The field of the invention relates to cryopumps.
Cryopumps and in particular two stage cryopumps are configured to provide high vacuums by capturing type I gases such as water vapour at a first stage temperature and type II gases such as nitrogen at a second stage temperature. In some cases they are further configured to cryoadsorb type III gases such as hydrogen.
Where such cryopumps are used to evacuate semiconductor process chambers then it is important that they can store large quantities of type II gasses and are able to recover the chamber pressure between wafers. The longer a pump can perform (store gasses and recover pressure) without needing to be regenerated the more valuable the pump is for its user. The inside volume of a cryopump, the frost temperature and shielding along with how efficiently the frost is formed dictates the amount of gas that can be stored.
Conventional cryopumps have used the same vessel size and internal volume from the 10 or 11K top plate to the 100K sputter plate for many years. Such cryopumps conventionally have an have an 8″ (20 cm) internal diameter frontal opening that corresponds to the opening in the process chamber being evacuated. Over that span of time pumping performance requirements have grown as new processes emerge and longer time between regeneration of the cryopumps are expected. Enhancements have been made to the existing array designs and shielding to increase the capacity of the pump and its vacuum stability.
It would be desirable to further increase the capacity of a cryopump to capture type II gasses and thereby extend the capacity and time between regenerations of such a pump.
The discussion above is merely provided for general background information and is not intended to be used as an aid in determining the scope of the claimed subject matter. The claimed subject matter is not limited to implementations that solve any or all disadvantages noted in the background.
A first aspect provides a cryopump comprising: a vessel comprising a radiation shield having a frontal opening, said frontal opening forming an inlet to said vessel; a frontal array thermally coupled to said radiation shield and mounted across said frontal opening; a cryopanel structure mounted within said vessel; a two stage refrigerator extending into said vessel, a first stage of said refrigerator being thermally coupled to said radiation shield and a colder second stage of said refrigerator being thermally coupled to said cryopanel structure; wherein said vessel comprises an elongate vessel a distance between a surface of said cryopanel structure closest to said frontal opening and a surface of said frontal array closest to said cryopanel structure comprising between 0.6 and 1.2 times the diameter of said frontal opening.
As noted above cryopumps are often used to generate and maintain a vacuum in a semiconductor processing chamber such as in physical vapour deposition processes. In such processing it is important that the vacuum is maintained to a high vacuum level, and that where a wafer is exchanged, this high vacuum is achieved again quickly. Cryopumps are capture pumps and thus, they need periodically to be regenerated. Regeneration of a pump means that during this process the processing chamber cannot be used and thus, it is advantageous if the frequency of the regeneration can be reduced.
The frequency of regeneration is related to the capacity of the pump and the amount of gas molecules that can be captured before the operation of the pump deteriorates. Gas molecules may be captured as frost on the cryopanels and this frost grows up towards the frontal opening. There is a temperature gradient across the length of the frost as it grows and where the frost gets too warm then gas molecules start to escape and this reduces the effectiveness of the pump. Furthermore, where a cryopump is used in the semiconductor processing industry, it is designed to fit into the confined space associated with a semiconductor processing fab and thus, there is a desire to provide a compact pump.
Conventionally cryopumps have been configured to have a frontal opening of 8 inches (20.3 cm) which corresponds to the opening of a semiconductor processing chamber. They are also configured with a length from the base to the frontal opening of about 1.2 times the size of the diameter, that is 24.6 cm (9.7 inches) and a length from the upper surface of the cryopanel structure to the lower surface of the frontal array of less than half the diameter of the frontal opening, around 3.8 inches (9.6 cm).
The inventor found that by elongating the vessel, and in particular increasing the distance between the cryopanel structure and the frontal array, the capacity of the cryopump and in particular the region where frost is stored is increased and yet the capture of the molecules remains effective. Elongating the vessel by increasing this dimension provides additional space in the portion of the vessel that stores the “frost” or captured type II gases. Furthermore, lengthening the distance between the cryopanel structure and the frontal array allows the cryopanel structure to be more remote from the frontal opening and as the frontal opening is a source of radiation this allows the cryopanel structure to maintain a lower temperature and thus, provides improved retention of the frost.
In some embodiments, said distance is between 0.7 and 0.9 times the diameter of said frontal opening.
In other embodiments the distance is between 0.8 and 1.1 times the diameter of the frontal opening.
Although the optimal increase in length does depend on circumstances, the configuration of the pump, including the temperature of the second stage cryopanels and the effectiveness of the radiation shields, and also in some cases on the proposed use of the pump, it has been found in many circumstances that elongating the vessel such that the distance between the cryopanel structure and the frontal array is between 0.7 and 0.9 times the diameter of said frontal opening provides a particularly effective increase in storage capacity without unduly degrading the capture stability of the gas.
