US 7,987,641 B2Grant
Mounting system for a solar panel
Issue Date:2011-08-02
•3 Claims
•8 Drawing Sheets
Abstract
An integrated module frame and racking system for a solar panel is disclosed. The solar panel comprises a plurality of solar modules and a plurality of splices for coupling the plurality of solar modules together. The plurality of splices provide a way to make the connected modules mechanically rigid both during transport to the roof and after mounting for the lifetime of the system, provide wiring connections between modules, provide an electrical grounding path for the modules, provide a way to add modules to the panel, and provide a way to remove or change a defective module. Connector sockets are provided on the sides of the modules to simplify the electrical assembly of modules when the modules are connected together with splices.
Metadata
Assignee
- Andalay Solar, Inc.
Inventor
- Barry Cinnamon
Application Information
Application Number:US 11/851,914
Filing Date:2007-09-07
Priority Date:2004-05-18
Art Unit:3635
Classifications
IPC:
E04D13/18E04B2/00H01L31/042
Patent Drawings (8 sheets)
Description
Cross-Reference to Related Applications
[0001] Under 35 USC §120, this application is a divisional application and claims the benefit of priority to U.S. patent application Ser. No. 10/849,069, filed May 18, 2004, entitled “Mounting System for a Solar Panel”, and is related to co-pending patent application filed concurrently on even-date herewith, entitled, “Mounting System for a Solar Panel” as Ser. No. 11/851,674, all of which is incorporated herein by reference.
Field of the Invention
[0002] The present invention relates generally to solar panels and more particularly to an assembly and mounting system for a solar panel.
Background of the Invention
[0003] Solar electric systems are the most environmentally friendly way of generating electricity. To provide such solar electric systems, typically there is a solar panel, which comprises a plurality of solar modules, which are coupled together. The solar panels are typically assembled directly on the roof of a building, assembled on the ground and then mounted on a roof of a building, or installed on a dedicated ground or pole mounted frame. FIG. 1 illustrates a conventional solar panel assembly 10. The solar panel in this embodiment comprises three solar modules, 12A-12C. However, one of ordinary skill in the art recognizes there could be any number of modules and they could be in any configuration to form a solar panel.
[0004] Each of the solar panel modules 12A-12C includes a junction box 14A-14C which receives cables 16, which are applied in serial fashion from one module to the next. Also included within each of these modules 12A-12C is an electrical ground wire assembly 18, which is used to ground the modules and the underlying frame at the appropriate points. In addition, each of the modules includes extra wiring from nearby modules that must be wrapped and tied down in between, as shown at 20A and 20B to ensure that the wires do not get damaged. FIG. 1A is a view of the grounding screw for the solar panel. The screw or bolt assembly 22, which must be provided in several places, attaches the ground wire assembly 18 to each piece of equipment in the assembly at least once, in this case five (5) places, on each of the solar modules 12A-12C and underlying frame, thereby creating a grounded assembly.
[0005] Referring back in FIG. 1 , there are two metal rails 24 that extend in parallel with and along the length of the solar modules 12A-12C. These rails form the underlying support structure for the solar modules. The rails are attached to the roof so that the entire solar panel can be mounted in a single rigid geometric plane on the roof, thereby improving the durability and aesthetics of the installation. In some cases the rails are mounted to the roof first (attached to the roof with L shaped brackets and lag bolts to the underlying rafters), and then the modules are attached to the rails with bolt-fastened clips. In other cases, as shown in FIG. 1B , the rails are attached to the modules first (in this case with hex nuts and bolts or in other cases clips), and then the entire module-rail assembly (or panel) is attached to the roof with L shaped brackets 26 (FIG. 1 ) and lag bolts to the underlying rafters. These rails 24 are also electrically grounded as indicated above.
