L3, L4, L5 or L6 are not interrupted in these overlapping areas OL13, OL24, OL35, OL46, OL57 and OL68. As a result, a local thickening of the mixer structures by 50% as compared to a respectively continuous arrangement of the material layers is tolerated in the area of the arches 2100 and 2200 across the entire length of the mixer 20 (along the longitudinal direction L) in the area of the first and second guide elements 210 and 220 in order to render manufacturing the mixer 20 by means of the segmented arrangement of the material layers easier, and also to introduce stiffening structures in a targeted manner.

(40) As is shown based on the folded out rendering of FIG. 5A for a variant based hereon with a differing configuration or layering of the material layers, thickened areas are present in the respective overlapping areas OL46, OL57 and OL68 due to the material layers of two adjoining material layer bondings overlapping in pairs at the edge side. However, these thickened areas can for example be provided at an outer contour of the mixer 20 for the radially outwardly extending first guide elements 210, and at an inner contour of the mixer 20 in the radially inwardly extending second guide elements 220 in order to keep their influence on the fluid flows f1 and f2 as small as possible.

(41) Based on FIGS. 6 and 7, possible variants for constructing the mixer 20 from individual batts 20a to 20f that are arranged in segments are illustrated in an analogous manner to FIGS. 3 and 4. Here, the material layers overlap in the area of the convex curvatures 2100 of the first guide elements 210 and thus at the lobes of the mixer 20, or in the area of the concave inner curvatures 2200 of the second guide elements 220 and thus at the gullies of the mixer 20, respectively at the edge side.

(42) Depending on the size of the batts for forming the individual material layers a1, b1 and c1 that are stacked on top of each other, they can of course also extend across multiple radially outwardly extending first and radially inwardly extending second guide elements 210, 220 of the mixer 20. Correspondingly, a segment of the mixer 20 that is shown in FIG. 8 and that can for example be manufactured with a manufacturing tool 3 of FIG. 9 has three exemplary material layers a1, 131 and c1. Here, respectively one inner section a10, a11 or a12 of a radially outer material layer a1 at a concave inner curvature 2200 at the outer side, as well as respectively one inner section c10 or c11 of a radially inner material layer c1 at a convex outer curvature 2100 at the inner side form a local thickening of the wall of the mixer 20. However, such a thickening respectively has no (relevant) influence on the flow along the respective inner section a10 to a12 or c10, c11.

(43) For manufacturing the mixer 20 from individual material layers that do not extend across the entire circumference of the mixer 20, a positive mold may for example be provided as the manufacturing tool 3, which has a base body 30 with radially outwardly protruding radial arms 30a to 30d, in a manner corresponding to FIG. 9. These radial arms 30a to 30d, with the gaps lying in between them and having a funnel-shaped cross-section, define the blossom-shaped or meander-shaped contour of the mixer to be manufactured 20. The individual material layers or material layer bondings are correspondingly arranged at an outer contour of the corresponding manufacturing tool 3, for example they are draped thereat in a suitable manner, before subsequently a curing process is performed, for example by introducing the matrix material between the fibers by infiltration with a resin material and/or thermal treatment of the material layers.

(44) In order to be able to provide a local thickening and stiffening by means of material layers that are overlapping at the edge side in the area of the convex curvature 2100 and the concave inner curvature 2200 without substantially increasing the wall thickness of the mixer structure as compared to a material layer arrangement without a corresponding overlapping, the manufacturing tool 3 is provided with a compensation contour in the area of a radially outermost section of each radial arm 30a to 30d, as well as at a radially innermost section of the respective gap lying between them. This may for example be a flattened section or material recess in the area of the radially outermost sections of the radial arms 30a to 30d or a material thickening 32 in the area of the funnel-shaped gaps formed between the protruding radial arms 30a to 30d. In this way, the material layers draped onto the corresponding manufacturing tool 3 form a contour at the respective overlapping areas OL13 to OL68, that shows only a minor local thickening and barely influences the fluid flows f1 and f2 guided through these areas, or does not influence them at all.

