Assembly for producing a molding made of removable material of a turbomachine
12343790 · 2025-07-01
Assignee
Inventors
- Hervé Bruno Marc Osmont (Moissy-Cramayel, FR)
- Ramzi BOHLI (Moissy-Cramayel, FR)
- Alexis LOURETTE (MOISSY-CRAMAYEL, FR)
- Joseph Toussaint Tami Lizuzu (Moissy-Cramayel, FR)
Cpc classification
B22D25/02
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
An assembly for producing a molding, made of removable material, of a turbomachine blade, includes an injection mold for the removable material in which a first core element and a second core element are mounted in a predetermined molding position, wherein the first and second core elements extend in a first direction. The mold includes a first face for molding a pressure-side face of the blade and a second face for molding a suction-side face of the blade and arranged facing the first face in a second direction perpendicular to the first direction. Retaining members hold the cores in position in the injection mold.
Claims
1. An assembly for producing a molding, made of removable material, of a turbomachine blade, comprising an injection mold for said removable material in which a first core element and a second core element are configured to be mounted in a predetermined molding position, the first and second core elements extending in a first direction, the mold comprising: a first molding face configured to mold a pressure-side face of the blade and a second molding face configured to mold a suction-side face of the blade and arranged facing the first face in a second direction perpendicular to the first direction, and retaining members configured to hold the cores in position in the injection mold, wherein at least a first retaining member extends from the first face of the mold in the second direction and extends at least partially through the first and second core elements, the first retaining member comprising a first support point at which the first retaining member bears against the first core element and a second support point at which the first retaining member bears against the second core element.
2. The assembly according to claim 1, wherein the first core element and the second core element are shaped so that the first support point of the first retaining member blocks movement of the first core element in a first directional orientation along a third direction perpendicular to the first and second directions, and the second support point of the first retaining member blocks movement of the second core element in a second directional orientation that is opposite to the first directional orientation along the third direction.
3. The assembly according to claim 1, wherein a second retaining member extends from the first molding face in the second direction, the second retaining member comprising a first support point at which the second retaining member bears against the first core element and a second support point at which the second retaining member bears against the second core element, said first support point and second point of support of the second retaining member being different from the first support point and the second support point of the first retaining member.
4. The assembly according to claim 3, wherein the first core element and the second core element are shaped so that the first support point of the second retaining member blocks movement of the first core element in the first directional orientation along a third direction perpendicular to the first and second directions and the second support point of the second retaining member blocks movement of the second core element in a second directional orientation that is opposite to the first directional orientation along the third direction.
5. The assembly according to claim 4, wherein the second retaining member comprises a spacing means between the first support point of the second retaining member and the second support point of the second retaining member, the spacing means ensuring, during production of the molding made of removable material, a spacing of a constant distance between said support points along the third direction.
6. The assembly according to claim 1, wherein the first retaining member comprises a spacing means between the first support point of the first retaining member and the second support point of the first retaining member, the spacing means ensuring, during production of the molding made of removable material, a spacing of constant distance between said support points along at least one among the first direction, the second direction, or the third direction.
7. The assembly according to claim 1, wherein the first retaining member and/or the second retaining member is movable between a retaining position, in which the second retaining member holds at least one core element, and a retracted position, the retaining member comprising a retraction mechanism configured to position the retaining member in the retaining position or in the retracted position.
8. The assembly according to claim 1, wherein the first retaining member and/or the second retaining member comprises an axis of rotation and a head that is eccentric relative to the axis of rotation and that cooperates with the first core element and the second core element.
9. A method for producing a molding, made of removable material, of a turbomachine blade, the method comprising: providing a first core element and a second core element, said core elements extending in a first direction; and providing an injection mold for said removable material, wherein the mold comprises: a first molding face configured to mold a pressure-side face of the blade and a second molding face configured to mold a suction-side face of the blade and arranged facing the first face in a second direction perpendicular to the first direction; and retaining members configured to hold the cores in position in the injection mold, among which at least a first retaining member extends from the first molding face in the second direction, the method further comprising the step of positioning the first core element and the second core element on the first molding face such that the first retaining member extends at least partially through the first and second core elements and comprises a first support point at which the first retaining member bears against the first core element and a second support point at which the first retaining member bears against the second core element.
10. The method according to claim 9, the mold further comprising a second retaining member extending from the first molding face in the second direction, the method further comprising the step of positioning the first core element and the second core element on the first molding face such that the second retaining member comprises a first support point at which the second retaining member bears against the first core element and a second support point at which the second retaining member bears against the second core element.