[0006] For ventilation and drainage purposes it is beneficial to mount the panel above the roof with a small air gap between the roof surface and underside of the modules and rails. For wiring and grounding purposes for roof assembled panels it is beneficial to have access below the modules so that wires can be connected and tied. For single geometric plan purposes it is beneficial to provide some vertical adjustability of the mounting point to account for variability (waviness) in roof surfaces. For these reasons the roof mounting bracket (whether it is an L shaped bracket or different design) generally provides some vertical adjustability (typically 1-3 inches). Moreover, roof attachments must be made to a secure underlying surface, generally a rafter. These rafters may not be consistently spaced. Therefore, the mounting rails typically include some kind of adjustable groove so that the mounting point from the rail to the roof attachment (L bracket) can be directly over a secure mounting point—wherever this point may be.
[0007] The conventional solar panel 10 requires many individual operations to construct and mount in order to provide a reliable and high performance solar electric system. Mounting on uneven roof surfaces requires many small parts and adjustments. Making sure there is airflow and drainage requires the panel to be raised off the roof slightly, but aesthetic considerations require the panel to be close to the roof. Each module in the panel must be wired together, extra wiring must be tucked away securely, and every conductive component must be electrically grounded. All the required parts and steps increase the cost of the system, which ultimately negatively affects the payback of the system. In addition, conventional solar modules are shipped in cardboard boxes on palettes, requiring additional shipping costs and substantial unpacking and cardboard disposal costs.
[0008] Accordingly, what is desired is a solar module which is more self contained, including all the mounting and wiring hardware, without requiring all of the individual operations, minimizing the number of electrical grounding steps required, and minimizing the amount of wiring and cables that need to be managed. Finally, the system should be one that minimizes the number of parts and tools that an installer would need to assemble and install the panel. This system should be easily implemented, adaptable to various environments and cost effective. The present invention addresses such a need.
Summary of the Invention
[0009] An integrated module frame and racking system for a solar panel is disclosed. The solar panel comprises a plurality of solar modules and a plurality of splices for coupling the plurality of solar modules together. The plurality of splices provide a way to make the connected modules mechanically rigid both during transport to the roof and after mounting for the lifetime of the system, provide wiring connections between modules, provide an electrical grounding path for the modules, provide a way to add modules to the panel, and provide a way to remove or change a defective module. Connector sockets are provided on the sides of the modules to simplify the electrical assembly of modules when the modules are connected together with splices.
[0010] A solar panel in accordance with the present invention is optimized for fast and reliable installation. In addition, the fewer parts and simpler assembly technique reduces the potential for installation error. In addition, multiple modules for the panel can be supported during transport. In addition, modules and panels can be assembled closer together, improving space usage and improving aesthetics. Furthermore, individual modules can be added to and connected with existing solar panels. In addition, the use of an integrated mounting rail allows the panel to be mounted closer to the roof, improving aesthetics. Further, a minimal number of parts are utilized for the entire assembly. Finally, solar modules can be securely stacked and shipped with pre-installed mounting brackets, reducing shipping, packing and unpacking costs.
Brief Description of the Drawings
[0011] FIG. 1 illustrates a conventional solar panel assembly.
[0012] FIG. 1A is a view of a grounding screw for the solar panel.
[0013] FIG. 1B is a view of a module attached to a rail.
[0014] FIG. 2 illustrates a perspective view of a mounting system for a solar panel in accordance with the present invention.
[0015] FIG. 2A is a diagram of a back view of the solar panel in accordance with the present invention.
[0016] FIG. 2B shows an east-west splice that allows connection of a module or panel to the side (typically east or west) of an existing module.
[0017] FIG. 2C shows a north-south splice that allows connection of a module or panel above or below (typically north or south) of an existing module.
[0018] FIG. 3 illustrates a splice in accordance with the present invention.
[0019] FIG. 4 illustrates a groove on the module panel and a surface mounting bracket for securing the module panel to the roof.
[0020] FIG. 5 illustrates a shipping stack of solar modules with pre-installed mounting brackets, through attachment rod and splice storage.