(45) With a view to a possible stability-oriented arrangement of the overlapping areas of at least two material layers it can also be provided in one embodiment variant that the overlapping edge rims do not (throughout) extend in parallel to the longitudinal direction L or the central axis M. In the embodiment variant illustrated in FIGS. 10, 10A and 10B, the edge rims 201bb and 202bb of the overlapping material layers 20aa to 20cc extend in the three-dimensional space and in a curved manner with respect to at least two spatial axes that are perpendicular to one another. Here, a section of the mixer 20 with multiple first and second guide elements 210, 220 is formed by two mixer segments 21.1 and 21.2 that respectively comprise multiple (in the present case three) material layers 20aa to 20cc that overlap in pairs at the edge side.

(46) At that, the individual material layers 20aa to 20cc define respectively one edge segment 200.1 or 200.2 for the mixer edge 200 and (just like the segments of the previous embodiment variants) extend across the entire axial length of the mixer 20. In contrast to the above-described embodiment variants, the overlapping edge rims 201bb and 202bb do not extend in an axially linear manner, but respectively have a course that, in addition to an axial directional component, also has a directional component in the circumferential direction U as well as a directional component in the radial direction r with respect to the central axis M of the finished mixer 20. Thus, the individual edge rims 201bb and 202bb extend in the manner of a spline, so that a starting point of an edge rim 201bb or 202bb that is located upstream in the area of the respective edge segment 200.1 or 200.2 is offset with respect to at least one further point of the respective edge rim 201bb or 202bb that is located downstream in longitudinal direction L regarding all three spatial directions that are perpendicular to each other. For example, in an edge rim 201bb of a material layer 20bb that is shown in FIG. 10A, a left-side curvature, on the one hand, and a radially outwardly oriented curvature of the edge rim 201bb, on the other hand, is provided, with a view along the longitudinal direction L beginning at a starting point at the edge segment 200.1. In contrast, in an edge rim 202bb that is shown in FIG. 10B, a right-side curvature, on the one hand, and a radially outwardly oriented curvature, on the other hand, is provided.

(47) The individual mixer segments 21.1 and 21.2 that are respectively comprised of multiple material layers 20aa to 20cc are brought into abutment at a manufacturing tool 3 so as to overlap each other, so that respectively two material layers 20bb/20aa and 20cc/20bb of the two mixer segments 21.1 and 21.2 overlap in a large planar area at least at two first guide elements 210. In this manner, additional three-dimensionally extending overlapping areas are provided at the edge rims 201bb and 202bb along both sides of a first guide element 210 that is arched in a convex manner. In particular at the per se even side walls 231-234 that are located opposite each other along the circumferential direction U, local thickenings V1 to V4 are created approximately centrally, extending in the axial direction and locally stiffening the mixer structure without any disruptive influence on the fluid flow f1 and f2 that is guided via the mixer 20. This is in particular illustrated by way of example based on the sectional view of FIG. 11.

(48) A segment of the mixer 20 shown in FIG. 12 further illustrates the material areas Ba, Bb and Bc of different stiffness that are defined at the mixer 20 by the corresponding arrangement and in particular through the edge-side overlappings of single material layers. A mostly small curvature of the material and a low stiffness is provided in an area that is close to the mixer edge, and also across a larger part of the side walls 231-234 (material area Ba). In a further material area Bb, which comprises the convex outer curvatures 2100 and the concave inner curvatures 2200 of the two first and second guide elements 210 and 220, respectively one area with an increased stiffness is formed by means of the material layers of the ceramic matrix composite that are stacked on top of each other. In material areas Bc, which extend across the axial length of the mixer 20 and on both sides of a convex outer curvature 2100 at opposing side walls 231, 232 and 233, 234, a local stiffening is provided by material layers that overlap at the edge side.

