In a high temperature fuel cell system, such as a solid oxide fuel cell (SOFC) system, an oxidizing flow is passed through the cathode side of the fuel cell while a fuel flow is passed through the anode side of the fuel cell. The oxidizing flow is typically air, while the fuel flow can be a hydrocarbon fuel, such as methane, natural gas, pentane, ethanol, or methanol. The fuel cell, operating at a typical temperature between 750° C. and 950° C., enables the transport of negatively charged oxygen ions from the cathode flow stream to the anode flow stream, where the ion combines with either free hydrogen or hydrogen in a hydrocarbon molecule to form water vapor and/or with carbon monoxide to form carbon dioxide. The excess electrons from the negatively charged ion are routed back to the cathode side of the fuel cell through an electrical circuit completed between anode and cathode, resulting in an electrical current flow through the circuit.
In order to optimize the operation of SOFCs, the oxidizing and fuel flows should be precisely regulated. Therefore, the flow regulating structures, such as interconnects in the fuel cell system should be precisely manufactured. One type of interconnect currently used is a metal interconnect formed by a powder metallurgy technique. The metal interconnect is typically a chromium-based alloy.
Embodiments include an interconnect for a fuel cell stack that includes a first support frame having a first surface that is configured to be secured to a first surface of a first fuel cell in the stack, the first support frame having a coefficient of thermal expansion (CTE) that substantially matches a CTE of an electrolyte material of the first fuel cell, and a gas flow separator section that is secured to a second surface of the first support frame, opposite the first surface of the first support frame, where the gas flow separator section has a CTE that does not substantially match the CTE of an electrolyte material of the first fuel cell. In various embodiments, the interconnect further includes a second support frame having a first surface that is configured to be secured to a second surface of a second fuel cell, opposite the first surface of the first fuel cell, the second support frame having a coefficient of thermal expansion (CTE) that substantially matches a CTE of an electrolyte material of the second fuel cell. The second support frame may have a second surface, opposite the first surface, that is configured to contact a surface of the gas flow separator section.
Further embodiments include a fuel cell stack that includes a plurality of fuel cells each having an anode-side and a cathode-side and an electrolyte material having a first coefficient of thermal expansion (CTE), and a plurality of interconnects, wherein each interconnect comprises an anode support frame attached directly or indirectly to the anode-side of a first one of a plurality of fuel cells, a cathode support frame attached to the cathode-side of a second one of the plurality of fuel cells, where the anode support frame and the cathode support frame are formed of a material having a CTE that substantially matches the CTE of the electrolyte material of the first and second fuel cells, and a gas flow separator section provided between the anode support frame and the cathode support frame, the gas flow separator section being formed of a material having a CTE that does not substantially match the CTE of the electrolyte material of the fuel cells.
Further embodiments include a fuel cell system that includes a plurality of fuel cell stacks arranged in a substantially cylindrical configuration, wherein each fuel cell stack comprises a plurality of fuel cells, and a plurality of interconnects between the fuel cells, wherein the stacks have an asymmetric cross-sectional shape perpendicular to an axis of the stack having a width dimension that increases from an initial width at or proximate to a first inner edge to a second maximum width at a position that is closer to a second outer edge than to the first inner edge.
Further embodiments include a method of fabricating a fuel cell stack that includes attaching an anode support frame to an anode-side of a fuel cell, attaching a cathode support frame to a cathode-side of the fuel cell, the anode support frame and the cathode support frame being formed of a material having a CTE that substantially matches a CTE of an electrolyte material of the fuel cell, and attaching a first gas flow separator section to one of the anode support frame and the cathode support frame, wherein the gas flow separator section is formed of a material having a CTE that does not substantially match the CTE of the electrolyte material of the fuel cell.
Further embodiments include a method of using a fuel cell stack that includes flowing a fuel in a fuel inlet flow channel defined by inlet openings formed in a plurality of stacked metal sheets, flowing the fuel into an inlet fuel plenum formed between surfaces of adjacent metal sheets, and flowing the fuel from the inlet fuel plenum through an anode support frame to a fuel flow field, the anode support frame having a first surface that is secured to an anode-side of a fuel cell and a second surface that is secured to an anode-facing surface of a metal sheet, the anode-facing surface of the metal sheet including a ridged portion that contacts the anode-side of the fuel cell to define the fuel flow field.
