Patent Application
20190128133
The invention relates to turbomachine distributors, and a turbomachine comprising such distributors.
The invention relates to the placing of anti-wear material on sectors of fixed distributor blades, especially turbine blades.
In a turbomachine, the turbine recovers some of the energy from the combustion of gases to operate the fan, the compressor and the accessories. One of the pieces constituting the turbomachine is the distributor.
For this, a known process consists of depositing, after manufacture of the blade, anti-wear material in the region of some friction zones by brazing or filling, in the region of the protuberance and in the region of the contact surface. But this process, called “stelliting”, from the commercial name of the anti-wear material generally employed, is complicated and causes cracking, brittle zones at the interface between the two materials and missing material.
Also, these zones which wear, must be repaired regularly. Typically, the rest of the anti-wear material is removed and a new layer is laid.
Document FR2993002 describes another type of fastening between the sectors, with especially a pin lodged in a slot and wedged in between two opposite surfaces, which acts as anti-wear material.
Another known process consists of placing an insert in the blade which, after heating, forms an integral. But this causes difficulties at the interfacing, especially due to the bi-material character of the blade.
There is consequently a need for improving to simplify the “stelliting” of distributor segment.
The invention proposes an assembly comprising:
a sector of fixed blades for turbomachine distributor comprising at one circumferential end a protuberance and at another circumferential end a contact surface, such that the protuberance of a sector arrives opposite the contact surface of another adjacent sector,
a detachable cap comprising a surface with anti-wear material, configured to be engaged detachably on the protuberance of the sector, such that the anti-wear material is in contact with the contact surface of the other sector.
The invention can comprise the following characteristics, taken singly or in combination:
the sector comprises an internal platform comprising an upper plate, on which are fixed the fixed blades and a lower plate, connected to the upper plate by a spacer,
the protuberance and the contact surface are at the ends of the upper plate or of the lower plate,
the anti-wear material is in the form of a wafer which defines the surface,
the cap is made entirely of anti-wear material,
the anti-wear material comprises cobalt or an alloy of cobalt,
the cap is in the form of a block comprising a blind recess forming a cavity suitable for receiving the protuberance, such that the protuberance is enveloped by the cap,
the contact surface comprises anti-wear material.
The invention also relates to a portion of turbomachine distributor comprising at least two assemblies such as described earlier, defining two sectors, wherein the protuberance of one of the two sectors comprises the detachable cap put in place, the latter being engaged with the contact surface (120) of the other sector.
Finally, the invention proposes a distributor comprising a plurality of portions such as described earlier, the portions being placed end to end.
Other characteristics, aims and advantages of the invention will emerge from the following description which is purely illustrative and non-limiting and which must be considered with respect to the appended drawings, in which:
The detailed description will be given on a sector of distributor, for example in the region of the turbine stages.
A distributor 1 is made by assembling several sections 1 placed end to end circumferentially around an axis X-X of the turbomachine.
Each section comprises an internal platform 100 (which generally refers to abradable material and creates sealing with the upstream and/or downstream mobile wheel), an external platform (not shown), attached to a housing, and a plurality of blades 2 whereof the radial ends are attached to the two platforms respectively. The blade 2 is the part which receives the flow of air emanating from an air stream (primary stream for a dual-flow turbomachine turbine for example). When installed, the blade 2 extends radially towards the outside relative to the longitudinal axis X-X of the turbomachine. The direction of extension of the impeller 110 substantially defines a direction Z-Z. In one embodiment the segment 1 comprises six blades.
The internal platform therefore exhibits a form of annular segment type.
The surfaces of the platforms radially delimit an aerodynamic flow channel, called a stream.
As illustrated in
Defined at the other circumferential end of the internal platform 100 is a contact surface 120 (see reference S120 in
The protuberance 110 is typically formed in the extension of the internal platform 100 according to the direction Y-Y. In the same way, the contact surface 120 is typically formed by recessing in the internal platform 100 to create the necessary axial offset.
The internal platform 100 can comprise an upper plate 102, separated from a lower plate 104 by a spacer 106. The upper plate 102 carries the blades 2 and the lower plate 104 serves for example to carry the abradable material to ensure tightness with upstream and/or downstream wheels.
A cap 200 is provided to better generate friction. It can be fitted on (
The surface 205 is made of anti-wear material and rubs the contact surface 120 of the platform 100.
The cap 200 therefore serves as sheath for the protuberance and installs anti-wear material (called “stellite”) on the internal platform rapidly and simply.
The cap 200 therefore envelops the whole end of the protuberance, ensuring good hold. Its sole degree of liberty is according to the axis Y-Y, where it comes to stop against the adjacent segment.
In one embodiment, the anti-wear material 210 is in the form of an applied wafer which defines the surface 205. The worn wafer can simply be exchanged for a new one.
In another embodiment, the whole cap 200 is made of anti-wear material. This embodiment has the advantage of also offering better resistance to wear caused by tangential shifts according to the direction Y-Y′.
The cap 200 is in the form of a block with a blind recess 202 having a base 204. The recess 202 creates a cavity inside which the protuberance 110 is housed.
The recess 202 has a form complementary to the protuberance 110 so it can the least possible play between the two. Also, as the protuberance is generally not circular in cross-section, neither is the recess 202 and the rotation of the cap 200 is naturally prevented.
Because of the cap 200, there is no need for the contact surface 120 of the segment to comprise an anti-wear material, therefore simplifying “stelliting”. But since stellite is a very hard material, it is preferable to have a contact surface 120 likewise made of anti-wear material, generally the same. The contact surface 120 is preferably covered by a cap in turn.
The placing of the cap 200 is done by insertion in translation according to the direction Y-Y, which is rapid and minimally labour-intensive. Simple nesting is preferred, without adhesive or other fastening means and just one operator is required.
Once the material 210 worn, only the cap 200 or the wafer is replaced.
Also, such a cap does not dictate reviewing the structure of the segment 1. In fact, the thickness of stellite deposited by brazing (for example) is replaced by the thickness of the cap 200 and of the surface 205 of anti-wear material.
Cobalt or an alloy of cobalt is used as anti-wear material, for example.
The length according to the direction Y-Y has to be sufficient to ensure retention, such as five millimeters for example.
| Number | Date | Country | Kind |
|---|---|---|---|
| 17 60288 | Oct 2017 | FR | national |