In some embodiments, the diameter of the frontal opening is between 20 and 21 cm (7.8 and 8.2 inches) and the distance between said cryopanel structure and said frontal array is between 12 cm and 25 cm (4.7 and 10 inches).
In some embodiments, said second stage of said two stage refrigerator is configured to maintain a temperature of said cryopanels to below 9K.
As noted above the storage capacity of a cryopump may be increased by increasing the volume available to store the frost. However, as the frost grows towards the frontal opening, there is a temperature gradient across the frost and elongating this distance makes maintaining the portion of the frost closest to the frontal opening at a low temperature increasingly difficult. When the frost reaches a certain temperature then gas molecules will start to escape and the efficacity of the pump will deteriorate. Providing a cryopanel structure of a lower temperature enables the frost length to increase, while the temperature of the surface remote from the cryopanels remains low enough to securely hold the gas molecules.
In some embodiments, said frontal array comprises a disk element and an annular element, said disk element and said annular element being mounted axially displaced from each other said annular element being mounted to be closer to said frontal opening than said disk element, a diameter of said disk element being equal to or greater than a diameter of the aperture in said annular element and smaller than an outer diameter of said annular element, said outer diameter of said annular element being equal to or greater than a diameter of said frontal opening.
A further way of maintaining a low temperature within the vessel and protecting the increased volume of frost from radiation is to improve the effectiveness of the frontal array. Providing a frontal array with longitudinally displaced elements allows the channels into the vessel to be in the axial plane and not the radial plane. This avoids or at least impedes any line of sight channels into the vessel and thereby protects the vessel from external radiation, allowing the upper surface of the frost to maintain a lower temperature.
In some embodiments, said frontal array comprises a further axially extending cylindrically-shaped element, said cylindrically-shaped element connecting said disk element and annular element, said cylindrically-shaped element comprising a cylindrical surface, said cylindrical surface comprising a plurality of apertures.
A further aspect provides a cryopump comprising: a vessel comprising a radiation shield having a frontal opening, said frontal opening forming an inlet to said vessel; a frontal array thermally coupled to said radiation shield and mounted across said frontal opening; a cryopanel structure mounted within said vessel; a two stage refrigerator extending into said vessel, a first stage of said refrigerator being thermally coupled to said radiation shield and a colder second stage of said refrigerator being thermally coupled to said cryopanel structure, said second stage of said refrigerator being configured to maintain a temperature of said cryopanel structure to below below 9K.
A yet further aspect provides a cryopump comprising: a vessel comprising a radiation shield having a frontal opening, said frontal opening forming an inlet to said vessel; a frontal array thermally coupled to said radiation shield and mounted across said frontal opening; a cryopanel structure mounted within said vessel; a two stage refrigerator extending into said vessel, a first stage of said refrigerator being thermally coupled to said radiation shield and a colder second stage of said refrigerator being thermally coupled to said cryopanel structure; wherein said frontal array comprises a disk element and an annular element, said disk element and said annular element being mounted axially displaced from each other said annular element being mounted to be closer to said frontal opening than said disk element, a diameter of said disk element being equal to or greater than a diameter of the aperture in said annular element and smaller than an outer diameter of said annular element, said outer diameter of said annular element being equal to or greater than a diameter of said frontal opening.
In some embodiments, said frontal array comprises an axially extending cylindrically-shaped element, said cylindrically-shaped element connecting said disk element and annular element said cylindrically-shaped element comprising a cylindrical surface, said cylindrical surface comprising a plurality of apertures.
Further particular and preferred aspects are set out in the accompanying independent and dependent claims. Features of the dependent claims may be combined with features of the independent claims as appropriate, and in combinations other than those explicitly set out in the claims.
Where an apparatus feature is described as being operable to provide a function, it will be appreciated that this includes an apparatus feature which provides that function or which is adapted or configured to provide that function.
The summary is provided to introduce a selection of concepts in a simplified form that are further described in the detailed description. This summary is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used as an aid in determining the scope of the claimed subject matter.
Embodiments of the present invention will now be described further, with reference to the accompanying drawings, in which:
Before discussing the embodiments in any more detail, first an overview will be provided.
Cryopumps and in particular, PVD (physical vapour deposition) process cryopumps store large quantities of type II gasses and are required to recover the chamber pressure between wafers. The longer a pump can perform (store gasses and recover pressure) without needing to be regenerated the more valuable the pump is for its user. Enhancements have been made to the conventional array designs and shielding to increase the capacity of the pump and its vacuum stability. These improvements have enabled the usable physical volume available for frost within the pump below the sputter plate to be enhanced. Although these enhancements have had some success in helping to better utilize the volume available to store the gasses they have not been able to significantly increase the litres of gas it can store. To further increase the volume of a pump with a conventional flange size, it is proposed to elongate the pump such that an extra volumetric capacity further from the frontal opening is provided. In some embodiments, to further improve gas storage capacity better radiation shielding is provided and/or a lower temperature second stage cryopanel.