The accompanying drawings, which are incorporated herein and constitute part of this specification, illustrate example embodiments of the invention, and together with the general description given above and the detailed description given below, serve to explain the features of the invention.
The various embodiments will be described in detail with reference to the accompanying drawings. Wherever possible, the same reference numbers will be used throughout the drawings to refer to the same or like parts. References made to particular examples and implementations are for illustrative purposes, and are not intended to limit the scope of the invention or the claims.
Various embodiments include interconnects for a fuel cell stack, fuel cell stacks and systems incorporating such interconnects, and methods of fabricating interconnects for a fuel cell stack.
For solid oxide fuel cell stacks, the currently-used interconnects are typically made from an electrically conductive metal material, and may comprise a chromium alloy, such as a Cr—Fe alloy. The interconnects are typically fabricated using a powder metallurgy technique that includes pressing and sintering a Cr—Fe powder, which may be a mixture of Cr and Fe powders and/or pre-alloyed Cr—Fe powder, to form a Cr—Fe alloy interconnect in a desired size and shape (e.g., a “net shape” or “near net shape” process). A typical chromium-alloy interconnect comprises more than about 90% chromium, such as about 95% chromium. The interconnect may also contain less than about 10% iron, such as about 4-5% iron, may contain less than about 2%, such as about zero to 1%, of other materials, such as yttrium or yttria, as well as residual or unavoidable impurities.
The currently-used interconnects are typically formed as a unitary structure. When incorporated into a fuel cell stack, the interconnect is positioned between two adjacent fuel cells in the stack. The anode-side of the interconnect is secured to the anode-side of a first adjacent fuel cell via a seal. The cathode-side of the interconnect is secured to the cathode-side of the second adjacent fuel cell via another seal. The fuel cell stack may be internally manifolded for fuel and externally manifolded for air. In some cases, the stack may be internally manifolded for both fuel and air. When the stack is internally manifolded for fuel and/or air, riser channel openings are formed through the fuel cells and/or the interconnects in the stack to allow the fuel and/or air to travel through the stack to each of the fuel cells.
A primary reason why chromium-based materials are used for interconnects in fuel cell stacks is that chromium-based materials exhibit a good coefficient of thermal expansion (CTE) match with the materials, such as yttria stabilized zirconia (YSZ) and/or scandia stabilized zirconia (SSZ), commonly utilized as the electrolyte of the fuel cells. However, chromium is a relatively brittle material and processing of this material using net-shape or near-net-shape powder metallurgy techniques is very challenging and expensive. Some processes require the use of 1600+ ton presses to form the pressed powder interconnects, as well as sintering of the interconnects in a high-temperature furnace (e.g., 1350 to 1450° C.) in a hydrogen environment to produce the finished parts. In addition, chromium is a relatively expensive material, and the commercially available chromium powders are difficult to press using current powder-metallurgy techniques.
In one embodiment of the invention, the interconnect is made from multiple separate parts that may be made by methods which are less expensive and/or complex than powder metallurgy, such as metal sheet stamping, machining, etc.
Referring to
As shown in
The anode support frame 102 and the cathode support frame 104 may be formed of a material having a coefficient of thermal expansion (CTE) that substantially matches a CTE of the fuel cell 120, and in particular a CTE of an electrolyte material of the electrolyte-supported fuel cell 120. In various embodiments, the anode support frame 102 and/or the cathode support frame 104 may have a CTE that is within about 1%, such as within 0.5%, and preferably within 0-0.1% of the CTE of an electrolyte material for the fuel cell. The fuel cell 120 may be a solid oxide fuel cell having a ceramic electrolyte material, which may be a stabilized zirconia, such as scandia stabilized ziconia (SSZ) and/or yttria stabilized zirconia (YSZ). Alternatively, the electrolyte may comprise another ionically conductive material, such as a doped ceria. In some embodiments, the CTE of the anode support frame 102 and/or the cathode support frame 104 may be between about 9.53×10−6/° C. and 9.71×10−6/° C., such as 9.57-9.67×10−6/° C., and preferably about 9.62×10−6/° C., to match the 9.62×10−6/° C. CTE of SSZ. Alternatively, the CTE of the support frame(s) 102, 104 can be between about 10.4-10.6×10−6/° C., such as about 10.5×10−6/° C., to match the 10.5×10−6/° C. CTE of YSZ. For anode supported cells, the CTE of the frames may be selected to match the anode CTE.
