The invention relates generally to solar panel assemblies, and more particularly to a system that provides for the storage and deployment of solar panels.
Many military and civilian operations in remote areas require the generation of on-site electrical power. The cost of deploying fuel for generators and camp lighting can be quite expensive in terms of both fuel cost and the difficulty of delivering such fuel along potentially dangerous routes. In an effort to reduce the number of fuel delivery convoys, alternative energy sources are being explored. Many regions, such as the desert areas of the Middle East, are especially conducive to the use of solar power systems. Unfortunately, existing systems suffer from one or more shortcomings related to functionality and/or efficiency/optimization. Some are cumbersome to set up. Most do not consider array protection during storage and shipment. Still others do not provide for deployment angle adjustability relative to the sun's seasonal orientation to garner maximum power yield.
Accordingly, it is an object of the present invention to provide a storage and deployment system for solar panels.
Another object of the present invention is to provide a solar panel storage/deployment system readily adapted to become a self-contained power generator.
Still another object of the present invention is to provide a solar panel storage and deployment system easily optimized for seasonal orientations of the sun.
In accordance with the present invention, a solar panel storage and deployment system includes a container having an opening formed therein. Also included is an assembly of solar voltaic panels transitionable between a folded state and a deployed state. The assembly defines a series of accordion-like folds along the length thereof when in its folded state. The assembly arrays the panels in a substantially planar arrangement when the assembly is in its deployed state. The assembly has a first end and a second end with the first and second ends remaining in the container when the assembly is in its folded state, and the second end positioned outside of the container when the assembly is in its deployed state. The system also includes at least one stake adapted to be anchored to a position in proximity to and outside of the container. At least one link is provided for coupling the second end of the assembly to the stake(s) when the assembly is in its deployed state.
Other objects, features and advantages of the present invention will become apparent upon reference to the following description of the preferred embodiments and to the drawings, wherein corresponding reference characters indicate corresponding parts throughout the several views of the drawings and wherein:
Referring now to the drawings, simultaneous reference will be made to
System 100 includes a container 10 that houses the elements of system 100 during the storage, shipping, and deployment thereof. Some of these elements in conjunction with container 10 also provide support for one side of a solar panel assembly as will be described later herein. Container 10 can be a standardized container (e.g., an ISO container) or a specially designed container without departing from the scope of the present invention. Container 10 will typically be of rigid construction.
As used herein, the term “solar panel” refers to a flexible or rigid solar voltaic panel that, when exposed to solar energy, generates DC power. One commercial source for flexible solar voltaic panels is Xunlight Corporation, Toledo, Ohio. One commercial source for a rigid solar panel (e.g., poly crystalline cells mounted in a rigid metal frame) is Suntech, San Francisco, Calif. Thus, the term “solar panel assembly” as used herein includes pre-made solar panels as well as a plurality of solar cells arranged into solar voltaic panels where the panels can be flexible or rigid without departing from the scope of the present invention. By way of illustrative example, the embodiment in
The number of solar panels 12 used in the above-described solar panel assembly is not a limitation of the present invention. Flexible substrate 14 can be any material that can support panels 12 and withstand the rigors of an operational environment. For example, flexible substrate 14 could be a tensile fabric such as fabrics made from commercially-available fibers such as KEVLAR or SPECTRA fibers. Hinges 16 can be simple one-piece plastic hinges or multiple-piece hinges without departing from the scope of the present invention. The coupling of hinges 16 to substrate 14 can be achieved in a variety of ways that are not limitations of the present invention. Substrate 14 can extend the full length of the solar panel assembly (as shown) or between adjacent ones of hinges 16 without departing from the scope of the present invention.
Deployment and retraction of the assembly from and into container 10 is made via opening 10A formed in container 10 where opening 10A can be sealable. While the solar panel assembly is in its folded state, solar panels 12 are in a substantially vertical orientation within container 10 and the assembly can be supported on a bearing support 20 mounted/housed in container 10. In general, bearing support 20 (e.g., slide rails, slide table, etc.) provides a sliding support platform on which the lowermost ones of hinges 16 slide as the solar panel assembly transitions to its deployed state and transitions back to its folded state. More specifically, one end of the assembly (e.g., an end 14A of substrate 14) remains attached to bearing support 20 as the other end of the assembly (e.g., an opposing end 14B of substrate 14) is drawn out through opening 10A of container 10.
When the solar panel assembly is deployed as shown in
Retraction and re-packing of the solar panel assembly from its deployed state (
In addition to the mechanical storage and deployment features provided by the present invention, an electrical system can be provided to cooperate with solar panels 12 so that the present invention is a self-contained power provider.
As mentioned above, stake 22 and link 24 cooperate to tension and angularly orient the solar panel assembly of panels 12/substrate 14/hinges 16. An example of a stake 22 and link 24 is illustrated in
The advantages of the present invention are numerous. Solar arrays are safely and securely stored for shipping, but readily deployed once on site. A simple angular orientation system allows the orientation of the panels to be easily adjusted for optimum capture of solar energy. By using a foldable solar panel assembly, the storage size of the assembly is optimized for storage. An onboard electrical system can be added to make the entire system a self-contained AC power source.
Although the invention has been described relative to specific embodiments thereof, there are numerous variations and modifications that will be readily apparent to those skilled in the art in light of the above teachings. It is therefore to be understood that, within the scope of the appended claims, the invention may be practiced other than as specifically described.
The invention described herein may be manufactured and used by or for the Government of the United States of America for Governmental purposes without payment of any royalties thereon or therefore.
Number | Name | Date | Kind |
---|---|---|---|
5969501 | Glidden et al. | Oct 1999 | A |
6201181 | Azzam et al. | Mar 2001 | B1 |
7230819 | Muchow et al. | Jun 2007 | B2 |
7795837 | Haun et al. | Sep 2010 | B1 |
20080068782 | Muchow et al. | Mar 2008 | A1 |
20090102415 | Muchow et al. | Apr 2009 | A1 |
20100026235 | Harris | Feb 2010 | A1 |
20110277809 | Dalland et al. | Nov 2011 | A1 |
20120291847 | Rowe et al. | Nov 2012 | A1 |