Patent Application
20240326138
Many high specification materials of the type used in the aerospace industry are metal alloys which are extremely hard and durable and which can withstand high temperatures and stresses. They are used in many applications where such materials are often required for high performance components. These components also often have small geometrical tolerances and so careful machining is required using specialist hardened cutting tools and materials.
Complex geometries can be created using multi-axis machining centers such as a 5-axis machining center. The high cutting speeds used in such machines can generate vibrations that are detrimental to the precise tolerances needed in some components.
The inventors have established that the performance of such machinery can be improved in terms of accuracy, reliability and cutting performance using an unconventional modification. This can dramatically increase productivity.
The present disclosure is concerned with a machining apparatus particularly, but not exclusively, for lathe or milling machine made components. One such machine is a milling machine in which a cutting bit or tip is held in a tool holder which is caused to rotate at high speed and to cut through material.
Viewed from a first aspect of this disclosure, there is provided a damping apparatus for a machine tool, the damping apparatus comprising an annular body with an inwardly facing surface, the inwardly facing surface arranged for coupling to an outer surface of a machine tool stem or an outer surface of a machine tool holder, wherein the annular body comprises an internal cavity, the cavity comprising a damping mass.
Thus, according to such an arrangement a machine tool damper is provided that may be conveniently fitted to any machine tool, including retrofitting to existing machine tools. The arrangement provides a dynamic moving body mass within the apparatus housing that responds to and substantially dampens vibrations generated by cutting actions of a cutting tool to which the damper is arranged. The annular body allows for convenient coupling to a candidate part of a machine tool stem or holder.
Advantageously the arrangement may be adapted to be coupled to any size of machine tool holder or stem and provides a simple and reliable construction that is highly resistant to the working environment of machine tooling. The arrangement may be conveniently manufactured as described herein and provides for highly reliable operation.
Furthermore the tooling damper may be optimised to the specific operating ranges of a cutting action though the selection of damper mass and elastomer.
The damping mass may be is coupled to and spaced from the inwardly facing surface of the internal cavity by one or more elastomeric or rubber coupling(s). The elastomeric or rubber couplings act as the dynamic couplings that distort as dynamic forces are applied to the material. The incompressibility of rubber causes the elastomeric material to distort rather than merely compress under loads. This provides the damping action.
The elastomeric couplings may optionally be arranged around the circumference of the damping mass. Thus, cutting forces acting in complex multi-directions can be damped.
The damping mass may be in the form of a generally cylindrical body with two opposing end faces and one or more elastomeric couplings arranged on the end faces of the damping mass. According to such an arrangement a simple and reliable construction of tooling damper can be realised which is simple to manufacture and also minimises complex modelling to select the damping mass and required elastomeric reaction forces. Radial and axial cutting forces as well as complex cutting forces can thus be damped.
In one arrangement the elastomeric couplings may be in the form of O-rings. Thus, manufacturing costs can be minimised and tight tolerances that O-ring seals provide can allow for reliable damping action.
Advantageously, the elastomeric couplings may be in the form of a plurality of discrete elastomeric elements. Thus, high cutting forces can be damped using multiple elastomeric elements and/or cutting forces can be damped with minimal diameter elastomeric elements.
The elastomeric couplings may also be coupled to the inwardly facing surface of the annular body thus facing the damping mass. Such an arrangement allows the damping mass to be manufactured as a simple geometrical shape with an outer surface machined to cooperate with the inwardly facing elastomeric elements.
In an alternative arrangement the elastomeric couplings or elements may be coupled to the outer surfaces of the damping mass. The inwardly facing surfaces of the annular body may then be machined to cooperate with the outwardly facing elastomeric elements.
Furthermore, the elastomeric or rubber elements may be continuous and portions of the inwardly facing surfaces of the annular body and/or outer surfaces of the damping mass may be provided with recesses in alignment with the line of contact of the elastomeric elements and the damping mass. Thus, the elastomeric or rubber elements may be retained in position such that vibration forces or alternatively forces used during manufacture of the damper do not dislocate the elements i.e. move the elements out of their predetermined damping positions.
The damping mass itself may be in the form of a single metallic or plastic element. This provides for simple manufacture and assembly of the damping arrangement.
The inwardly facing surface of the annular body may additionally be provided with a plurality of circumferentially spaced recesses or grooves in alignment with one or more elastomeric or rubber couplings. Again, the position of the elements can thereby be ensured.
The grooves or recesses may advantageously be equally spaced around the damper. For example, 6 grooves may be equally spaced around the damper. Each groove or recess may extend between 5 and 15 degrees around the circumference of the damper and have a depth of between 0.5 and 3 mm.
In an alternative arrangement the damping mass may be formed of a plurality of discrete and independent elements contained within the internal cavity. In such an arrangement a single damping mass surrounded by elastomeric elements may be replaced with a plurality of discrete elements within the annular body.