Detailed Description
[0021] The present invention relates generally to solar panels and more particularly to a mounting system for solar panels. The following description is presented to enable one of ordinary skill in the art to make and use the invention and is provided in the context of a patent application and its requirements. Various modifications to the preferred embodiment and the generic principles and features described herein will be readily apparent to those skilled in the art. Thus, the present invention is not intended to be limited to the embodiment shown but is to be accorded the widest scope consistent with the principles and features described herein.
[0022] A system and method in accordance with the present invention provides for an integrated module frame and racking system for a solar panel. The solar panel in accordance with the present invention is optimized for fast installation on a structure with a particular emphasis on completing all installation activities from the top of the module (without wiring, grounding and attachments from below). This optimization includes all steps in assembling and installing the solar panel. Furthermore utilizing the integrated frame and racking system multiple modules for the panel can be supported during transport. In addition by utilizing the integrated system in accordance with the present invention individual modules can be added to and connected with existing solar panels and can be mounted in a more aesthetically pleasing way. Finally, a minimal number of parts are utilized for the entire assembly.
[0023] To describe the features of the present invention in more detail, refer now to the following description in conjunction with the accompanying drawings.
[0024] FIG. 2 illustrates a perspective view of a mounting system for a solar panel 100 in accordance with the present invention. As is seen, there are three modules 102A-102C shown that are coupled together that include several features that allow for a modularized and integrated system for the solar panel 100. Firstly, there is a splice that mechanically connects one module to another and provides the electrical grounding connection between the solar modules. The mechanical strength of the splice and attachment technique to the module frame allows each module frame to function in the same rigid way as the underlying frame rail in a conventional solar panel assembly. In addition, there are cable connector grooves between modules that minimize the amount of wiring activities that are required for connecting the modules together. Finally, the system includes only requiring one electrical grounding connection to the entire panel; module to module and module to rail grounding connections are not needed. To describe the feature of the invention in more detail refer now to the following description in conjunction with the accompanying figures.
[0025] FIG. 2A is a diagram of a back view of the solar panel 100 in accordance with the present invention. As has been above-mentioned the solar panel 100 includes a plurality of modules 102A-102C. However, one of ordinary skill in the art readily recognizes that the panel 100 could include any number of modules in both the X and Y directions and could be in any configuration and its use would be within the spirit and scope of the present invention. The solar panel 100 requires significantly fewer parts to assemble and is more easily constructed than the conventional solar panel 10 of FIG. 1 . Referring now to FIG. 2B , as is seen there is an east-west (e-w) splice 104 shown internal to two modules 102A and 102B that connect the modules 102A and 102B. The splice 104 provides several useful features for the panel 100, including mechanical rigidity between modules, a grounding path between modules, an alignment method between modules, a securing method between modules and a compression method between modules.
[0026] Also north-south splices between rows can be effectively utilized. FIG. 2C shows a north-south splice 104E that allows connection of a module or panel above (typically north) or below an existing module. This splice 104E provides alignment between rows, rigidity between rows and provides a grounding connection. Use of this north-south splice 104E reduces mounting points on the mounting surface.
[0027] In a preferred embodiment, the splice is a rigid removable connecting piece that protrudes from the side or top of the module when inserted in one module. Additionally, the splice is generally hidden when installed, by virtue of mounting inside the module frame hollow section or side groove. The splice allows for a very close fit between modules, thereby improving space utilization. Also, the splice has conductive capability (including the nonconductive main part with conductive wires or surface). The splice has a slightly arched profile to counteract module sag after installation (similar to the arch on a bridge). It should also be understood, that although the splice in this embodiment is internal to the solar modules, one of ordinary skill in the art readily recognizes that the splice could be external and its use could be within the spirit and scope of the present invention.
