1. Field of the Invention
The subject of this invention is a layout of a blisk that can be used in a turbine or a turbomachine compressor, for example.
2. Description of the Related Art
It is conventional that blades are provided with bulbs engaged in grooves notched into the disk, which hold the blades in place on the disk despite centrifugal forces that occur during operation. The grooves may be oriented along the axis of the disk and each may contain a bulb, or they may be circular and contain all the bulbs. The bulbs usually comprise oblique upper faces that bear on overhanging faces with the same obliqueness as the groove when centrifugal forces are applied. Inclinations of the groove relative to a median plane are sufficient so that no jamming occurs between these faces when centrifugal forces have ceased.
The invention is based on a wish to build some blades from a composite material such as CMC (Ceramic Matrix Composite). The difficulty that then arises is that the method of manufacturing by casting, compulsory for these materials, prevents excessive discontinuities in the orientation and therefore makes it essential that the inclination of the upper part of the bulb connected to the outer part of the blade in the radial direction should not exceed about 30°, while the inclination of the faces overhanging the groove has to be at least 40° to prevent jamming. Therefore, such blades cannot be directly integrated into a disk. The invention overcomes this problem.
In its general form, it relates to a layout comprising a disk and at least one blade, the bulb of which is housed in a groove in the disk, the groove comprising two faces overhanging a bottom of the groove with a first inclination relative to a median plane of the groove, characterised in that the bulb comprises two upper faces located under the overhanging faces but with a second inclination relative to said median plane that is less than the first inclination, and in that inserts are added between the bulb and the disk, which include main parts arranged between the overhanging faces and the upper faces, external parts connected to the main parts, extending through an opening in the groove and on a peripheral face of the disk, the distance between them increasing towards the free ends opposite the main parts, and internal parts connected to the main parts, extending between the bulb and the bottom of the groove, the distance between them reducing towards the free ends opposite the main parts.
The thickness of the main parts is variable, the inclination of their opposite faces being equal to the inclination of the overhanging face or upper face located in front of them, and therefore compensate for their difference in inclination, while the external parts hold inserts in position at rest by bearing on the peripheral face of the disk, and the internal parts have the same effect during operation, possibly bearing in contact with the bulb.
Therefore, this design of composite material blades can be used in a metal disk, and the inserts can also be metallic. According to one advantageous characteristic, the inserts are separated from each other at the internal parts to avoid the risk of creating any jamming by arching of the internal parts; and according to another advantageous characteristic, in an operating state in which the bulb is bearing on the central parts and the central parts are bearing on the overhanging faces, there are clearances between the external parts and the disk and between the internal parts and the bulb. As a result of this characteristic, the blade and then the inserts can drop towards the bottom of the groove when centrifugal forces cease, to prevent jamming.
The invention will now be described with reference to the FIGURE that shows a layout conforming with the invention in an operating state of the machine, in which centrifugal forces are applied on the different elements.
A groove (1) is formed in a disk (2) and it contains a bulb (3) of a blade (4). The groove (1) comprises a bottom face (5) and then two oblique overhanging faces (6) leading to an opening in the groove (1) leading to a peripheral face (7) of the disk (2). The bulb (3) also comprises a bottom face (8) above the face of the groove (2) and two oblique upper faces (9) in front of the overhanging faces (6) of the groove (1), and that are connected to the outer part of the blade (4). The bottom face (8) of the bulb (3) is connected to the upper faces (9) through a large radius rounding (10) that enables fabrication when the blade (4) is made of a composite material, but such rounding is not possible between the upper faces (9) and the outer part of the blade (4), such that the inclination of the upper faces (9) (measured from an imaginary median plane of the groove (1) defined by a local radial direction (R) of the disk (2) and an axial direction (A) of the groove (1) and the bulb (3)) is less than the inclination required for the overhanging faces (6) of the groove (1). Inserts (11) are then inserted between the bulb (3) and the wall of the groove (1). Each comprises a central part (12), an external part (13) and an internal part (14), the external and internal parts being attached to the central part (12) through its opposite ends. The central part (12) of each of the inserts (11) extends between an overhanging face (6) and an upper face (9) corresponding to it, and its opposite lateral faces have the same inclination as the face in front of them, such that the bulb (3) bears on the inserts (11) through first bearing surfaces (15) and the inserts (11) bear on the overhanging faces (6) through second bearing surfaces (16). The external parts (13) are curved outwards from the groove and overhang the peripheral face (7) of the disk (2) from which they are separated by clearances. The internal parts (14) are curved towards the middle of the groove (1) and extend towards each other from the central parts (12), but do not touch each other. Clearances separate them from the bottom (5) of the groove and from the bottom (8) of the bulb (3).
Satisfactory support of the blade (4) in the groove (1) is guaranteed by sufficiently large surface areas of the bearing surface contact areas (15 and 16) through which centrifugal forces applied on the blade (3) are transmitted to the disk (2) with a low contact pressure. And when the machine returns to rest and centrifugal forces cease, the bulb (3) and the inserts (11) drop to the bottom of the groove, the bottom (8) of the bulb (3) bearing on the internal parts (14) and the external parts (13) bearing on the peripheral face (7) without any jamming.
Number | Date | Country | Kind |
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10 50164 | Jan 2010 | FR | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2011/050245 | 1/11/2011 | WO | 00 | 7/3/2012 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2011/086056 | 7/21/2011 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
2950083 | Compton et al. | Aug 1960 | A |
3132841 | Wilder, Jr. | May 1964 | A |
4417854 | Cain et al. | Nov 1983 | A |
4802824 | Gastebois et al. | Feb 1989 | A |
6619924 | Miller | Sep 2003 | B2 |
7713029 | Davies | May 2010 | B1 |
8206118 | Propheter-Hinckley et al. | Jun 2012 | B2 |
20100284816 | Propheter-Hinckley et al. | Nov 2010 | A1 |
20140003924 | Bonneau et al. | Jan 2014 | A1 |
Number | Date | Country |
---|---|---|
2 077 376 | Jul 2009 | EP |
2 608 674 | Jun 1988 | FR |
Entry |
---|
U.S. Appl. No. 14/449,308, filed Aug. 1, 2014, Garin, et al. |
International Search Report Issued Apr. 14, 2011 in PCT/EP11/50245 Filed Jan. 11, 2011. |
Number | Date | Country | |
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20120308391 A1 | Dec 2012 | US |