Description
DESCRIPTION OF THE DRAWINGS
(1) Other features, details and advantages will become apparent upon reading the detailed description below, and upon analyzing the attached drawings, in which:
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DETAILED DESCRIPTION
(11) The terms upstream and downstream used below are defined in relation to the direction of flow of gases through a turbomachine, indicated by arrow F in
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(13) Paired core elements 21, 22 extend in three perpendicular directions, a first direction Z, hereinafter designated longitudinal direction Z corresponding in the final blade to the longitudinal direction connecting the root to the tip of the blade, a second direction Y, hereinafter designated transverse direction Y, passing through the pressure-side and suction-side faces of the blade, and a third direction X, hereinafter axial direction X, corresponding in the final blade to the upstream/downstream direction (arrow F). In
(14) Trailing core element 21 further comprises a notch 32 in its downstream edge 30. Notch 32 is arranged in the area of head 25f. Notch 32 is substantially U-shaped, oriented so that the opening of the U-shaped concavity is oriented along axial direction X.
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(16) In particular, retaining members P1a, P1f, P2a, P2f, P3a and P3f allow leading core 22 element or trailing core element 21 of both core elements 21, 22 to be held in position along transverse direction Y. Retaining members P1a, P2a, and P3a are provided for holding leading core element 22 in position along transverse direction Y. Retaining members P1f, P2f, and P3f are provided for holding trailing core element 21 in position along transverse direction Y. Each of retaining members P1a, P1f, P2a, P2f, P3a and P3f extends from first molding face 20, in transverse direction Y. Each of these members bears against one of the two cores, which prevents movement of the cores along transverse direction Y.
(17) In particular, retaining members P1a, P2a, P2f and P1f are arranged in the area of foot 26a, 26f of the cores. Retaining members P1a, P2a, P2f and P1f are aligned along axial direction X. Retaining members P1a, P2a, P2f and P1f are arranged near the free end 31a, 31f of the cores. In other words, retaining members P1a, P2a, P2f and P1f are arranged outside the free end of the cores, but in the area of foot 26a, 26f of the cores. Retaining members P1a, P2a, P2f and P1f end in a support surface for the respective core, each of these support surfaces being substantially flat. In addition, each of these support surfaces is substantially perpendicular to transverse direction Y. These surfaces are located outside the functional area.
(18) Retaining members P3a and P3f are arranged in the area of head 26a, 26f of the cores. Retaining member P3a and retaining member P3f are offset along longitudinal direction Z. In other words, retaining members P3a and P3f are not aligned along axial direction X. Retaining members P3a and P3f end in a support surface for the respective core, each of these support surfaces following the shape of the area of contact with the core. In other words, for optimal support, the support surfaces of retaining members P3a and P3f follow the shape of the surface of the core area with which they are in contact.
(19) Additionally and alternatively, the second molding face may comprise retaining members similar to the retaining members described above, so as to lock the cores in position along transverse direction Y.
(20) First molding face 20 may further comprise retaining members P6a and P6f. Retaining members P6a and P6f allow leading core element 22 or trailing core element 21 to be held in position along longitudinal direction Z, for example. Each of these members respectively bears against leading core element 22 and trailing core element 21, which prevents movement of the cores along longitudinal direction Z. Retaining member P6a is provided for example to retain leading core element 22 in position along longitudinal direction Z. Retaining member P6a extends from the first molding face, in transverse direction Y. Retaining member P6a bears against lower cutout wall 272a of leading core element 22. Retaining member P6f is provided, for example, for holding trailing core element 21 in position along longitudinal direction Z. Retaining member P6f extends from the first molding face, in axial direction X, in the downstream to upstream directional orientation. Retaining member P6f comes to rest in notch 32 of downstream edge 30 of trailing core element 21.
(21) Alternatively, a retaining member P6f may be provided instead of retaining member P6f. Retaining member P6f is provided for holding trailing core element 21 in position along longitudinal direction Z. Retaining member P6f extends from first molding face 20, in transverse direction Y. Retaining member P6f bears against lower cutout wall 272f of trailing core element 21. In addition, retaining members P6a and P6f are arranged so that the cutouts of the two cores are substantially aligned along axial direction X.
(22) Only one of the two retaining members P6f and P6f is used for the production of the wax molding, to position trailing core element 21 in longitudinal direction Z. Depending on the retaining member used, P6f or P6f, the retaining member not in use is removed from the molding surface so as not to create a hyperstatic system. The choice of which point to use depends on the distribution of the desired expansion of the two cores during casting of the alloy.
