Embodiments of the present disclosure generally relate to semiconductor processing equipment. More particularly, embodiments of the present disclosure relate to an abatement system and a vacuum processing system for abating compounds produced in semiconductor processes.
The process gases used by semiconductor processing facilities include many compounds, such as perfluorocarbons (PFCs), which must be abated or treated before disposal, due to regulatory requirements and environmental and safety concerns. Typically, a remote plasma source may be coupled to a processing chamber to abate the compounds coming out of the processing chamber. A reagent may be injected into the plasma source to assist the abatement of the compounds.
Conventional abatement technology for abating PFCs utilizes water vapor as a reagent, which provides good destruction removal efficiency (DRE). However, abatement of certain compounds using water vapor in the remote plasma source can result in the formation of solid particles in the remote plasma source and equipment downstream of the remote plasma source, such as exhaust line and pumps. In addition, the exhaust exiting the remote plasma source may be at an elevated temperature, which can cause issues at the pump downstream of the remote plasma source.
Accordingly, what is needed in the art is an improved abatement system for abating compounds produced in semiconductor processes.
Embodiments of the present disclosure relate to an abatement system and a vacuum processing system for abating compounds produced in processes. In one embodiment, an exhaust cooling apparatus includes a body assembly having a first end, a second end, an inlet port and an outlet port, the body assembly having a hollow interior fluidly connecting the inlet port and the outlet port, a first plate disposed in the hollow interior, and a second plate disposed in the hollow interior between the first plate and the outlet port, the second plate having temperature control elements operable to maintain the second plate cooler than the first plate.
In another embodiment, an abatement system includes a first plasma source, an exhaust cooling apparatus coupled to the first plasma source, and a second plasma source coupled to the exhaust cooling apparatus.
In another embodiment, an exhaust cooling apparatus includes a body assembly having a first end, a second end, an inlet port and an outlet port, the body assembly having a hollow interior fluidly connecting the inlet port and the outlet port, a tray disposed in the hollow interior, and a plate disposed in the hollow interior between the tray and the outlet port.
So that the manner in which the above recited features of the present disclosure can be understood in detail, a more particular description of the disclosure, briefly summarized above, may be had by reference to embodiments, some of which are illustrated in the appended drawings. It is to be noted, however, that the appended drawings illustrate only typical embodiments of this disclosure and are therefore not to be considered limiting of its scope, for the disclosure may admit to other equally effective embodiments.
To facilitate understanding, identical reference numerals have been used, where possible, to designate identical elements that are common to the figures. It is contemplated that elements and features of one embodiment may be beneficially incorporated in other embodiments without further recitation.
The vacuum processing chamber 190 has a chamber exhaust port 191 coupled to the plasma source 100 of the abatement system 193 via a foreline 192. The exhaust cooling apparatus 117 is coupled to the plasma source 100 in order to cool the exhaust exiting the plasma source 100 and to collect particles formed in the plasma source 100. The exhaust cooling apparatus 117 is coupled to an exhaust conduit 194 to pumps and facility exhaust, schematically indicated by a single reference numeral 196 in
The plasma source 100 is utilized to perform an abatement process on gases and/or other materials exiting the vacuum processing chamber 190 so that such gases and/or other materials may be converted into a more environmentally and/or process equipment friendly composition. In some embodiments, an abatement reagent source 114 is coupled to the foreline 192 and/or the plasma source 100. The abatement reagent source 114 provides an abatement reagent into the plasma source 100 which may be energized to react with or otherwise assist converting the materials exiting the vacuum processing chamber 190 into a more environmentally and/or process equipment friendly composition. Optionally, a purge gas source 115 may be coupled to the plasma source 100 for reducing deposition on components inside the plasma source 100.
The exhaust cooling apparatus 117 is coupled between the plasma source 100 and the exhaust conduit 194 for reducing the temperature of the exhaust exiting the plasma source 100 and for collecting particles formed in the plasma source 100. In one example, the exhaust cooling apparatus 117 is a part of the abatement system 193. The exhaust exiting the plasma source 100 may deposit on cold surfaces (surfaces having a temperature substantially lower than the temperature of the exhaust) inside of the exhaust cooling apparatus 117. An example of the material deposited in the exhaust cooling apparatus is silicon dioxide. In some embodiments, the vacuum processing chamber 190 includes a remote plasma source for generating cleaning radicals, such as fluorine radicals, that are flowed into the vacuum processing chamber 190 to clean the vacuum processing chamber 190. Unreacted cleaning radicals may exit the vacuum processing chamber 190 and enter the plasma source 100 and the exhaust cooling apparatus 117 to remove materials deposited in the plasma source 100 and the exhaust cooling apparatus 117. In some embodiments, the cleaning process of the vacuum processing chamber 190 is performed efficiently, so a minimum amount of unreacted cleaning radicals may exit the vacuum processing chamber 190. The minimum amount of cleaning radicals is not enough to clean the plasma source 100 and the exhaust cooling apparatus 117.