In embodiments, one or both of the anode support frame 102 and the cathode support frame 104 may formed of a chromium-based alloy, such as a chromium-iron alloy that may contain at least about 80% chromium, such as more than about 90% chromium (e.g., about 93-97% chromium), and less than about 20% iron, such as less than about 10% iron (e.g., 4-6% iron). The material of the support frame 102, 104 may further include 0% to about 2% of one or more other materials, such as yttrium or ytrria, as well as unavoidable impurities. Any other suitable materials may be used which have a CTE match to the cell electrolyte. The anode support frame 102 and the cathode support frame 104 may be formed by a suitable fabrication process, such as stamping, machining, or via a powder metallurgy technique. In embodiments, the anode support frame 102 and/or the cathode support frame 104 can have a thickness of between about 0.1 to about 10 mm, such as 0.5 to 5 mm (e.g., 0.5 to 2 mm, such as about 1 mm).
The anode support frame 102 has a second surface 130 adapted to be secured to the anode-facing major surface 112 of the gas flow separator section 106. A sealant material (not illustrated) may be provided between the second surface 130 of the anode support frame 102 and the anode-facing major surface 112 of the gas flow separator section 106. In various embodiments and as described in further detail below, the CTE of the cell electrolyte and anode support frame 102 may not match the CTE of the gas flow separator section 106 (e.g., the CTE may differ by 10% or more, such as 15-20%). When the anode support frame 102 is secured between the anode-side 118 of the fuel cell 120 and the anode-facing surface 112 of the gas flow separator section 106, the ridged portion 108 of the anode-facing major surface 112 of the gas flow separator section 106 contacts directly or indirectly against the anode-side 118 of the fuel cell 120 to define a fuel gas flow field. As shown in
The cathode support frame 104 has a second surface 136 adapted to contact a cathode-facing major surface 114 of a gas flow separator section 106. The second surface 136 of the cathode support frame 102 may contact a cathode-facing major surface 114 of a gas flow separator section 106 that is different than the gas flow separator section 106 to which the anode support frame 102 is secured. As shown in
As described above, the gas flow separator section 106 may be comprised of multiple components. A first component, which in preferred embodiments comprises a shaped metal sheet 140, includes the ridged portion 108 on an anode-facing major surface 112. A second component, which in preferred embodiments also comprises a shaped metal sheet 144, includes the ridged portion 110 on a cathode-facing major surface 114. The ridged portions 108, 110 may comprise a plurality of ribs separating fuel or oxidizer flow channels in the respective flow field. The shaped metal sheets 140, 144 may be relatively thin sheets, and each sheet may have a thickness of less than about 10 mm, such as less than about 5 mm, and may preferably have a thickness that is less than about 2 mm, such as about 1 mm or less. The sheets may be formed into a desired shape using a sheet metal stamping technique. The sheets 140, 144 may be made of any metal or alloy which can withstand the 750-950° C. stack operating temperatures, such as Inconel® or Haynes® alloy (e.g., Inconel 600, Haynes 230, etc.). Embodiments may include a high temperature nickel-chromium based alloy (e.g., 40-75% Ni-14-25% Cr), optionally further including one or more of iron (e.g., <10% Fe), cobalt (e.g., <15% Co), molybdenum (e.g., <10% Mo), niobium (e.g., <6% Nb), aluminum (e.g., <2% Al), titanium (e.g., <3% Ti), as well as 1% or less each of other constituents, including manganese, copper, silicon, carbon, phosphorous and boron. Other embodiments may include a high-temperature nickel-chromium-tungsten-molybdenum based alloy (e.g., >50% Ni, 20-24% Cr, 13-15% W, 1-3% Mo), with 5% or less each of other constituents, including cobalt, iron, aluminum, manganese, carbon, silicon, phosphorous, sulfur, titanium, boron, copper and/or lanthanum, as well as other suitable high-temperature nickel-based and/or cobalt-based alloys.
