The present invention relates to broaching of slots for parts such as turbine rotor discs or turbomachine compressor discs.
It applies especially to broaching of slots of “fir-tree sections” or “bulbs” type for rotor discs or turboengine compressors or aircraft turboprop.
In classical terms, a turboengine or aircraft turboprop comprises a compressor part and a rotary turbine. This turbine in turn comprises a rotor disc which has peripheral attachments (slots in the form of “fir tree sections” or “bulbs”) which are distributed over its circumference and which take up and hold the feet of the blades of said turbine. Some compressor discs also comprise such attachments.
These attachments are generally machined by broaching.
For this reason, as illustrated in
In the case of slots 3 as “fir tree sections” or in the form of “bulbs” on the periphery of a rotor disc 4 of a turbomachine turbine or a compressor disc, the broaching is often done at a specific inclination (broaching angle α in
These alternative forces (arrows F1, F2, F3 in
This problem is particularly exacerbated in the case of small-sized parts.
An aim of the invention is to resolve this problem.
Many general multicriterion methods of optimisation of broaching tools have already been proposed.
In general, manufacturers of broaches are prohibited from using sub multiple pitches of the thickness to be broached. In the most current cases where the parts to be broached are stacked, use of a sub-multiple pitch of the thickness to be broached is likely to generate substantial deformations on the parts. In general, this rule is also applied in the event where a single part is broached.
The article by Ozturk, O. & Budak, ‘Modeling of broaching process for improved tool design’. Proceedings IEMCE'03, Washington, D.C., Nov. 16-21 2003, p. 1-11 has already proposed using broaching tools with a sub-multiple pitch of the thickness of the part.
The authors indicate in this article that even with this solution it is extremely difficult to produce a variation in zero force between the entry and exit of a part.
Also, this article does not focus on the problems of inclined broaching.
An aim of the invention is especially to reduce the variation in cutting forces and reduce deforming of slots.
For this purpose, a broaching process is proposed of at least one slot in a part such as a turbine rotor disc or a turbomachine compressor disc, said slot being machined by means of an inclined broach with a broaching angle relative to the part. Said broach has an inter-tooth pitch as a sub-multiple of the length to be broached.
So, given the difference between the thickness of the part to be broached and the length to be broached which is due to inclination of the broaching, the inter-tooth pitch of the broach is optimised so as to minimise deforming of the slots.
A broach is also proposed for executing this process.
Other characteristics and advantages of the invention will emerge from the following description which is purely illustrative and non-limiting, and must be considered with respect to the appended figures, in which:
The broach 1 comprises a plurality of teeth 2. Two successive teeth are separated in pairs by a core 5, the empty space between the core and the apex of the tooth constituting the chip chamber.
The machining it executes is inclined (broaching angle α), such that the thickness Ep of the part to be broached constituted by the rotor disc 4 is different to the length to be broached L.
As illustrated in
In this way, a tooth 2 enters the slot 3 in formation at the periphery of the machined part (rotor disc 4) at the moment when another tooth 2 exits from it.
The forces (arrows F1 to F4 in
This principle is illustrated by
Given the intervals of tolerancing admitted for the parts machined in this way, the value of the pitch is advantageously selected as equal to:
where:
It should be noted that the thickness Ep is determined for a given pass of broach 1.
It is calculated from rim to rim between broaching edges on entry and exit of the machined slot 3.
It is likely to vary according to the depth of the slot to which the pass of the broach 1 corresponds, with a rotor disc able to have a variable thickness, especially at the level of its periphery.
The broaching angles α are also determined for each pass. They correspond to the angle between the axis A of descent of the broach 1 and the thickness of the part 4 at the level of the area to be broached.
The broaching which has just been described is particularly interesting in the case of small-sized turbine rotor discs and in particular discs with reduced inter-blade spacing.
By way of example, this broaching can be used advantageously in the case of turbine discs or compressors with thicknesses less than 20 mm, a maximal slot depth (Pmax in
The number of teeth n is preferably equal to 2 but could also be equal to 3 or 4.
Number | Date | Country | Kind |
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1350893 | Feb 2013 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2014/050144 | 1/27/2014 | WO | 00 |