A second plasma source 102 may be utilized to generate cleaning radicals to clean the plasma source 100 and/or the exhaust cooling apparatus 117. The second plasma source 102 may be coupled to the exhaust cooling apparatus 117 via a conduit 104, as shown in
Optionally, a pressure regulating module 182 may be coupled to at least one of the plasma source 100 or the exhaust conduit 194. The pressure regulating module 182 injects a pressure regulating gas, such as Ar, N, or other suitable gas which allows the pressure within the plasma source 100 to be better controlled, and thereby provide more efficient abatement performance. In one example, the pressure regulating module 182 is a part of the abatement system 193.
A plate 220 is disposed in the body assembly 202 of the exhaust cooling apparatus 117. The plate 220 may be planar or curved. During operation, the plate 220 collects materials, such as silicon dioxide, exiting the plasma source 100 (as shown in
The reaction of the cleaning radicals and the materials collected on the plate 220 may have an increased reaction rate at an elevated temperature, such as the temperature of the exhaust entering the exhaust cooling apparatus 117. Thus, the plate 220 is not cooled. For example, the plate 220 does not include a cooling channel formed therein for a coolant to flow therethrough. In the embodiment depicted in
The reaction of the cleaning radicals and the materials collected on the plate 220 may be exothermic, further contributing to maintaining an elevated temperature of the plate 220. In one embodiment, the temperature of the plate 220 ranges from about 400 degrees Celsius to about 500 degrees Celsius.
A cooling device 222 may be coupled to the second plate 210 to prevent the seal disposed between the second plate 210 and the second end 206 of the body assembly 202 from degrading due to the elevated temperature of the second plate 210. The cooling device 222 may be a tube or passage connected to a coolant source, and a coolant is flowed through the tube to lower the temperature of the second plate 210. A thermal insulator (not shown) may be disposed between the second plate 210 and the plate 220 to prevent cooling of the plate 220 by the cooled second plate 210. A cooling device (not shown) may be coupled to the first plate 208 to prevent the seal disposed between the first plate 208 and the first end 204 from degrading due to the elevated temperature of the first plate 208. Similarly, cooling devices 216, 218 may be coupled to the inlet port 212 and the outlet port 214, respectively, to protect seals in that region of the exhaust cooling apparatus 117. In one example, the cooling device 216 may be a tube including a coolant inlet 228 and a coolant outlet 230. The cooling device 218 may be the same as the cooling device 216. Cooling devices 216, 218 may conform to the shape of the openings of the inlet port 212 and the outlet port 214. In one embodiment, the cooling devices 216, 218 are circular, as shown in
The plate 220 is coupled to the second plate 210, for example via a plurality of bolts 234 or other suitable technique. An optional thermal insulator 240 may be disposed between the second plate 210 and the plate 220 to thermally insulate the plate 220 from the cooled second plate 210. The thermal insulator 240 may be any suitable insulator, such as a ceramic standoff or tube slid over the bolts 234. In one embodiment, the thermal insulator 240 is a ceramic washer. The plate 220 and the cooling plate 231 may be fabricated from the same material. The plate 220 and the cooling plate 231 may each have a length that is less than a length of the body assembly 202 of the exhaust cooling apparatus 117. The length of the body assembly 202 is defined as a length between the first plate 208 and the second plate 210. Because the plate 220 and the cooling plate 231 are coupled to opposite plates 210, 208, and the length of the plate 220 and the cooling plate 231 is less than the length of the body assembly 202, the exhaust entering the exhaust cooling apparatus 117 may flow along a serpentine path P1 defined around the plate 220 and the cooling plate 231. The plate 220 and the cooling plate 231 are offset lengthwise, as shown in
Described differently, the plate 220 may be coupled at a first end to the second plate 210 in a cantilevered manner, while the second end of the plate 220 may be spaced from first plate 208. Similarly, the cooling plate 231 may be coupled at a first end to the first plate 208 in a cantilevered manner, while a second end of the cooling plate 231 may be spaced from the second plate 210. As the opposite ends of the plates 220, 231 are spaced from opposite plates 208, 210, the exhaust entering the exhaust cooling apparatus 117 may flow along a serpentine path P1 defined around the plate 220 and the cooling plate 231. The serpentine path P1 increases the residual time of the exhaust gases passing through the exhaust cooling apparatus 117, thereby increasing the efficiency of particle removal from the exhaust stream. Furthermore, the serpentine path P1 ensures that no particles can fall directly through the outlet port 214 and into the pump. The gaps G1, G2 between opposite ends of the plates 220, 231 and the opposite plates 208, 210 minimize the pressure drop from the inlet port 212 to the outlet port 214. Without the gaps G1, G2, the material deposited on the plate 220 and the cooling plate 231 can quickly block off the gas path and create ever increasing pressure drop across the inlet port 212 to the outlet port 214 until the vacuum pumping becomes inefficient to meet process chamber requirements.