[0028] FIG. 3 illustrates a splice 104 in accordance with the present invention. The splice 104 is tapered to allow for easy initial assembly line up and a final tight fit between the modules 102A and 102B. In a preferred embodiment it is precisely located in the panel 100 in a centerline fashion. In a preferred embodiment the splice 104 is a tapered conductive metal to provide a grounding path between modules, and includes a sharp edge to improve grounding to each module. The splice 104 is also grooved for easy screw insertion from the top or the side of the module 102. The splice 104 precisely aligns the modules 102 and allows the assembler to compress the connector sockets 108, thereby completing an electrical connection between the two adjacent modules. The electrical connection between the two adjacent modules by the splice 104 eliminates the need to run a grounding wire between each module. As is seen only one other grounding wire is required for an entire panel assembly as long as all solar modules are connected with a splice. The splice provides sufficient rigidity between modules so that the entire panel can be transported and lifted to a roof, or installed directly on a roof or other surface in a secure and long lasting fashion.
[0029] In a preferred embodiment, each splice would utilize a screw for attachment to secure the two modules together. Other mechanisms for securing the two modules together include but are not limited to a cam type compression device, a press fit or toothed barb device, a spring clip attachment, a through pin and an expandable section at each end. For a three module solar panel, as illustrated in exploded view, a total of four splices and eight self-threading screws are utilized to provide the solar panel. Accordingly, a minimal number of parts are required for the assembly of the panel. The splice also includes a plurality of raised features, which couple the modules together. The first raised feature 132 acts as a stop for the splice. The second raised feature 134 acts as a grounding path for the splice.
[0030] Referring back to FIG. 2 , a plurality of connector sockets 108 are provided in each of the modules 102. These connector sockets 108 provide the following advantages:
[0031] The connector sockets 108 can be labeled (+/−) and then sized to only accept the proper cable connection, thereby minimizing wiring problems. The connector sockets 108 are located on the modules (on the left/right or E-W sides, and/or on the top/bottom or N/S sides) to prevent improper wiring based on cable lengths and connector socket size/configuration. The connector sockets 108 are on frame sides to allow for easy and reliable module interconnection. The connector sockets 108 on frame sides allow for pre-installed home run return wire paths. The connector sockets 108 on frame sides allow for interconnection of strings. The connector sockets 108 on frame sides allow for concealed wire connections after modules are mounted. Finally, the overall design improves wire management and grounding.
[0032] Optimally a cable holder 136 can be used in this solar panel. Referring back to FIG. 2A , a cable holder 136 is coupled to a side portion of a module to hold cables that may be stored in the panel. Typically the cable holder 136 is a cable clip that holds the stored cable in place.
[0033] FIG. 4 illustrates a groove 142 on the metal plate 138 of the module. The groove allows for securing the panel (composed of one or more modules) to a structure, such as a roof, with the mounting bracket. The grooves 142 on the sides of each of the metal plate are aligned when the modules are connected with splices, thereby creating a continuous groove along the entire panel to allow for the connection of the solar panel to a roof or the like. In so doing the solar panel can be rigidly mounted on a structure in a single plane. The continuous groove allows attachment to an available secure point (typically a rafter) at any horizontal location. Typically the grooved portion will comprise an extrusion on a metal plate 138 shown in FIG. 4 that is part of the module thereby creating a full and roughly continuous extension in the panel. This groove 142 can be installed on both the sides (east-west) and top/bottom (north-south) of the modules, allowing the module to be installed in a variety of different orientations.
[0034] The mounting bracket 140 attaches securely to the roof and then attaches to the grooved metal plate 138 with a bolt. This bracket 140 may include provisions to mount the panel at a variable height to account for variations in surfaces. Alternatively, this bracket 140 may be mounted to the roof with a threaded bolt or other variable height mounting point. The solar panels can be mounted on a horizontal, vertical or sloped structure or surface utilizing the mounting bracket.
[0035] Finally, solar modules can be securely stacked and shipped with pre-installed mounting brackets, reducing shipping, packing and unpacking costs. FIG. 5 illustrates a shipping stack of solar modules with pre-installed mounting brackets, through attachment road and splice storage.
[0036] FIG. 5 illustrates how multiple modules are securely stacked for shipment on a single palette. Mounting brackets 140A-140E are pre-installed on sides of modules 104, thereby reducing field-installation labor. Note that, depending on rafter location, these brackets 140A-140B are easily loosened and moved during installation. A metal rod 200 is installed in holes in the mounting brackets 140A-140B, thereby preventing module shifting during shipment.