(23) In fact, retaining member P6 allows distributing the expansion of trailing core element 21 along longitudinal direction Z, towards head 25f and towards foot 26f, while avoiding too much of a difference in length compared to leading core element 22, particularly in the event of very different expansions between the two cores. On the other hand, retaining member P6f is advantageously used to control the dimensions of a so-called bottom wall of a squealer tip present in the final blade. The bottom wall of the squealer tip is physically realized by cutouts 27a, 27f of the cores, which form a portion filled with material in the final blade. The bottom of the squealer tip is substantially planar, and extends in transverse direction Y and axial direction X. Due to the fact that the cores do not touch one another, meaning that they are not in contact, a portion of material referred to as a residual wall of the squealer tip bottom, separates the squealer tip bottom into two parts arranged at different levels along longitudinal direction Z. Residual wall 26 extends in longitudinal direction Z, from the bottom of squealer tip. The height of the residual wall, in longitudinal direction Z, is a characteristic which must be controlled in order to meet the aerodynamic performance of the blade. Indeed, it is desirable that the height of the residual wall be as low as possible, so as to avoid, to the extent possible, too significant of a difference in level between the portions of the squealer tip bottom. Consequently, retaining member P6f, associated with retaining member P6a, places cutouts 27a and 27f in the same plane in the cores, which makes it possible to obtain two parts of the squealer tip bottom which are substantially in the same plane perpendicular to longitudinal direction Z.
(24) The first molding face further comprises retaining members P4 and P5. Retaining members P4 and P5 allow leading core element 22 or trailing core element 21 or both core elements 21,22 to be held in position along axial direction X. Retaining members P4 and P5 are retaining members common to the two cores, leading core element 22 and trailing core element 21. To this end, retaining members P4 and P5 each comprise a first support point at which it bears against the leading core and a second support point at which it bears against the trailing core. Retaining members P4 and P5 together prevent rotation of the cores around transverse axis Y. Each of retaining members P4 and P5 extends from the first molding face, in transverse direction Y.
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(26) Retaining member P4 (or first retaining member) may be arranged in the area of head 25a, 25f. Retaining member P5 (or second retaining member) may be arranged in the area of foot 26a, 26f at the connection to free end 31a, 31f. Retaining members P4 and P5 may further be aligned in longitudinal direction Z. Retaining members P4 and P5 are arranged in a non-functional zone, meaning external to the part.
(27) Retaining member P4 can be seen in
(28) Retaining member P5 can be seen in
(29) In addition, retaining member P4 and/or retaining member P5 may be movable between a retaining position and a retracted position. In the retaining position, visible in
(30) Alternatively, retaining member P4 and/or retaining member P5 may further comprise a spacing means D4, D5 between their first and second support points. The spacing means ensures a separation (or spacing) of a constant distance between the first and second support points, the separation distance being measured for example in axial direction X. More precisely, spacing means D4, D5 keeps the two cores spaced apart from each other without them being in contact, meaning without the cores touching each other. Given that the cores extend in the three spatial directions, the separation distance may be measured in longitudinal direction Z or in transverse direction Y. A spacing means is for example physically realized by the diameter of the retaining member. The retaining member may for example have a constant diameter along its entire length. According to another example, the retaining member may have a smaller diameter towards its free end, and a larger diameter towards its base (meaning towards the first molding face).
(31) Alternatively, retaining member P4 and/or retaining member P5 may further comprise adjustment means for adjusting the position of the cores in the first molding face. For example, the adjustment means is an eccentric, which may be rotated around transverse direction Y in order to shift the two cores in the plane formed by the transverse and axial directions.
(32) In another alternative, first molding face 20 may further comprise counter-braces, as illustrated in
(33) Alternatively, although not illustrated, the elements described above for retaining member P4 may be applied to retaining member P5, and conversely the elements described above for retaining member P5 may be applied to retaining member P4. For this purpose, the first retaining member may be retaining member P5 and the second retaining member may be retaining member P4. Thus, the first support point and the second support point of first retaining member P5 may respectively be points P5a and P5f, and the first support point and the second support point of second retaining member P4 may respectively be points P4a and P4f.
(34) We now describe a method for producing a molding, made of removable material, of a turbomachine blade, the method comprising: providing leading core element 22 and trailing core element 21; providing the injection mold for the removable material; positioning leading core element 22 and trailing core element 21 on first molding face 20. In this position, the first retaining member has a first support point at which it bears against a first support surface of a core element, the first bearing surface extending against the core in order to hold the core element in position along the second direction. Furthermore, in this position, retaining member(s) P4, P5 at least partially extend(s) into leading core 22 element and trailing core element 21.
(35) Alternatively, the method may comprise: closing the mold while positioning on the core elements the second molding face, with at least one complementary retaining member.