The plate 220 may be further supported by a plurality of stiffeners 250, such as tubes, bars, beams, angles or other elongated profile. The bolts 234, the plate 220 and the plurality of stiffeners 250 may be fabricated from the same material to reduce warpage or separating due to mis-matches in the coefficient of thermal expansions. The plate 220 may be curved, as shown in
The viewing port 224 includes a window 252 and a shutter 256. The window 252 may be fabricated from sapphire and may include a coating that blocks UV radiation. The shutter 256 may be automatically or manually actuated to shield or expose the window 252 from the interior of the exhaust cooling apparatus 117. The shutter 256 is half open for illustration, as shown in
The reaction of the cleaning radicals and the materials collected on the tray 302 may have an increased reaction rate at an elevated temperature, such as the temperature of the exhaust entering the exhaust cooling apparatus 117. Thus, the tray 302 is not cooled. For example, the tray 302 does not include a cooling channel formed therein for a coolant to flow therethrough. In other words, the temperature of the tray 302 is not controlled by a temperature controlling device. The tray 302 substantially takes the temperature of the exhaust entering the exhaust cooling apparatus 117. Alternatively, the tray 302 may be actively heated, for example by resistive heaters. The tray 302 is fabricated from a material having high thermal conductivity. The tray 302 may be fabricated from aluminum or stainless steel, such as 316L stainless steel.
The reaction of the cleaning radicals and the materials collected on the tray 302 may be exothermic. Heat transfer between the tray 302 and second plate 210 may be inhibited utilizing the techniques described above with reference to the heat transfer between the plate 220 and second plate 210.
A cooling device 308 is coupled to the first plate 208 to prevent the seal disposed between the first plate 208 and the first end 204 from degrading due to the elevated temperature of the first plate 208. The cooling device 308 includes a tube 310 connected to a coolant source, and a coolant is flowed through the tube 310 to lower the temperature of the first plate 208. Similarly, a cooling device 304 may be coupled to the second plate 210 to prevent the seal disposed between the second plate 210 and the second end 206 from degrading due to the elevated temperature of the second plate 210. The cooling device 304 may include a tube 306 connected to a coolant source, and a coolant is flowed through the tube 306 to lower the temperature of the second plate 210. A thermal insulator (not shown) may be disposed between the second plate 210 and the tray 302 to reduce the heat transfer between the tray 302 and the cooled second plate 210. Similarly, cooling devices 216, 218 may be coupled to the inlet port 212 and the outlet port 214, respectively.
Described differently, the tray 302 may be coupled at a first end to the second plate 210 in a cantilevered manner, while a second end of the tray 302 may be spaced from first plate 208. Similarly, the cooling plate 231 may be coupled at a first end to the first plate 208 in a cantilevered manner, while a second end of the cooling plate 231 may be spaced from the second plate 210. As the opposite ends of the tray 302 and plate 231 are spaced from opposite plates 208, 210, the exhaust entering the exhaust cooling apparatus 117 may flow along a serpentine P2 path defined around the tray 302 and the cooling plate 231. As noted above, the serpentine path P2 increases the residual time of the exhaust gases passing through the exhaust cooling apparatus 117, thereby increasing the efficiency of particle removal from the exhaust stream.
A liner 324 is coupled to an inside surface of the outlet port 214. The liner 324 may be cylindrical, as shown in
By including a plate, such as the plate 220, or a tray, such as the tray 302, in the exhaust cooling apparatus, reaction rate of the reaction between the materials deposited on the plate or in the tray and cleaning radicals due to the elevated temperature of the plate or the tray is improved. Furthermore, the plate or tray prevents solid materials from flowing through the exhaust cooling apparatus and into the pumps. The solid materials deposited on the plate or collected in the tray are reacted with cleaning radicals to form a gas, which does not cause any damage to downstream components.