In one arrangement the plurality of discrete and independent elements may be in the form of a plurality of metallic elements. Such elements may be, for example, selected from powder, shot peen or metallic spheres. Other materials may also be selected for each option such as plastics with a predetermined density to effect damping. In such arrangements the movement and friction between adjacent elements in the plurality of elements cause the damping action.
Viewed from another aspect, there is provided a damper for a tool comprising a cylindrical body and a central circular aperture; the cylindrical body comprising radially inwardly extending fixtures arranged to couple the damper to a portion of the tool, wherein the damper comprises a circumferentially extending cavity within the damper, the cavity comprising a movable damping mass.
Viewed from yet another aspect there is provided a cutting tool comprising a damping apparatus as described herein. According to such an aspect a damping apparatus may be fixed to the stem of a cutting tool. This fixture may be removable to allow for damped and non-damped operation and/or maintenance. For example, the damping apparatus may be coupled to a tool holder of the machine.
Viewed from yet another aspect there is provided a tool holder comprising a damping apparatus as described herein.
Viewed from another aspect there is provided a cutting tool for a machining center comprising an elongate cylindrical body and a damping apparatus as described herein.
Viewed from another aspect there is provided a method of damping a tool stem comprising the steps of:
It will be recognised that the damping arrangement and tools comprising such a damping arrangement provide a reliable and highly tuneable damper which may be easily manufactured and which required minimal maintenance. Such advantages are highly desirable in manufacturing applications which extremely tight tolerances are required at high machining outputs. One such example is an aerospace engine or hybrid fuel powered component manufacturing. The rotational speeds within such application make higher tolerances and reliability highly desirable.
Aspects of the disclosure will now be described, by way of example only, with reference to the accompanying figures in which:
Any reference to prior art documents in this specification is not to be considered an admission that such prior art is widely known or forms part of the common general knowledge in the field. As used in this specification, the words “comprises”, “comprising”, and similar words, are not to be interpreted in an exclusive or exhaustive sense. In other words, they are intended to mean “including, but not limited to”. The invention is further described with reference to the following examples. It will be appreciated that the invention as claimed is not intended to be limited in any way by these examples. It will also be recognised that the invention covers not only individual embodiments but also combination of the embodiments described herein.
The various embodiments described herein are presented only to assist in understanding and teaching the claimed features. These embodiments are provided as a representative sample of embodiments only, and are not exhaustive and/or exclusive. It is to be understood that advantages, embodiments, examples, functions, features, structures, and/or other aspects described herein are not to be considered limitations on the scope of the invention as defined by the claims or limitations on equivalents to the claims, and that other embodiments may be utilised and modifications may be made without departing from the spirit and scope of the claimed invention. Various embodiments of the invention may suitably comprise, consist of, or consist essentially of, appropriate combinations of the disclosed elements, components, features, parts, steps, means, etc, other than those specifically described herein. In addition, this disclosure may include other inventions not presently claimed, but which may be claimed in future.
The spindle is coupled to a spindle drive arrangement 4, which is arranged to rotate the spindle (and thus the tool) at high speed. At the opposing end of the machining center (to the drive arrangement) is the chamber that houses the component to be machined (the workpiece) 5 which is secured to a movable table 6. The table 6 is movable in multiple directions (vertically and rotationally). In combination with the axial movement of the cutting spindle the cutting tool can be moved relative to the workpiece in each of the axes shown to the right of
The machining center comprises a large number of sensors which accurately detect the position of the table 6 and cutting tool so that in operation accurate machining can be performed.
The table 6, spindle 3 and drive arrangement 4 each have a large mass to prevent excessive vibrations during a machining operation. Increasing the mass and rigidity of each of the components of the machining center reduces vibrations during machining, allowing for accurate machining. A vibration alarm 7 is however provided which deactivates the cutting (milling) operation if vibration levels exceed a predetermined threshold. In this scenario a vibration or ‘excessive movement’ alarm is used which detects machine vibration and compares it to a predetermined threshold or level. Vibrations may increase beyond a predetermined level for a number of reasons such as increased tool wear, an increased hardness in a portion of the workpiece or unfavorable cutting characteristics/conditions.
The inventors have however devised an alternative arrangement to effectively damp the vibrations directly on the tool holder or tool beam as described below.
All tools have a number of natural frequencies in their basic construction. Some of these natural frequencies can be disruptive and lead to excessive vibrations during a machining operation. The natural frequencies originate from each part or element in the tool. The different vibrations interact (both constructively and destructively) resulting in an overall vibrational performance of a tool being complex and specific to the given machine and, importantly, operating or cutting speeds and conditions.
In one example, there is a need to improve the dynamic stability of a cutting tool at a given cutting speed in revolutions per minute (rpm). For example, for a ceramic cutting tip this may be a cutting speed of 12,000 rpm and a frequency of 200 Hz.
