Patent Grant
10968915
The present application is a national stage application under 35 U.S.C. § 371 of International Patent Application WO 2011/092674 filed on Feb. 1, 2011. The present application claims priority under 35 U.S.C. § 119 and 35 U.S.C. § 365 from International Patent Application WO 2011/092674; the present application also claims priority under from 35 U.S.C. § 119 from Italian Patent Application TO2010A000070 filed on Feb. 1, 2010. The entire disclosures of the referenced International Patent Application and the referenced Italian Patent Application are specifically incorporated herein by reference.
The present teachings relate to a vacuum pump, and more particularly, a high-vacuum pump comprising one or more elements made of plastic material, and intended to obtain high vacuum degrees.
Many different kinds of vacuum pumps are known in the art and are used according to the vacuum degree to be obtained.
For example, turbomolecular pumps are widely used for obtaining very high vacuum degrees, up to 10−8 Pa.
These turbomolecular pumps generally comprise a vacuum-tight casing that has an inlet or suction port, an outlet or discharge port, and a plurality of pumping stages arranged between the suction and discharge ports.
Each pumping stage includes a stator stage, comprising a stationary ring-shaped stator element, and a rotor stage, comprising a rotating disc-shaped rotor element, mounted integral with a rotating shaft and optionally equipped with peripheral vanes.
When the rotating shaft and the rotor elements mounted integral therewith are made to rotate at high speed (typically exceeding 10,000 rpm and even up to 100,000 rpm), gas pumping from the suction port to the discharge port is obtained based on cooperation of the rotor elements with the stator elements.
Turbomolecular pumps are often associated, at the high pressure side, with a molecular drag vacuum pump.
A molecular drag vacuum pump generally comprises a vacuum-tight casing comprising an inlet or suction port, an outlet or discharge port and a plurality of pumping stages arranged between the suction and discharge ports.
The pumping stages produce pumping action by momentum transfer from a fast-moving surface (moving at speed comparable to thermal speed of the molecules) directly to gas molecules. Generally, the pumping stages comprise a rotor element and a stator element cooperating with each other and defining a pumping channel therebetween: collisions of gas molecules in the pumping channel with the rotor element rotating at a very high speed cause gas in the channel to be pumped, from the inlet to the outlet of the channel itself.
Generally, according to the prior art, the rotor elements and the stator elements in high-vacuum pumps, and especially in turbomolecular and molecular drag vacuum pumps, are made of aluminium alloys. The limited specific weight and good mechanical strength of certain aluminium alloys enable high rotation speeds to be attained.
Recently, fibre-reinforced plastics (FRP), have been considered and evaluated for making rotor elements and other parts.
Generally, such solutions aim to attain a structural strength that is considerably higher than that of aluminum and its alloys and reduced weights, which enable higher peripheral speeds to be attained for the rotor elements, which in turn, increases the pumping speed of the vacuum pump. This is especially important for large pumps, where the maximum rotation speed of the rotor elements may be limited by the structural strength of the material.
The solutions concern the manufacture of disc-shaped rotor elements for turbomolecular pumps by using thermosetting resins reinforced with long fibres, such as carbon fibres, glass fibres, aramidic fibres and the like.
In order to increase the structural strength of the rotor element, such solutions use long reinforcing fibres all oriented in the maximum stress direction, for instance, the circumferential direction.
Such known solutions, appear very encouraging at theoretical level, but are difficult to put into practice, due to very high production costs. First, the need to obtain high structural strengths limits the degrees of freedom in the choice of the materials to be used. Second, the need to arrange the reinforcing fibres along one or more predetermined directions considerably increases the complexity of the production process and the costs related thereto.
In view of the above, there is a need for a high-vacuum pump, that uses plastic materials and that has lower production costs and reduced weight.
According to embodiments of the present teachings, use of plastic material in place of aluminium or other similar metals is aimed at reducing the production costs.
Thanks to the use of thermoplastic or thermosetting resins, possibly reinforced with short fibres, it is possible to make elements for the vacuum pump according to the embodiments of the present teachings by injection moulding, thus obtaining a production cost that is limited and competitive with respect to the conventional rotor elements made of aluminium.