(49) A manufacturing tool 3 that is illustrated in FIGS. 13A to 13E can in particular be used for manufacturing a mixer 20 that is constructed of segments in a manner corresponding to the previously explained embodiment variants. At that, the manufacturing tool 3 models the contour of the mixer 20 as a positive mold, so that material layers in the form of batts that are draped at the outer contour of the manufacturing tool 3 yield the desired blossom-shaped or meander-shaped contour of the mixer 20. The manufacturing tool 3 correspondingly extends along a longitudinal direction L and has radially protruding radial arms 30a*, that emulate the contour of the radially outwardly extending first guide elements 210. At that, the individual radial arms 30a* are respectively supported in a form-fit manner at a base body 30 that emulates the radially inwardly extending second guide elements 220 of the mixer 20 via the gaps defined between the individual radial arms 30a*.

(50) In the present case, the base body 30 of the manufacturing tool 3 tapers off along a longitudinal direction L, while the individual radial arms 30a* taper off counter to the same, so that the corresponding contour of the mixer 20 is emulated. In order to facilitate demolding of the mixer 20 that is curing at the manufacturing tool 3, the individual radial arms 30a* are respectively supported at the base body 30 in a longitudinally displaceable manner. Thus, for demolding the mixer 20, each radial arm 30a* can be separated from the base body 30 in the longitudinal direction L. For this purpose, the base body 30 forms multiple longitudinally extending fastening grooves 300. Respectively one longitudinally extending fastening web 301a* of a radial arms 30a* is inserted into each fastening groove 300 in the manner of a dovetail joint when the components of the ceramic matrix composite are arranged at the manufacturing tool 3 for manufacturing the CMC mixer 20.

(51) The base body 30 and/or the radial arms 30a* that can be inserted thereat can for example be manufactured from a material that has a thermal expansion coefficient of more than 17/10.sup.6 K. For example, a corresponding manufacturing material can comprise aluminum. After the manufacturing tool 3 has cooled off, the base body 30 and/or the respective radial arm 30a* shrinks as well, whereby demolding of the cured mixer 20 is considerably facilitated.

(52) What is further illustrated based on FIGS. 14 to 19 is an embodiment variant of a possible manufacturing method, in which the manufacturing tool 3 of FIGS. 13A to 13E is also made use of, where appropriate, and by means of which in particular a mixer 20 of the previously described embodiment variants can be manufactured.

(53) Within the scope of the shown embodiment variant, a mixer with a blossom-shaped or meander-shaped contour corresponding to FIG. 14 is virtually divided into a plurality of individual mixer segments 21.1, of which one is shown by way of example in FIG. 15, in a computer-aided and automated manner by means of a software. Subsequently, it is determined by means of an algorithm with how many material layers 20aa to 20dd the corresponding mixer segment 21.1 can be created, with at least one design parameter being specified, for example the position and the spatial course of the local stiffening due to material layers overlapping at the edge side is determined in an automated manner. This respectively also includes the specification as to which geometry the individual material layers 20aa to 20dd corresponding to FIGS. 16A to 16D should have for this purpose.

(54) In a subsequent simulation step, it is determined in a manner corresponding to FIGS. 17A to 17D and 18A to 18D how the individual material layers 20aa to 20dd have to be arranged on a for example rectangular material surface, so that they can be cut out from the material surface with as minimal offcuts as possible. Consequently, the corresponding algorithm for example determines in which order the individual material layers 20aa to 20dd have to be virtually arranged on the material surface, so that as little fiber material as possible remains unused in the cutting-out procedure. The usable material surface for example results from rolling out a tissue or fiber roll FR in a manner corresponding to FIG. 19. In this way, an arrangement of sectional lines CA on the material surface of the fiber roll FR is specified and electronically transmitted to a corresponding processing device, for example in a computer-aided and automated manner, with the processing device subsequently cutting out the individual material layers 20aa to 20dd from the material surface along these sectional lines. Subsequently, the thus created material layers 20aa to 20dd are draped according to the calculations at a manufacturing tool, such as for example the manufacturing tool 3 of FIGS. 13A to 13E to form the individual mixer segment 21.1 of FIG. 15.