In effect, the inside volume of a cryopump, the frost temperature and shielding plus how efficiently the frost is formed dictates the amount of gas that can be stored. If the pump's useful gas volume is increased by lengthening the vessel and cylindrical radiation shield then the capacity may be increased. In particular, if the lengthening is performed in conjunction with an improved shielded sputter plate and/or with a refrigerator unit with lower 2nd stage temperature then an increased storage capacity of up to 50% is possible. Increasing the volume of the cryopump is important to allow a significant increase in its capacity for storing type II gasses. To conclude an elongated cryopump improves capacity, and does so particularly effectively when configured with better shielding and/or lower 2nd stage cryopanel temperatures.
In the conventional cryopump shown schematically and not to scale in the left-hand figure the distance between the cryopanel structure and the frontal array is about half the diameter 42 of the frontal opening. In embodiments the vessel is elongated so that this distance is increased to about 0.6 to 1.2 times the diameter, preferably between 0.7 and 0.9 times.
The cryopump comprises a radiation shield 12 that surrounds the region A where frost is stored. The radiation shield extends above the flange 15 by between 0.6 and 1″ (1.5 to 2.5 cm) to isolate the cryopump from the vacuum vessel.
The capacity to capture gas and still recover pressure afterwards of the cryopump according to the embodiment is increased by making the vessel 10 and radiation shield 12 longer with more length/volume inside radiation shield 12. In this embodiment the cryopump also has an improved frontal array plate 20 across the frontal opening 22.
The cryopump also has a reduced temperature of the second stage refrigerator that cools the cryopanel structure 30. This reduced temperature helps lower the frost temperature at the cryopanel structure and correspondingly along the frost cylinder and thereby compensates to some extent the effect of the increased frost length on the upper surface temperature of the frost.
Allowing the frost to grow and form a longer cylinder makes keeping the upper surface of the frost at a low enough temperature to inhibit gas molecules escaping more difficult. Decreasing the inlet radiant heat load by improving the shielding performed by the frontal array and/or decreasing the temperature of the cryopanel structure and thus, the temperature of the base of the frost cylinder may each help in keeping the temperature of the upper surface of the frost cylinder at a lower temperature. Where the refrigerator's 2nd stage temperature is lowered below 10K preferably below 9K then this helps avoid or at least reduce the escape of gas molecules.
A conventional frontal array plate 50 with holes in the form of louvers blocks most radiation but still allows some line of sight preferential pumping to occur. When the gas is being pumped it forms a crystal-like vertical structure that looks to be more like threads than an accumulation of frost layered horizontally. These crystal “rods” start growth on the cold ˜10K cryopanel like millions of threads attached to the cryopanel and stretching up to the 100K sputter plate or anything not at or below ˜25K. Type II gas also pumps below the 10K cryopanel and forms on the lower panels and charcoal arrays but in limited quantities.
Increasing the length of the available volume for gasses to accumulate, decreasing the 2nd stage cryopanel temperature, and allowing less radiation/preferential pumping of gasses will increase the volume that can be stored. Furthermore, doing so by elongating the vessel is less expensive that would be the case were a larger vessel with a larger flange size manufactured, it is also easily manufactured.
The length of the extension may be from 1″ up to 6″ (2.5 to 15 cm).
The shielding by the improved frontal array and/or the lower 2nd stage temperature although particularly useful in this embodiment are also applicable for use in other cryopumps.
Although illustrative embodiments of the invention have been disclosed in detail herein, with reference to the accompanying drawings, it is understood that the invention is not limited to the precise embodiment and that various changes and modifications can be effected therein by one skilled in the art without departing from the scope of the invention as defined by the appended claims and their equivalents.
Although elements have been shown or described as separate embodiments above, portions of each embodiment may be combined with all or part of other embodiments described above.
Although the subject matter has been described in language specific to structural features and/or methodological acts, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are described as example forms of implementing the claims.
Number | Date | Country | Kind |
---|---|---|---|
2117699.5 | Dec 2021 | GB | national |
This application is a Section 371 National Stage Application of International Application No. PCT/IB2022/061581 filed Nov. 30, 2022, and published as WO 2023/105349 A1 on Jun. 15, 2023, the content of which is hereby incorporated by reference in its entirety and which claims priority of British Application No. 2117699.5, filed Dec. 8, 2021.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/IB2022/061581 | 11/30/2022 | WO |