Electrical generator system

• US 7,378,749 B2
• Filed: 10/26/2005
• Issued: 05/27/2008
• Est. Priority Date: 10/26/2005
• Status: Expired due to Fees

• Current Assignee: Donald O. Moore
• Original Assignee: Donald O. Moore
• Inventors: Moore, Donald O.
• Primary Examiner(s): Schuberg; Darren
• Assistant Examiner(s): Cuevas; Pedro J.
• Application Number:
  US11/258,705
• Publication Number:
  US 20070090649A1
• Time in Patent Office: 944 Days
• Field of Search: 290/2, 310/181
• US Class Current: 290/2
• CPC Class Codes: F01N 5/025 the device being thermoelectric generators
• CPC Class Codes: F02C 6/18 using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants using waste heat as source of energy for refrigeration plants F25B27/02; using the waste heat of a gasturbine for steam generation or in a steam cycle see F01K23/10
• CPC Class Codes: H02K 99/10 Generators

Abstract

An electrical generator system includes a source for producing heated gases, a conduit connected to the source for receiving a flow of the heated gases, and a generator assembly positioned in close proximity to the conduit. The generator assembly includes a plurality of magnets positioned in a spaced relationship, the plurality of magnets producing a magnetic field. At least one electrical conductor is positioned adjacent the plurality of magnets to conduct an electrical current generated in response to the flow of heated gases in the conduit and the magnetic field.

Claims

1. An electrical generator system, comprising:

an internal combustion engine for producing heated ionized combustion gases;

a conduit connected to said internal combustion engine for receiving a flow of said heated ionized combustion gases; and

a generator assembly positioned in close proximity to said conduit, said generator assembly including;

a plurality of magnets positioned in a spaced relationship, said plurality of magnets producing a magnetic field; and

at least one pair of electrodes positioned inside said conduit adjacent to said plurality of magnets to conduct an electrical current generated in response to said flow of heated ionized combustion gases in said conduit from said magnetic field, wherein said at least one pair of electrodes or a plurality of pairs of electrodes are alternatingly interposed between adjacent pairs of magnets of said plurality of magnets.

2. The electrical generator system of claim 1, wherein said plurality of magnets is positioned in a spaced relationship along a periphery of said conduit.

3. The electrical generator system of claim 1, wherein said at least one pair of electrodes includes a pair of separated copper plates forming a housing around said plurality of magnets.

4. The electrical generator system of claim 1, wherein said generator assembly is configured as a plurality of copper clad ceramic magnets that are positioned to be exposed to at least one of heat and particle flow produced by said heated ionized combustion gases.

5. The electrical generator system of claim 1, wherein said heated ionized combustion gases are exhaust gases produced by said internal combustion engine.

6. The electrical generator system of claim 5, wherein said generator assembly is located in one of a land vehicle, a watercraft and an aircraft.

7. The electrical generator system of claim 5, wherein said conduit includes an exhaust pipe connected in fluid communication with said internal combustion engine, wherein said plurality of magnets are positioned in a spaced relationship around a periphery of said exhaust pipe.

8. The electrical generator system of claim 5, wherein said conduit includes a muffler connected in fluid communication with said internal combustion engine, wherein said generator assembly is housed inside said muffler.

9. The electrical generator system of claim 8, further comprising a plurality of said generator assemblies, said plurality of said generator assemblies being housed inside said muffler.

10. The electrical generator system of claim 8, wherein said at least one pair of electrodes includes a plurality of copper disks alternatingly interposed between adjacent pairs of said plurality of magnets.

11. The electrical generator system of claim 5, further comprising a plurality of said generator assemblies, wherein said plurality of said generator assemblies are arranged inside said conduit in a manner to muffle sound produced by said internal combustion engine.

12. The generator system of claim 1, wherein each of said plurality of magnets has a plurality of faces that are exposed to a particle flow.

13. A generator assembly, comprising:

a tubular housing configured to be positioned in close proximity to a flow of heated ionized combustion gases;

a plurality of magnets positioned in a spaced relationship along said tubular housing, said plurality of magnets producing a magnetic field; and

at least one pair of electrodes positioned adjacent said plurality of magnets to conduct an electrical current generated in response to said flow of heated ionized combustion gases and said magnetic field, wherein said at least one pair of electrodes is interposed between an adjacent pair of magnets of said plurality of magnets, wherein said at least one pair of electrodes or plurality of pair of electrodes are alternatingly interposed between adjacent pairs of magnets of said plurality of magnets.

14. The generator assembly of claim 13, wherein said plurality of magnets are positioned in a spaced relationship along a periphery of a conduit.

15. The generator assembly of claim 13, wherein said at least one pair of electrodes includes a pair of separated copper plates forming a housing around said plurality of magnets.

16. The generator assembly of claim 13, wherein said generator assembly is configured as a plurality of copper clad ceramic magnets that are positioned to be exposed to at least one of heat and particle flow produced by said heated ionized combustion gases.

17. The generator assembly of claim 13, wherein said generator assembly is located in one of a land vehicle, a watercraft and an aircraft.

18. The generator assembly of claim 13, wherein each of said plurality of magnets has a plurality of faces that are exposed to a particle flow.