While the foregoing is directed to embodiments of the present disclosure, other and further embodiments of the disclosure may be devised without departing from the basic scope thereof, and the scope thereof is determined by the claims that follow.
This application claims priority to U.S. Provisional Patent Application Ser. No. 62/508,930, filed on May 19, 2017, which herein is incorporated by reference.
Number | Name | Date | Kind |
---|---|---|---|
2290323 | Graham | Jul 1942 | A |
2514894 | Naab | Jul 1950 | A |
3081068 | Milleron | Mar 1963 | A |
3719052 | White | Mar 1973 | A |
3892550 | Riis | Jul 1975 | A |
5141714 | Obuchi et al. | Aug 1992 | A |
5211729 | Sherman | May 1993 | A |
5422081 | Miyagi et al. | Jun 1995 | A |
5427610 | Croker | Jun 1995 | A |
5453125 | Krogh | Sep 1995 | A |
5746790 | Niimura et al. | May 1998 | A |
5819683 | Ikeda et al. | Oct 1998 | A |
5904757 | Hayashi et al. | May 1999 | A |
5928426 | Aitchison | Jul 1999 | A |
6015463 | Cox | Jan 2000 | A |
6156107 | Hayashi et al. | Dec 2000 | A |
6238514 | Gu | May 2001 | B1 |
6241793 | Lee et al. | Jun 2001 | B1 |
6488745 | Gu | Dec 2002 | B2 |
6517913 | Cheung | Feb 2003 | B1 |
6528420 | Tong et al. | Mar 2003 | B1 |
6689252 | Shamouilian | Feb 2004 | B1 |
6908499 | Lin | Jun 2005 | B2 |
6966936 | Yamasaki | Nov 2005 | B2 |
7044997 | Mardian et al. | May 2006 | B2 |
7387685 | Carpenter et al. | Jun 2008 | B2 |
7727296 | Tojo et al. | Jun 2010 | B2 |
7867312 | Engerran | Jan 2011 | B2 |
8057564 | Tsuji | Nov 2011 | B2 |
8246705 | Bain et al. | Aug 2012 | B2 |
8915775 | Ikeda et al. | Dec 2014 | B2 |
9057388 | Comeau et al. | Jun 2015 | B2 |
9240308 | Cox et al. | Jan 2016 | B2 |
9669139 | Coulthard et al. | Jun 2017 | B2 |
9896761 | Hara et al. | Feb 2018 | B2 |
10036090 | Komori et al. | Jul 2018 | B2 |
20010003892 | Rikyuu et al. | Jun 2001 | A1 |
20020159924 | Arno et al. | Oct 2002 | A1 |
20070175188 | Tsuji | Aug 2007 | A1 |
20090217634 | Choi | Sep 2009 | A1 |
20100275900 | Bain et al. | Nov 2010 | A1 |
20120258516 | Schultz et al. | Oct 2012 | A1 |
20130284724 | Cox et al. | Oct 2013 | A1 |
20130340681 | Wagner et al. | Dec 2013 | A1 |
20140261702 | Meng | Sep 2014 | A1 |
20140262033 | Herbert et al. | Sep 2014 | A1 |
20150000870 | Hosotani et al. | Jan 2015 | A1 |
20150187562 | Lee et al. | Jul 2015 | A1 |
20150247658 | Cosby, II et al. | Sep 2015 | A1 |
20150252473 | Dickinson | Sep 2015 | A1 |
20150255256 | Cox et al. | Sep 2015 | A1 |
20150357168 | Dickinson | Dec 2015 | A1 |
20160107117 | Raj et al. | Apr 2016 | A1 |
20160133442 | Cox et al. | May 2016 | A1 |
20180166306 | Hou et al. | Jun 2018 | A1 |
20180337027 | L'Heureux et al. | Nov 2018 | A1 |
Number | Date | Country |
---|---|---|
203779727 | Aug 2014 | CN |
104973603 | Oct 2015 | CN |
54154814 | Dec 1979 | JP |
2004063866 | Feb 2004 | JP |
201536114 | Sep 2015 | TW |
201604320 | Feb 2016 | TW |
Entry |
---|
Taiwanese Office Action (with attached English translation) for Application No. 106112166; dated Dec. 24, 2018; 9 total pages. |
PCT International Search Report and Written Opinion dated Jul. 31, 2018, for International Application No. PCT/US2018/029031. |
Number | Date | Country | |
---|---|---|---|
20180337027 A1 | Nov 2018 | US |
Number | Date | Country | |
---|---|---|---|
62508930 | May 2017 | US |