[0037] In this illustration, mounting brackets are offset so that every-other bracket is aligned, although using a different bracket configuration all the brackets can be in one vertical plane or installed at different locations on the module frame. Splices are slid over the metal rod for storage during shipping. In this embodiment, a stack of 16 modules would have 32 mounting brackets pre-installed on module frames, and 32 splices stored on four metal securing rods.
Summary
[0038] An integrated module frame and racking system for a solar panel is disclosed. The solar panel comprises a plurality of solar modules and a plurality of internal splices for coupling the plurality of solar modules together. The plurality of internal splices provide a way to make the connected modules mechanically rigid both during transport to the roof and after mounting for the lifetime of the system, provide wiring connections between modules, provide an electrical grounding path for the modules, provide a way to add modules to the panel, and provide a way to remove or change a defective module. Connector sockets are provided on the sides of the modules to simplify the electrical assembly of modules when the modules are connected together with splices.
[0039] A solar panel in accordance with the present invention is optimized for fast and reliable installation. In addition, the fewer parts and simpler assembly technique reduces the potential for installation error. In addition, multiple modules for the panel can be supported during transport. In addition, modules and panels can be assembled closer together, improving space usage and improving aesthetics. Furthermore, individual modules can be added to and connected with existing solar panels. In addition, the use of an integrated mounting rail allows the panel to be mounted closer to the roof, improving aesthetics. Finally, a minimal number of parts are utilized for the entire assembly.
[0040] Although the present invention has been described in accordance with the embodiments shown, one of ordinary skill in the art will readily recognize that there could be variations to the embodiments and those variations would be within the spirit and scope of the present invention. For example, although the splice is preferably made of a conductive material such as aluminum, it could be made utilizing a non-conductive material which has a conductive capability added to its surface and its use would be within the spirit and scope of the present invention. Accordingly, many modifications may be made by one of ordinary skill in the art without departing from the spirit and scope of the appended claims.
Claims
Post-issuance certificates present
The text shown below may not reflect later post-issuance changes.
What is claimed is:
1. A solar module comprising:
a body portion having a frame;
one or more splices, wherein each splice couples the frame of the body portion rigidly to a frame of the body portion of an adjacent solar module;
a bracket that securely attaches the solar module to a roof wherein the bracket is located along any portion of the frame;
wherein each splice further comprises a body for coupling the frames of the solar module and the adjacent solar module together and a securing mechanism for securing the frames of the solar module and the adjacent solar module together.
2. The solar module of claim 1, wherein the securing mechanism further comprises one of a screw, a cam type compression device, a press fit barb device, a toothed barb device, a spring clip attachment, a through pin and an expandable section at each end of the splice.
3. The solar module of claim 1 further comprising a coupling mechanism for coupling the frames of the solar module and the adjacent solar module together, the coupling mechanism further comprises one of a screw, a cam type compression device, a press fit barb device, a toothed barb device, a spring clip attachment, a through pin and an expandable section at each end of the splice.