Indeed, the short fibres used as reinforcement are randomly oriented in the matrix of the plastic material which eliminates the need to arrange the fibres along a preferential direction and allows employing the injection moulding technique in the production process. Even if using short fibres instead of long fibres gives a lower structural rigidity, experimental tests have shown that elements made from resins reinforced with short fibres have a structural strength slightly lower than, but anyway of the same order of magnitude as that of similar elements made of aluminium alloys.
Moreover, if the specific mechanical strength, that is the ratio between tensile breaking stress and specific weight, is considered, elements made from resins reinforced with short fibres have performance quite similar to that of similar elements made of aluminium alloys.
According to one embodiment, the vacuum pump includes at least one rotor element made of plastic material reinforced with short fibres.
According to another embodiment, the vacuum pump includes at least one stator element made of plastic material reinforced with short fibres.
According to another embodiment, the vacuum pump includes at least one turbomolecular rotor or stator element made of plastic material reinforced with short fibres.
According to another embodiment, the vacuum pump includes at least one molecular drag rotor or stator element made of plastic material reinforced with short fibres.
Typically, the plastic material used for the elements of the vacuum pump includes a thermoplastic resin, and such as a semi-crystalline polymer.
Preferably, the short fibres used for the elements of the vacuum pump include carbon or graphite short fibres, glass short fibres or aramidic short fibres.
The embodiments of the present teachings are especially suitable for manufacturing small-size or medium-size vacuum pumps (up to pumping speeds of the order of 700 l/s) and may provide for considerable reduction in the production costs when compared to the conventional solutions.
Further features and advantages of the teachings will become apparent from the following detailed description of embodiments of the teachings, given by way of non-limiting example with reference to the accompanying drawings, in which:
Referring to
The high-vacuum pump 101 includes a vacuum-tight casing 103 mounted on a base 105, in which an electric motor 107 is housed. A suction port 109 and a discharge port 111 are defined in casing 103. Inside casing 103, a plurality of turbomolecular pumping stages (“pumping stages”) 113, 213 are provided between the suction port 109 and the discharge port 111. More particularly, from the suction port 109 to the discharge port 111 a first plurality of turbomolecular pumping stages 113 and a second plurality of pumping stages 213 can be identified, the pumping stages 213 being provided downstream from the turbomolecular pumping stages 113.
In detail, each turbomolecular pumping stage 113 comprises at least; one stationary ring-shaped stator element 113a, fastened to casing 103; one disc-shaped rotor element 113b, mounted integral with a central rotating shaft 115 made to rotate at high speed, (higher than 10,000 rpm and up to 100,000 rpm) by electric motor 107; wherein the ring-shaped stator element 113a and the one disc-shaped rotor element 113b mutually cooperate for exerting a pumping effect on gas passing through turbomolecular pumping stage 113.
In detail, each pumping stage 213 comprises at least: one stationary stator element 213a, fastened to casing 103; one rotor element 213b, mounted integral with a central rotating shaft 115 made to rotate at high speed (higher than 10,000 rpm and up to 100,000 rpm) by electric motor 107; wherein the stator element 213a and the rotor element 213b mutually cooperate for exerting a pumping effect on gas passing through turbomolecular pumping stage 113.
According to embodiments of the present teachings, the vacuum pump comprises a plurality of pumping stages arranged between a suction port and a discharge port. Each the pumping stage comprises a plurality of elements mutually cooperating for pumping gas passing through the pumping stage, the elements comprising at least one stationary stator element and at least one rotating rotor element cooperating with each other, wherein at least one of the elements of at least one of the pumping stages is made of a plastic material charged with reinforcing short fibres.
Preferably, the plastic material is a thermoplastic resin or a thermosetting resin.
More preferably, the plastic material is a semi-crystalline polymer, and further more preferably, an aromatic semi-crystalline polymer.
Preferably, the reinforcing short fibres are randomly oriented in the matrix of plastic material.
Preferably, the reinforcing short fibres are carbon or graphite short fibres, glass short fibres or aramidic short fibres.
Preferably, the short fibre charge in the plastic material is in the range 10% to 50% in weight of the material, and more preferably in the range 30% to 40% in weight of the material.
