1. Field of the Invention
The present invention relates generally to the field of hot air engines. More specifically, the present invention discloses a solar-powered hot air engine.
2. Background of the Invention
A variety of hot air engines, such as Stirling engines, have been in existence for centuries. A general summary is provided in the Wikipedia article on Stirling engines, which discusses the various configurations of a Stirling engine and is hereby incorporated by reference. The prior art in this field also includes a variety of solar-powered hot air engines, as taught for example, by U.S. Pat. No. 6,996,983 (Cameron), U.S. Pat. No. 5,404,723 (Parker et al.) and U.S. Pat. No. 4,642,988 (Benson).
For example, the Cameron patent discloses a rotary Stirling engine having a glass window for transmitting solar radiation into the heat chamber. Cameron also discloses a blackened wall within the heat chamber for absorbing solar radiation.
However, it appears that nothing in the prior art teaches or suggests a solar-powered hot air engine having the specific physical configuration of the present invention. In particular, the present invention employs a thin disk of regenerator material having low thermal conductivity on the face of the displacer piston at the hot end of the cylinder, and a layer of material with high absorptivity and low emissivity covers the regenerator material and the interior surface of the cylinder. This configuration has the advantages of being directly applicable to conventional hot air engines that use pistons, such as the beta-type Stirling engine shown in
This invention provides a hot air engine, such as a Stirling engine, having a cylinder with hot and cold ends, and a solar collector directing radiation through a window into the hot end of the cylinder. A thin layer of regenerator material having low thermal conductivity is placed on the face of the displacer piston at the hot end of the cylinder, and a layer of material with high absorptivity and low emissivity covers the regenerator material and the interior surface of the cylinder to maximize absorption of the solar energy within the hot end of the cylinder.
These and other advantages, features, and objects of the present invention will be more readily understood in view of the following detailed description and the drawings.
The present invention can be more readily understood in conjunction with the accompanying drawings, in which:
Turning to
A solar collector 15 (e.g., a parabolic reflector) directs solar radiation 10 through a window 24 into the hot end of the cylinder 22. The window 24 can be made of glass or a suitable transparent ceramic material. Preferably, the window 24 is located at the head of the hot end of the cylinder 22, so that solar radiation 10 gathered by the solar collector 15 passes through the window 24 into the hot end of the cylinder 22 and toward the face of the displacer piston 26 as illustrated in
As shown in
Any of a wide variety of materials can be employed as the absorptive coating, including carbon black, nickel III oxide (Ni2O3), ceramics and ceramic/metal composite materials (i.e., cermet materials). An extensive list of potentially-suitable materials is provided on page 12 of C. E. Kennedy, “Review of Mid- to High-Temperature Solar Selective Absorber Materials” (National Renewable Energy Laboratory, July 2002, NREL/TP-520-31267), which is hereby incorporated by reference. Optionally, a layer of regenerator material 33 can be placed between the absorptive layer 32 and the wall of the cylinder 22, as shown in
The effectiveness of the absorptive layers 32, 36 can be enhanced by increasing the exposed surface area of these layers. For example, this can be done by creating a three-dimensional texture to the surfaces. The increased surface area provides greater absorption of incoming solar radiation by the absorptive layers 32, 36, and also increases heat transfer to the working gas in the hot chamber of the cylinder 22.
Optionally, the present invention can also include an insulating layer 38 between the regenerator material 34 and the face of the piston 26 to decrease unwanted heat transfer into the piston 26. For example, the insulating layer 38 could be multi-layer insulation or suitable refractory material.
The above disclosure sets forth a number of embodiments of the present invention described in detail with respect to the accompanying drawings. Those skilled in this art will appreciate that various changes, modifications, other structural arrangements, and other embodiments could be practiced under the teachings of the present invention without departing from the scope of this invention as set forth in the following claims.
The present application is based on and claims priority to the Applicant's U.S. Provisional Patent Application 62/105,580, entitled “Solar-Powered Hot Air Engine,” filed on Jan. 20, 2015.
Number | Date | Country | |
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62105580 | Jan 2015 | US |