Method and apparatus for solar power conversion
View Patent ↗A solar power conversion system using a plurality of engines to convert solar energy to electrical energy. The plurality of engines are supported adjacent to a housing having a single thermal cavity. The cavity is provided with solar energy from a solar collector. Each of the engines can be turned off or regulated to maintain an optimum operating temperature for a common heater head in communication with each of the engines. Therefore, the power conversion system can be regulated for variations in insolation to maintain an optimum temperature in the heater head. Therefore, increased life cycle energy efficiency of the power conversion system can be obtained.
1. A power conversion system for converting thermal energy into electrical energy, comprising:
a housing having a thermal cavity for receiving and collecting thermal energy directed into the cavity from an external component;
a plurality of engines disposed in communication with the thermal cavity, the engines being able to use the collected thermal energy to perform work;
at least one of said engines having an alternator operably associated therewith for producing electrical energy from mechanical energy performed by said one engine; and
at least one of said engines is adapted to be controlled so that the amount of thermal energy in said thermal cavity can be controlled.
2. The system of claim 1 , wherein the thermal cavity is able to receive thermal energy produced by a combustible fuel.
3. The system of claim 2 , wherein the combustible fuel is selected from a group consisting of: hydrocarbons, hydrogen, carbon, and mixtures thereof.
4. The system of claim 1 , wherein each of said engines comprises an alternator.
5. The system of claim 1 , further comprising a controller for controlling said alternator in a manner to manage the usage of thermal energy in said thermal cavity.
6. The system of claim 5 , further comprising a temperature sensor in communication with said controller and with said thermal cavity for sensing a temperature within said thermal cavity and communicating a signal representative thereof to said controller.
7. The system of claim 1 , wherein each of said engines includes an alternator operably associated therewith for generating electrical energy from mechanical energy produced by said engine, and wherein said system further comprises a controller for controlling each of said engines in a manner to manage the usage of thermal energy collected in said thermal cavity.
8. The system of claim 1 , wherein at least one of said engines comprises a Stirling cycle engine.
9. The system of claim 1 , wherein at least one of said engines comprises a Rankine cycle engine.
10. The system of claim 1 , wherein at least one of said engines comprises a Brayton engine.
11. The system of claim 1 , wherein said plurality of engines are supported by said housing radially about said thermal collection cavity.
12. A power conversion system for converting thermal energy into electrical energy, comprising:
a housing having a thermal cavity for receiving and collecting thermal energy directed into the cavity from an external component;
a plurality of engines disposed in communication with the thermal cavity, the engines being able to use the collected thermal energy to perform work and to generate electrical energy from said work, each of said engines further being supported about said thermal cavity; and
a controller for controlling said engines in a manner to manage the usage of thermal energy collected within said thermal cavity.
13. The system of claim 12 , further comprising a temperature sensor in communication with said thermal cavity and said controller for providing signals to said controller representative of a temperature of said thermal cavity.
14. The system of claim 12 , wherein said controller controls said engines so that efficiency of the engines is optimized.
15. The system of claim 12 , wherein each of said engines includes an alternator, and each of said alternators being responsive to signals from said controller.
16. The system of claim 12 , wherein said engines are supported radially about said thermal cavity.