(55) The material layers 20aa-20dd can be so-called dry batts or impregnated batts with ceramic filaments. Depending on the fiber material that is used as the basis, different further process steps for curing and thus for finishing the mixer 20 can be provided. Possible variants are illustrated by way of example based on FIGS. 20 to 23.

(56) For example, the individual material layers can be positioned as a layer bonding LA in a manufacturing tool 3 that is used as a positive or negative mold in a manner corresponding to FIG. 20. The corresponding material layer bonding La is then already imbued by layers with a corresponding matrix material, e.g. resin. For the purpose of curing, any present air locks are pressed out of the material layer bonding (laminate) La that is arranged at the manufacturing tool 3, and a heat treatment is performed.

(57) If a pre-impregnated batt and an impregnated layer bonding LRE that is formed with the same is used, an autoclaving process can be realized as part of the curing procedure. Here, the curing is performed by using an autoclave 4 that is shown schematically in FIG. 21.

(58) FIG. 22 illustrates, in a schematic manner, a curing process by using an infusion method, for example a so-called VAR or VARI method, in which a matrix material, for example a resin, is supplied from a matrix reservoir RR to a layer bonding LRE that is arranged under vacuum in the manufacturing tool 3.

(59) In contrast to that, in the injection method that is shown based on FIG. 23, e.g. an RTM method, matrix material is supplied to a layer bonding LRE arranged between two tool parts via an inlet 51 of an injection tool 5, wherein excess matrix material and any outgassing are discharged via a drain 52 of the injection tool 5.

(60) With the provided layered and/or segmented structure of a mixer 20 with a blossom-shaped or meander-shaped contour preferably from a ceramic fiber-reinforced composite, different curing methods, in particular such as are corresponding to FIGS. 20 to 23, can be realized in an unproblematic manner by means of different manufacturing tools 3, 3inv that model the contour of the mixer 30 as a positive or negative mold. Here, a simplified demolding of the mixer 20 is in particular obtained by means of longitudinally displaceable radial arms 30a* or 30inv of the respective manufacturing tool 3, 3inv.

(61) FIGS. 24 and 24A once more illustrate a manufacturing tool 3 with a conical base body 30 at which radially protruding radial arms 30a* are supported in a displaceable manner for defining the first and second guide elements 210 and 220 of the mixer 20. At that, the individual material layers are arranged as (a) layer bonding(s) La at the outer contour of the manufacturing tool 3, for example in a manual or mechanical manner by means of pre-impregnated batts or dry batts.

(62) A manufacturing tool 3inv corresponding to FIGS. 25 and 25A predefines a negative mold. Here, the manufacturing tool 3inv surrounds a hollow space in the shape of a circular ring that defines the mixer opening O of the mixer 20 to be manufactured and into which radial arms 30inv project radially inward. Together with the gaps lying in between them, these radial arms 30inv define the outer contour of the second guide elements 220 as well as of the first guide elements 210 of the mixer 20. Thus, in this variant, a material layer bonding La is arranged at the inner side along the inner contour of the manufacturing tool 3inv in order to manufacture the mixer 20 in one piece. Here, too, the individual radial arms 30inv are longitudinally displaceable, so that demolding of the mixer 20 is considerably facilitated.