Patent Citations (129)
| Patent | Date | Inventor | Cited By |
|---|---|---|---|
| US510315(A) | 1893-12-01 | Begtrup | Applicant |
| US511576(A) | 1893-12-01 | Baker | Applicant |
| US516017(A) | 1894-03-01 | La Rue | Applicant |
| US519444(A) | 1894-05-01 | Clark | Applicant |
| US562225(A) | 1896-06-01 | Hutter | Applicant |
| US564958(A) | 1896-07-01 | Holmes | Applicant |
| US565505(A) | 1896-08-01 | Publow | Applicant |
| US3630253(A) | 1971-12-01 | Sherman | Applicant |
| US4112922(A) | 1978-09-01 | Skinner et al. | Applicant |
| US4146785(A) | 1979-03-01 | Neale | Applicant |
| US4154223(A) | 1979-05-01 | Lof | Applicant |
| US4219011(A) | 1980-08-01 | Knoos | Applicant |
| US4271825(A) | 1981-06-01 | Schwob et al. | Applicant |
| US4429872(A) | 1984-02-01 | Capachi | Applicant |
| US4570408(A) | 1986-02-01 | Frascaroli et al. | Applicant |
| US4691818(A) | 1987-09-01 | Weber | Applicant |
| US4718185(A) | 1988-01-01 | Conlin et al. | Applicant |
| US4966631(A) | 1990-10-01 | Matlin | Applicant |
| US5046791(A) | 1991-09-01 | Kooiman | Examiner |
| US5127762(A) | 1992-07-01 | Havlovitz | Applicant |
| US5143556(A) | 1992-09-01 | Matlin | Applicant |
| US5144780(A) | 1992-09-01 | Gieling et al. | Applicant |
| US5164019(A) | 1992-11-01 | Sinton | Applicant |
| US5164020(A) | 1992-11-01 | Wagner et al. | Applicant |
| US5203135(A) | 1993-04-01 | Bastian | Applicant |
| US5205694(A) | 1993-04-01 | Nagoshi et al. | Applicant |
| US5232518(A) | 1993-08-01 | Nath et al. | Applicant |
| US5316592(A) | 1994-05-01 | Dinwoodie | Applicant |
| US5497587(A) | 1996-03-01 | Hirai et al. | Applicant |
| US5505788(A) | 1996-04-01 | Dinwoodie | Applicant |
| USD374169(S) | 1996-10-01 | Kopish | Applicant |
| US5571338(A) | 1996-11-01 | Kadonome et al. | Applicant |
| US5596981(A) | 1997-01-01 | Soucy | Applicant |
| US5628580(A) | 1997-05-01 | Rinderer | Applicant |
| USD387655(S) | 1997-12-01 | Kopish | Applicant |
| US5706617(A) | 1998-01-01 | Hirai et al. | Applicant |
| US5746029(A) | 1998-05-01 | Ullman | Applicant |
| US5746839(A) | 1998-05-01 | Dinwoodie | Applicant |
| US5960790(A) | 1999-10-01 | Rich | Applicant |
| US6061978(A) | 2000-05-01 | Dinwoodie | Applicant |
| US6093884(A) | 2000-07-01 | Toyomura et al. | Applicant |
| US6105317(A) | 2000-08-01 | Tomiuchi et al. | Applicant |
| US6111189(A) | 2000-08-01 | Garvison et al. | Applicant |
| US6148570(A) | 2000-11-01 | Dinwoodie et al. | Applicant |
| US6201180(B1) | 2001-03-01 | Meyer et al. | Applicant |
| US6207889(B1) | 2001-03-01 | Toyomura et al. | Applicant |
| US6269596(B1) | 2001-08-01 | Ohtsuka et al. | Applicant |
| US6274402(B1) | 2001-08-01 | Verlinden et al. | Applicant |
| US6295818(B1) | 2001-10-01 | Ansley et al. | Applicant |
| US6313395(B1) | 2001-11-01 | Crane et al. | Applicant |
| US6337283(B1) | 2002-01-01 | Verlinden et al. | Applicant |
| US6360491(B1) | 2002-03-01 | Ullman | Applicant |
| US6370828(B1) | 2002-04-01 | Genschorek | Applicant |
| US6387726(B1) | 2002-05-01 | Verlinden et al. | Applicant |