An advantage of using thin sheets is that it is easier to form fine features such as the ribs using, for example, a metal stamping technique. One drawback to thin sheets is that they are relatively inefficient at conducting heat from the central region of the stack to the periphery of the stack, and ultimately out of the stack. In embodiments, the gas flow separator section 106 may include an isothermal plate 142, which may increase the ability of the gas flow separator section 106 to efficiently conduct heat from the interior of the stack to the periphery of the stack and ultimately out of the stack. The isothermal plate 142 may be positioned between and in thermal contact with the shaped metal sheets 140, 144. The isothermal plate 142 may be formed from same or different metal alloy material as the shaped metal sheets 140, 144, and may have a thickness of less than about 10 mm, such as less than about 5 mm, and may preferably have a thickness that is less than about 2 mm, such as about 1 mm or less. In embodiments, the isothermal plate 142 may be thicker than the shaped metal sheets 140, 144.
The gas flow separator section 106 may be assembled by attaching the anode-side shaped metal sheet 140 to the cathode-side shaped metal sheet 144 with the isothermal plate 142 between the two sheets 140, 144. The various components of the gas flow separator section 106 may be attached using any suitable attachment technique, such as laser welding, friction welding, brazing, spot welding, etc.
In other embodiments, the gas flow separator section 106 may comprise more or less than three components. For example, the gas flow separator section 106 may be a unitary structure having ridged portions 108, 110 defining flow fields over the anode-facing and cathode-facing surfaces of the structure. In other embodiments, the gas flow separator section 106 may be a two-piece structure that may include, for example, a first section having a ridged portion over an anode-facing surface that may be joined to a second section having a ridged portion over a cathode-facing surface. In other embodiments, the gas flow separator section 106 may include more than three components, and may include, for example, multiple isothermal plates and/or shaped metal sheets formed in multiple sections.
The component(s) of the gas flow separator section 106, such as the anode-side shaped metal sheet 140, the cathode-side shaped metal sheet 144 and the isothermal plate 142 shown in
Thus, in embodiments, the anode support frame 102 and cathode support frame 104 may have a CTE that substantially matches the CTE of the fuel cell electrolyte material (e.g., differs by 1.0% or less, such as 0.5% or less, e.g., 0-0.1%), and the gas flow separator section 106 (e.g., shaped sheet 140, shaped sheet 144 and/or isothermal plate 142) may have a CTE that does not substantially match the CTE of the fuel cell electrolyte material (e.g., differs by more than 1.0%). There may therefore be a mismatch in the CTE between the anode and cathode support frames 102, 104 and the one or more components of the gas flow separator section 106. Because these components may be made from relatively strong and sturdy materials, such as metals, these components may handle the stresses produced by the CTE mismatch better than other, more fragile components, such as the fuel cell electrolyte. In contrast, since the CTE of the frames substantially matches that of the cell electrolyte, there are little to no CTE mismatch stresses on the fragile ceramic electrolyte.
As shown in
As is shown in
The fuel may enter the fuel cell via the bridge 218 of the anode support frame 102. As shown in
In embodiments, the ridged portion 108 may be formed via a stamping process on a thin metal sheet. In one embodiment, the channels 304 formed between adjacent ridges 302 can have a depth that is less than about 10 mm, such as less than about 5 mm (e.g., 0.5 to 2.5 mm), and in preferred embodiments may have a depth of less than about 1 mm. The channels 304 may be wider proximate the fuel inlet plenum 216 to help distribute the fuel evenly across the flow field. The channels 304 may be narrower over the central portion of the flow field, and may then widen again proximate an outlet plenum 232.
As shown in
As is shown in
Fuel may exit the fuel cell via the bridge 234 of the anode support frame 102. As shown in
As is shown in the embodiment of
As shown, for example, in
As shown in
The interconnects 100 according to the various embodiments may be incorporated into a fuel cell stack.
While solid oxide fuel cell interconnects and electrolytes are described above in various embodiments, embodiments can include any other fuel cell interconnects, such as molten carbonate, phosphoric acid or PEM fuel cell interconnects, or any other shaped metal or metal alloy or compacted metal powder or ceramic objects not associated with fuel cell systems.
The foregoing method descriptions are provided merely as illustrative examples and are not intended to require or imply that the steps of the various embodiments must be performed in the order presented. As will be appreciated by one of skill in the art the order of steps in the foregoing embodiments may be performed in any order. Words such as “thereafter,” “then,” “next,” etc. are not necessarily intended to limit the order of the steps; these words may be used to guide the reader through the description of the methods. Further, any reference to claim elements in the singular, for example, using the articles “a,” “an” or “the” is not to be construed as limiting the element to the singular.