(63) In the injection tool 5 of FIGS. 26 and 26A, the two manufacturing tools 3 and 3inv are combined with each other. The manufacturing tools can for example be inserted into each other, so that the one manufacturing tool 3 forms an inner tool part and the other manufacturing tool 3inv forms an outer tool part. In that case, the two manufacturing tools 3 and 3inv define a circumferentially continuous hollow space in between them, with its contour corresponding to the contour of the mixer 20. Before the two manufacturing tools 3 and 3inv are joined together, the individual material layers are arranged at the outer contour of the manufacturing tool 3 or at the inner contour of the manufacturing tool 3inv that is formed in an inverted manner with respect to the former. After the two manufacturing tools 3 and 3inv have been connected, the matrix material RE, for example in the form of a resin, is supplied via the inlet 51 of the injection tool 5. After a corresponding curing process, the mixer 20 is present as a structural component from ceramic fiber-reinforced composite formed in one piece and can be removed from the injection tool 5.

(64) FIG. 28 shows a section of the base body 30 of the manufacturing tool 3 or 3inv. The base body 30, which is shown in sections here, has a channel system 6 for manufacturing a mixer 20 with side walls 231-234 of the first and second guide elements 210, 220 that extend in parallel to each other in the axial direction. The channel system 6 serves for the targeted heating and/or cooling of the manufacturing tool 3, 3inv by means of a fluid, e.g. water or oil, so that the base body 30 can be effectively cooled and shrunk, for example following curing of the mixer 20, in order to render demolding easier. In the present case, the channel system 6 has multiply branched fluid channels 61, 62 that extend through the interior of the base body 30. Alternatively or additionally, the channel system 6 may have corresponding fluid channels 61, 62 inside the radial arms 30a-30d, 30a*, 30inv that, where necessary, may be connected to the base body, so that (also) the radially extending radial arms 30a-30d, 30a*, 30inv can be heated and/or cooled in a targeted manner by means of an internally guided fluid.

(65) Providing a channel system 6 in the base body 30 and/or in the radial arms 30a-30d, 30a*, 30inv has proven to be advantageous e.g. in combination with a base body 30 or radial arms 30a-30d, 30a*, 30inv which are manufactured from a material with a comparatively high thermal expansion coefficient, such as aluminum. Here, the radial expansion that varies strongly based on the temperature can be controlled in a targeted and in particular in an automated manner by means of the fluid that flows inside the fluid channels 61, 62 of the channel system 6 to provide heating during the arrangement of the material layers at the manufacturing tool 3, 3inv and/or the curing, and to provide cooling of the base body 30 and/or the radial arms 30a-30d, 30a*, 30inv for demolding.

PARTS LIST

(66) 11 low-pressure compressor 12 high-pressure compressor 13 high-pressure turbine 14 medium-pressure turbine 15 low-pressure turbine 2 mixer assembly group 20 mixer 200 edge of the mixer 200.1, 200.2 edge segment 201bb, 202bb edge rim 20a-20g batt/material layer 20aa, 20bb, 20cc, 20dd batt/material layer 21 interface 21.1, 21.2 mixer segment 210 guide element 2100 convex outer curvature 220 guide element 2200 concave inner curvature 231, 232, 233, 234 side wall 3 manufacturing tool 30 base body 300 fastening groove 301a* fastening web 30a-30d radial arm 30a* radial arm 30inv radial arm 31 recess 32 thickening 3inv manufacturing tool 4 autoclave 5 injection tool 51 inlet 52 drain 6 channel system 61, 62 (fluid) channel A exhaust a1-a5 material layer a10, a11, a12 inner section B bypass channel b1-b4 material layer Ba material area of lesser stiffness Bb material area of high stiffness Bc overlapping area BK combustion chamber section C Outlet cone c1-c4 material layer c10, c11 inner section CA arrangement of the sectional lines for cutting d1-d5 material layer E inlet/intake F fan f1, f2 fluid flow FC fan housing FR tissue/fiber roll L longitudinal direction L1-L8, La material layer bonding l1-l9 gap LRE layer bonding (impregnated with resin) M central axis/rotational axis O mixer opening OL13, OL24, OL35, overlapping area OL46, OL57, OL68 R inflow direction R radial direction RE matrix material RR matrix reservoir S1-S8 joint area T (turbofan) engine TT turbine U circumferential direction V compressor V1-V4 thickened/reinforced area