| US6423568(B1) | 2002-07-01 | Verlinden et al. | Applicant |
| US6465724(B1) | 2002-10-01 | Garvison et al. | Applicant |
| US6495750(B1) | 2002-12-01 | Dinwoodie | Applicant |
| US6501013(B1) | 2002-12-01 | Dinwoodie | Applicant |
| US6523320(B2) | 2003-02-01 | Stoof | Applicant |
| US6534702(B1) | 2003-03-01 | Makita et al. | Applicant |
| US6534703(B2) | 2003-03-01 | Dinwoodie | Applicant |
| US6568873(B1) | 2003-05-01 | Peterson | Applicant |
| US6570084(B2) | 2003-05-01 | Dinwoodie | Applicant |
| US6586668(B2) | 2003-07-01 | Shugar et al. | Applicant |
| US6670541(B2) | 2003-12-01 | Nagao et al. | Applicant |
| US6672018(B2) | 2004-01-01 | Shingleton | Applicant |
| US6675545(B2) | 2004-01-01 | Chen et al. | Applicant |
| US6675580(B2) | 2004-01-01 | Ansley et al. | Applicant |
| US6676326(B2) | 2004-01-01 | Wu | Applicant |
| US6722357(B2) | 2004-04-01 | Shingleton | Applicant |
| US6761008(B2) | 2004-07-01 | Chen et al. | Applicant |
| US6784360(B2) | 2004-08-01 | Nakajima et al. | Applicant |
| US6809251(B2) | 2004-10-01 | Dinwoodie | Applicant |
| US6809253(B2) | 2004-10-01 | Dinwoodie | Applicant |
| US6935623(B2) | 2005-08-01 | Cook | Applicant |
| US6959517(B2) | 2005-11-01 | Poddany et al. | Examiner |
| US6993917(B2) | 2006-02-01 | Unger et al. | Applicant |
| US7043884(B2) | 2006-05-01 | Moreno | Applicant |
| US7172184(B2) | 2007-02-01 | Pavani et al. | Applicant |
| US7328534(B2) | 2008-02-01 | Dinwoodie | Applicant |
| US7339110(B1) | 2008-03-01 | Mulligan et al. | Applicant |
| US7406800(B2) | 2008-08-01 | Cinnamon et al. | Applicant |
| US7435897(B2) | 2008-10-01 | Russell | Applicant |
| US7592537(B1) | 2009-09-01 | West | Applicant |
| US7634875(B2) | 2009-12-01 | Genschorek | Examiner |
| US7774998(B2) | 2010-08-01 | Aschenbrenner | Examiner |
| US2002/0046506(A1) | 2002-04-01 | Ullman | Applicant |
| US2002/0078991(A1) | 2002-06-01 | Nagao et al. | Applicant |
| US2003/0010372(A1) | 2003-01-01 | Dinwoodie | Applicant |
| US2003/0015637(A1) | 2003-01-01 | Liebendorfer | Examiner |
| US2003/0070368(A1) | 2003-04-01 | Shingleton | Applicant |
| US2003/0175071(A1) | 2003-09-01 | Layfield | Applicant |
| US2004/0063265(A1) | 2004-04-01 | Noble | Applicant |
| US2004/0163338(A1) | 2004-08-01 | Liebendorfer | Applicant |
| US2004/0179892(A1) | 2004-09-01 | Du Preez | Applicant |
| US2006/0005875(A1) | 2006-01-01 | Haberlein | Examiner |
| US2006/0118163(A1) | 2006-06-01 | Plaisted et al. | Applicant |
| US2007/0079865(A1) | 2007-04-01 | Warfield et al. | Applicant |
| US2007/0102036(A1) | 2007-05-01 | Cinnamon | Applicant |
| US2008/0029144(A1) | 2008-02-01 | Brazier et al. | Applicant |
| US2009/0078299(A1) | 2009-03-01 | Cinnamon | Applicant |
| DE3111969(A1) | 1982-10-01 | Applicant | |
| DE4444439(A1) | 1995-04-01 | Applicant | |
| DE2970348(U) | 1997-11-01 | Applicant | |
| JP47-023570 | 1971-07-01 | Applicant | |
| JP47-057885 | 1972-05-01 | Applicant | |
| JP57-077856 | 1982-05-01 | Applicant | |
| JP58-133945(U) | 1983-09-01 | Applicant | |
| JP59-191748(U) | 1984-12-01 | Applicant | |