Further, any step or component of any embodiment described herein can be used in any other embodiment.
The preceding description of the disclosed aspects is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these aspects will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other aspects without departing from the scope of the invention. Thus, the present invention is not intended to be limited to the aspects shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
This application claims the benefit of priority of U.S. Provisional Patent Application No. 61/714,928 filed Oct. 17, 2012, entitled “Interconnect for Fuel Cell Stack”, the entire contents of which are incorporated by reference herein.
Number | Name | Date | Kind |
---|---|---|---|
4135041 | Jung et al. | Jan 1979 | A |
4292379 | Kothmann | Sep 1981 | A |
4755429 | Nickols et al. | Jul 1988 | A |
4913982 | Kotchick et al. | Apr 1990 | A |
5162167 | Minh et al. | Nov 1992 | A |
5213910 | Yamada | May 1993 | A |
5215946 | Minh | Jun 1993 | A |
5248712 | Takeuchi et al. | Sep 1993 | A |
5256499 | Minh et al. | Oct 1993 | A |
5273837 | Aitken et al. | Dec 1993 | A |
5290642 | Minh et al. | Mar 1994 | A |
5342705 | Minh et al. | Aug 1994 | A |
5368667 | Minh et al. | Nov 1994 | A |
5382315 | Kumar | Jan 1995 | A |
5453331 | Bloom et al. | Sep 1995 | A |
5460897 | Gibson et al. | Oct 1995 | A |
5494700 | Anderson et al. | Feb 1996 | A |
5501914 | Satake et al. | Mar 1996 | A |
5518829 | Satake et al. | May 1996 | A |
5554454 | Gardner et al. | Sep 1996 | A |
5589017 | Minh | Dec 1996 | A |
5641585 | Lessing et al. | Jun 1997 | A |
5733499 | Takeuchi et al. | Mar 1998 | A |
5942349 | Badwal et al. | Aug 1999 | A |
5955392 | Takeuchi et al. | Sep 1999 | A |
5964991 | Kawasaki et al. | Oct 1999 | A |
5981098 | Vitale | Nov 1999 | A |
6001761 | Hata et al. | Dec 1999 | A |
6183897 | Hartvigsen et al. | Feb 2001 | B1 |
6251534 | McElroy | Jun 2001 | B1 |
6280868 | Badwal et al. | Aug 2001 | B1 |
6348280 | Maeda et al. | Feb 2002 | B1 |
6361892 | Ruhl et al. | Mar 2002 | B1 |
6406809 | Fujii | Jun 2002 | B1 |
6444340 | Jaffrey | Sep 2002 | B1 |
6492053 | Donelson et al. | Dec 2002 | B1 |
6492055 | Shimotori et al. | Dec 2002 | B1 |
6503653 | Rock | Jan 2003 | B2 |
6582845 | Helfinstine et al. | Jun 2003 | B2 |
6589681 | Yamanis | Jul 2003 | B1 |
6635378 | Yang et al. | Oct 2003 | B1 |
6777126 | Allen | Aug 2004 | B1 |
6803136 | Ong et al. | Oct 2004 | B2 |
6835488 | Sasahara et al. | Dec 2004 | B2 |
6890677 | Klitsner et al. | May 2005 | B2 |
6945266 | De Tezanos Pinto | Sep 2005 | B2 |
7045237 | Sridhar et al. | May 2006 | B2 |
7150934 | Yoshida et al. | Dec 2006 | B2 |
8173063 | Zobl et al. | May 2012 | B2 |
8563180 | Perry et al. | Oct 2013 | B2 |
20020012825 | Sasahara et al. | Jan 2002 | A1 |
20020081478 | Busenbender | Jun 2002 | A1 |
20020132156 | Ruhl et al. | Sep 2002 | A1 |
20030022053 | Anderson et al. | Jan 2003 | A1 |
20030082434 | Wang et al. | May 2003 | A1 |
20030157387 | Hase et al. | Aug 2003 | A1 |
20030165730 | Dohle et al. | Sep 2003 | A1 |
20030170527 | Finn et al. | Sep 2003 | A1 |
20030180602 | Finn | Sep 2003 | A1 |