Note that, in this context: the term “thermoplastic resin” denotes a polymer passing from the solid state to the viscous state when the temperature increases, and back from the viscous state to the solid state when the temperature decreases, so that it can be repeatedly worked and moulded; term “thermosetting resin” denotes a polymer the rigidity of which increases in irreversible manner when the temperature increases, so that it cannot be molten again without undergoing a degradation; the term “semi-crystalline polymer” denotes a polymer of which the chains, by folding, are capable of regularly arranging longer or shorter sections thereof side by side, thereby forming regular crystalline regions; the term “aromatic semi-crystalline polymer” denotes a semi-crystalline polymer comprising aromatic groups; the term “short fibres” denotes fibres the size of which is negligible with respect to the size of the matrix of plastic material into which the fibres are introduced; in particular, the short fibres generally have a size shorter than 10 mm and, preferably, shorter than 1 mm.
Since the short fibres have a negligible size with respect to the element made of plastic material, they are not oriented in a preferential direction, but are dispersed in a chaotic and substantially random manner inside the matrix of plastic material.
Advantageously, the elements of the vacuum pump made in accordance with the present teachings can be produced starting from a mixture of plastic material in a viscous state, charged with short fibres, by means of the injection moulding process.
The possibility of using such a process allows considerably limiting the production costs of the elements if compared to similar elements made of aluminium alloys, which conventionally are obtained, by mechanical machining or electrical discharge machining.
Such a process, on the contrary could not be used for manufacturing similar elements made of plastic materials reinforced with long fibres, which have to be arranged all along a preferential direction; in this case complex operations for correctly arranging the fibres are necessary and, in case of thermosetting materials, expensive processes to be performed in an autoclave are also required.
It is to be appreciated, that such an embodiment is not at all limiting, and that it is possible to provide a vacuum pump in which, for instance, at least the stator element of at least one turbomolecular pumping stage of the vacuum pump is made of plastic material charged with short fibres, without thereby departing from the scope of the present invention.
Referring to
It will be clear for the skilled in the art that rotor element 1 could even be smooth, without vanes, or could, have vanes with a different geometry.
Preferably, as shown in
In this respect, it is to be appreciated that experimental tests have shown that the stresses a turbomolecular rotor element undergoes are mainly circumferential stresses in the more central portion of the disc and substantially radial stresses in the portion where the vanes are present.
The chaotic and substantially random distribution of the short, fibres advantageously allows providing a good resistance to both the stresses at the disc center and the stresses at the disc periphery, even if the stresses are differently oriented: this should not be possible if long fibres, arranged along a single preferential direction, were used. It would, typically involve complex and expensive systems for joining parts having fibres that are differently oriented, in order to cope with the differently oriented stresses.
Turbomolecular rotor element 1 is entirely made of plastic material charged with short fibres.
In particular, VICTREX® PEEK (polyether ether ketone) material marketed by company Victrex plc, Thornton Cleveleys, Lancashire, UK or TORLON® material marketed by company Solvay Advanced Materials L.L.C., Alpharetta, Ga., USA, suitably charged with carbon short fibres in an amount of 30%-40%, exhibited performance that is particularly encouraging for making rotor elements such as rotor element 1 and is also compatible with the high-vacuum environment in which such materials are to operate.
In this respect, hereinafter a table is included in which some of the main characteristics of PEEK charged with 30% of carbon short fibres are compared with those of aluminum.
In particular, in the table below there are reported: the specific weight (PS); the tensile breaking stress (S); the specific mechanical strength (RMS=S/PS); the thermal emissivity (EMT).
By analysing the above table, the skilled in the art will immediately deduce that: using PEEK allows obtaining much lighter elements than when using aluminium; the tensile breaking stress of PEEK is lower than that of aluminium, but anyway of the same order of magnitude; the ratio of the structural strength to the specific weight of PEEK is substantially the same as that of aluminium; the polar moment of inertia of a rotor made of PEEK is lower than that of aluminium, what which allows reducing the ramp time in the transient phase; the thermal emissivity of PEEK is considerably higher than that of aluminium, what which sensibly increases thermal efficiency, taking into account that heat exchanges inside a vacuum pump mainly take place by radiation.