| JP2-42449(U) | 1990-03-01 | Applicant | |
| JP4-052367 | 1992-02-01 | Applicant | |
| JP6-069527 | 1994-03-01 | Applicant | |
| JP6-41156(U) | 1994-05-01 | Applicant | |
| JP10-159284 | 1998-06-01 | Applicant | |
| JP10-176403 | 1998-06-01 | Applicant | |
| JP10-317619 | 1998-12-01 | Applicant | |
| JP10-317621 | 1998-12-01 | Applicant | |
| JP11-002004 | 1999-01-01 | Applicant | |
| JP11-002011 | 1999-01-01 | Applicant | |
| JP11-006262 | 1999-01-01 | Applicant | |
| JP11-040835 | 1999-02-01 | Applicant | |
| JP11-222991 | 1999-08-01 | Applicant | |
| JP2000-150947 | 2000-05-01 | Applicant | |
| JP2000-345664 | 2000-12-01 | Applicant | |
| JP2001-148493 | 2001-05-01 | Applicant | |
| JP2001-210853 | 2001-08-01 | Applicant | |
| JP2002-294957 | 2002-10-01 | Applicant | |
| JP2003-227207 | 2003-08-01 | Applicant | |
| WO2005116359(A2) | 2005-12-01 | Applicant |
Non-Patent Literature (23)
- US 5,819,447, 10/1998, Yamawaki (withdrawn)Applicant
- PCT/US05/16849 International Search Report, Jun. 19, 2008.Applicant
- PCT/US05/16849 Written Opinion, Jun. 19, 2008.Applicant
- “Notification of Reasons for Rejection”, mailing date Jun. 9, 2009; Japanese Application No. JP2007-527321;Patent Attorney : Hironori Onda; Mamoru.Applicant
- JP Pub. 2002-141541 Patent Abstracts of Japan, dated May 17, 2002.Applicant
- JP Pub. 61-040963 Japanese Examined Utility Model.Applicant
- JP Pub. 07-202242 Patent Abstracts of Japan, dated Aug. 4, 1995.Applicant
- PCT/US2009/037021 International Search Report dated May 12, 2009.Applicant
- PCT/US2009/037021 Written Opinion dated May 12, 2009.Applicant
- PCT/US05/16849 International Search Report, Jun. 19, 2008.Applicant
- PCT/US05/16849 Written Opinion, Jun. 19, 2008.Applicant
- PCT/US08/10992 International Search Report, Nov. 25, 2008.Applicant
- PCT/US08/10992 Written Opinion, Nov. 25, 2008.Applicant
- “Re-Exam U.S. Appl. No. 95/001,304 (U.S. Appl. No. 10/849,069), Response to Inter-Parties Re-Exam Office Action Pursuant to 37 CFR 1.945”, filed on Sep. 23, 2010 (20 pgs.).Applicant
- “Re-Exam U.S. Appl. No. 95/001,304 (U.S. Appl. No. 10/849,069), Non-Final Office action dated Sep. 1, 2010”, mailed on Sep. 1, 2010 (22 pgs.).Applicant
- “Re-Exam U.S. Appl. No. 95/001,304 (U.S. Appl. No. 10/849,069), Response to Inter-Parties Re-Exam Office Action Pursuant to 37 CFR 1.945”, filed on May 14, 2010 (10 pgs.).Applicant
- “Re-Exam U.S. Appl. No. 95/001,304 (U.S. Appl. No. 10/849,069), Non-Final Office action dated Sep. 1, 2010”, mailed on Apr. 16, 2010 (40 pgs.).Applicant
- Re-Examination Action Closing Prosecution dated Nov. 30, 2010—U.S. Appl. No. 95/001,304.Applicant
- Third Party Comments dated Jan. 28, 2011—U.S. Appl. No. 95/001,304.Applicant
- Notice of Intent to Issue Re-Exam Certificate dated Apr. 4, 2011—U.S. Appl. No. 95/001,304.Applicant
- 95001304—Third Party Comments dated Oct. 25, 2010—19 pgs.Applicant
- 95001304—Response to Office Action dated Dec. 29, 2010—7 pgs.Applicant
- 95001304—Third Party Comments dated Jul. 2, 2010—11 pgs.Applicant