20040101742 | Simpkins et al. | May 2004 | A1 |
20040115509 | Yoshida | Jun 2004 | A1 |
20040151975 | Allen | Aug 2004 | A1 |
20040200187 | Warrier et al. | Oct 2004 | A1 |
20040265675 | Woodcock et al. | Dec 2004 | A1 |
20050008921 | Johnson | Jan 2005 | A1 |
20050017055 | Kurz et al. | Jan 2005 | A1 |
20050019646 | Joos | Jan 2005 | A1 |
20050136312 | Bourgeois et al. | Jun 2005 | A1 |
20050227134 | Nguyen | Oct 2005 | A1 |
20050255364 | Cho et al. | Nov 2005 | A1 |
20060154125 | Na et al. | Jul 2006 | A1 |
20060192323 | Zobl et al. | Aug 2006 | A1 |
20060204826 | Borchers | Sep 2006 | A1 |
20060204827 | Hickey et al. | Sep 2006 | A1 |
20060240309 | Dehne | Oct 2006 | A1 |
20060275649 | Keller et al. | Dec 2006 | A1 |
20070042257 | Chyou et al. | Feb 2007 | A1 |
20070134532 | Jacobson et al. | Jun 2007 | A1 |
20070196704 | Valensa et al. | Aug 2007 | A1 |
20070207375 | Jacobson et al. | Sep 2007 | A1 |
20070231676 | Cassidy et al. | Oct 2007 | A1 |
20080081223 | Yasumoto et al. | Apr 2008 | A1 |
20080193825 | Nguyen et al. | Aug 2008 | A1 |
20080199738 | Perry et al. | Aug 2008 | A1 |
20090068535 | Owejan et al. | Mar 2009 | A1 |
20100119909 | McElroy et al. | May 2010 | A1 |
20100119917 | Kumar et al. | May 2010 | A1 |
20100239937 | Janousek et al. | Sep 2010 | A1 |
20110143261 | Brandner et al. | Jun 2011 | A1 |
20110223510 | Greiner et al. | Sep 2011 | A1 |
20110275006 | Hawkes | Nov 2011 | A1 |
20130129557 | Herchen | May 2013 | A1 |
20130130146 | Batawi et al. | May 2013 | A1 |
20130130152 | Couse et al. | May 2013 | A1 |
20130130154 | Darga et al. | May 2013 | A1 |
20140272665 | Yoon | Sep 2014 | A1 |
Number | Date | Country |
---|---|---|
0615299 | Sep 1994 | EP |
61148766 | Jul 1986 | JP |
6-215778 | Aug 1994 | JP |
09-199143 | Jul 1997 | JP |
09-223506 | Aug 1997 | JP |
09-245810 | Sep 1997 | JP |
09-245811 | Sep 1997 | JP |
09-277226 | Oct 1997 | JP |
2000-281438 | Oct 2000 | JP |
10-2006-0019998 | Mar 2006 | KR |
WO03007413 | Jan 2003 | WO |
WO03071618 | Aug 2003 | WO |
WO2004102706 | Nov 2004 | WO |
WO2006016628 | Feb 2006 | WO |
Entry |
---|
“Powder Metallurgy Design Manual,” 3rd Edition, copyright Metal Powder Industries Federation, 1998. |
Haynes International High-Temperature Alloys, “HAYNES (Reg.) 214 (TM) alloy,” 1996, pp. 1-19. |
Haynes International High-Temperature Alloys, “HAYNES (Reg.) 230 (TM) alloy,” 2004, pp. 1-27. |
International Search Report and Written Opinion, International Application No. PCT/US2007/008224, dated Nov. 26, 2008, 10pgs. |
International Search Report, International Application No. PCT/US2003/004808, dated Aug. 19, 2003, 9pgs. |
Supplementary European Search Report, International Application No. PCT/US2003/004808, Jun. 2, 2008, 3pgs. |
International Search Report and Written Opinion, International Application No. PCT/US2010/027899, Oct. 20, 2010, 11pgs. |
International Search Report and Written Opinion, International Application No. PCT/US2012/065508, Apr. 14, 2011. |
International Preliminary Report on Patentability, International Application No. PCT/US2010/027899, Sep. 20, 2011, 6pgs. |
Number | Date | Country | |
---|---|---|---|
61714928 | Oct 2012 | US |