The arrangement comprises a tool beam (TB) that carries a ceramic tool (or the like) in a conventional distal cutting bit connector. The tool beam is located within the damping collar (DC) shown in the center of
It will be recognised that the arrangements conveniently allows the damper to be positioned at any point along the tool beam shaft, either abutting with the tool holder on the right or towards the distal end of the tool beam (towards the left).
The collar is located around the tool beam and is then tightened causing the collar to grasp the outer surface of the tool beam. The damper can then be secured to the tool beam at the desired position.
As will be described below, the unconventional damping arrangement and effect are achieved entirely within the damping collar DC meaning conventional tool beams and couplings to cutting machines can be used. Thus, a damper described herein can be conveniently retro-fitted to existing tool beams or tool holders for effective damping. If fact, the arrangement described herein can be adapted to fit onto any tool beam or tool holder to achieve a damping effect.
During operation of the machining apparatus vibrations are created in the machine and tool and this causes vibration of the outer casing of the damping collar. This in turn causes vibration of the damping mass through the elastomeric O-ring connections and this creates a damping effect because of the latency of movement of the damping mass with respect to the damping unit as the elastomeric couplings compress and expand out of synchronisation with the excitation frequency.
The specific performance of the damper can be selected depending on the characteristics of the machine and the desired damping performance. For example, the contact area between the damping mass and annular body (described below) may be modified in combination with the elastomer hardness to achieve the desired performance. In one example, a shore hardness of between 70 and 90 shore A may be used.
The arrangement comprises a tool holder (12) which holds and supports a cutting tool 13. The cutting tool itself holds a cutting tip which engages and cuts the workpiece during the milling operation.
According to the disclosure, an annular damping arrangement 14 is provided. In the example shown in
The damper (the damping collar illustrated in
The damper 14 is shown in
The annular body 15 comprises an internal cavity 18. The body 15 is formed of a first portion 19A in which the cavity 18 is formed and a second portion 19B which forms the closed end of the cavity 18. The two portions 19A and 19B are coupled together with a threaded portion 20. This allows the cavity to be closed.
The cavity 18 comprises a damping mass 21 which is contained within the cavity 18. As shown the damping mass 21 is spaced from the inner surface of the cavity by a space 22.
The damping mass 21 is separated from, and connected, to the inner surface of the cavity 18 by a plurality of elastic couplings 23A-23F. The elastic couplings are arranged to allow movement of the damping mass relative to the inner surfaces of the cavity. The elastic properties of the elastic couplings cause a latency in movement of the damping mass relative to the cavity surfaces. This latency provides a damping effect.
In the arrangement shown in
In use vibration of the tool/tool holder is transmitted to the annular body and, through the elastic couplings, to the damping mass. Because the elastic couplings impart a latency to the movement of the damping mass relative to the annular body a damping effect is achieved which acts to damp the vibration of the annular body and thereby the tool or tool holder to which the annular body is attached.
The O-ring seals provide the elastic coupling between the damping mass and the annular body. This provides for the relative movement of the damping mass with respect to the annular body and thus the damping effect can be realised. The cross-section shown in
The elastomeric elements, such as the O-rings, may be arranged to be in continuous contact with the damping mass 21 on one side and the inner surface of the cavity on an opposing surface. In such an arrangement the O-ring seals may extend continuously around the circumference of the damping mass and in circular profiles around the axial ends of the damping mass. The damping mass is thereby spaced from the surrounding cavity inner wall but is simultaneously coupled thereto through the elastomer material.
An alternative arrangement is shown in
It will be recognised that the recesses could equally be additionally or alternatively formed on the outer surface of the damping mass itself in another example embodiment.
By selecting the hardness of the O-ring material and the size of the recess a pre-loading or compressive force can be created on the O-ring. In effect the optimum attenuation for a given modal mass can be achieved by selecting the appropriate hardness. The selected hardness will be dependent on the vibration and damping mass and the desired attenuation.
The arrangement shown in
The elements 26 may be selected according to the desired damping requirements. The number and density of the elements may be selected to achieve a desired cumulative mass of the damping mass. In one arrangement a shot peen material may be used comprising individual elements having a size of approximately 0.30 mm in diameter (ranging between 0.2 mm and 0.4 mm). In one arrangement the diameter is 0.36 mm.
In another arrangement a metal, plastic or textile may be selected. The size may advantageously be between 0.3 mm and 15 mm in diameter and have a density of between 0.5 and 19 kg/dm3
In
Finally,
| Number | Date | Country | Kind |
|---|---|---|---|
| 2109869.4 | Jul 2021 | GB | national |
This application is a national stage of, and claims priority to, Patent Cooperation Treaty Application No. PCT/EP2022/068469, filed on Jul. 4, 2022, which application claims priority to United Kingdom Application No. GB2109869.4, filed on Jul. 8, 2021, which applications are each hereby incorporated herein by reference in their entireties.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2022/068469 | 7/4/2022 | WO |