By exploiting the injection moulding process, the production cost of a rotor element of PEEK is considerably lower than that of a rotor element of aluminium formed by mechanical machining or electrical discharge machining.
Moreover, use of a plastic material such as PEEK allows sensibly increasing the corrosion resistance with respect to an element made of aluminium.
Turning now to
In
Rotor elements 13 are mounted on base 15 of the turbomolecular vacuum pump 11 with the interposition of a bottom plate 17 containing the dowels for balancing the rotor.
The rotor elements 13 are fitted onto rotating shaft 19 of turbomolecular vacuum pump 11, which passes through the central through-holes formed in the elements and are stacked on one another to form the vacuum pump rotor.
The stack of rotor elements 13 is then axially compressed by screwing a nut 21 on the top end of shaft 19, which is threaded for that purpose.
A top plate 23 containing the dowels for balancing the rotor is interposed between the uppermost rotor element 13 and nut 21.
In a small pump like that shown in
In an alternative embodiment with respect to what is shown in
In this respect, it is to be noted that a rotor made of plastic materials reinforced with long fibres could not be manufactured as a monolithic piece by injection moulding, since the long fibres have to be arranged all along a preferential direction.
On the contrary, as in the rotor elements according to representative embodiments described below in which the short fibres are arranged in a chaotic and substantially random way, the manufacturing of a rotor comprising a plurality of rotor elements as a single, monolithic piece is allowed, thus permitting to manufacture a rotor in a very inexpensive process.
With reference now to
It is to be appreciated that such an embodiment is not at all limiting, and that it is possible to provide a vacuum pump in which, for instance, at least the stator element of at least one molecular pumping stage of the vacuum pump is made of plastic material charged, with short fibres.
Referring to
Preferably, the rotor element 33 comprises a rotor body having at least one spiral channel on a first surface and at least one further spiral channel on its opposite surface, each of the rotor surfaces cooperating with the smooth surface of a respective stator element for obtaining two different pumping stages, wherein in the spiral channels of the first surface of the rotor element 33 the gas flows in a first direction (i.e., centripetal or centrifugal) while in the spiral channels of the second surface of the rotor element 33 the gas flows in a second, direction opposite to the first direction (i.e., centrifugal or centripetal)
Advantageously, in the illustrated embodiment the cross-sectional area of the spiral channels is reduced from the center to the outer periphery of the rotor body irrespective of whether the gas flows through the channel in a centripetal or centrifugal direction. In such manner, the product of the channel cross-sectional area and the rotor velocity normal to the aforesaid area (i.e. the internal gas flow velocity) can be advantageously maintained constant.
It is to be appreciated, that such an embodiment is not at all limiting and that a different geometric configuration for the rotor spiral channels can alternatively be chosen.
Moreover, other different kinds of molecular pumping stages, such as for instance a conventional Siegbahn pumping stage.
Turning now to
In the rotor 31, all rotor elements 13 are of the kind shown in
The rotor elements 13 and rotor elements 33 are fitted onto the rotating shaft (not shown) of a vacuum pump, which passes through the central through-holes formed in the rotor elements and rotor elements and are stacked on one another to form the vacuum pump rotor 31.
As shown in
In an alternative embodiment with respect to what is shown in
It is also clear that the preceding detailed description is in no way limiting and that several changes and modifications are possible without departing from the scope of the present teachings, as defined in the appended claims.
In particular, even if in the illustrated embodiments reference has been made to one or more turbomolecular rotor elements and/or molecular drag rotor elements made of plastic material reinforced with short fibres, it is possible to envisage that the vacuum pump comprises in alternative, or in addition to, the turbomolecular rotor elements and/or molecular drag rotor elements one or more turbomolecular stator elements and/or molecular drag stator elements made of plastic material reinforced with short fibres, or even of non-reinforced plastic material given the lower stress the stator is subjected to.
| Number | Date | Country | Kind |
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| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/IB2011/050434 | 2/1/2011 | WO | 00 | 10/22/2012 |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2011/092674 | 8/4/2011 | WO | A |
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| Number | Date | Country | |
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| 20130045094 A1 | Feb 2013 | US |
