초록 ▼

A fuel system for improved fuel efficiency may include a fuel injector to transmit fuel in droplet form to a reaction region. A reaction rod may be positioned in the reaction region, where the reaction rod may have a convex end and a concave end. The fuel system may be used with engines such as gaso

A fuel system for improved fuel efficiency may include a fuel injector to transmit fuel in droplet form to a reaction region. A reaction rod may be positioned in the reaction region, where the reaction rod may have a convex end and a concave end. The fuel system may be used with engines such as gasoline engines, turbine engines, diesel engines, and steam engines.

대표청구항 ▼

What is claimed is: 1. A combustion system, comprising: an injection block, including a first region, defining a conduit for air flow, a second region, including a source of fuel, and an injector that converts the fuel to fuel droplets, and a third region, in which the air and fuel are mixed; a cha

What is claimed is: 1. A combustion system, comprising: an injection block, including a first region, defining a conduit for air flow, a second region, including a source of fuel, and an injector that converts the fuel to fuel droplets, and a third region, in which the air and fuel are mixed; a chamber, coupled to an outlet of said injection block, and receiving the mixed fuel droplets and air from said injection block; a vacuum production part, coupled to said chamber, and maintaining said chamber under vacuum; a chamber area reducing part, within said chamber, and reducing an area of said reducing part to accelerate the mixed fuel droplets and air in said area; and a combustion device, receiving fuel that has passed through said reducing part, and producing an exhaust gas; and an exhaust area couple to receive said exhaust gas, and coupling said exhaust gas to an outer surface of said chamber. 2. A combustion system as in claim 1, wherein said chamber is located coaxially within an exhaust pipe that carries said exhaust gas. 3. A combustion system as in claim 2, wherein said chamber is formed within a pipe, and said pipe is formed of a material capable of accepting a magnetic signature. 4. A combustion system as in claim 3 , further comprising a fuel pipe, carrying fuel to said second region of said injection block, wherein said pipe is formed of all non-magnetic material. 5. A combustion system as in claim 4, wherein said fuel pipe is made of copper. 6. A combustion system as in claim 1, wherein said injection block has a first direction in which the air and fuel mixture are passed to said chamber, wherein said air is introduced in a direction that is parallel to said first direction. 7. A combustion system as in claim 6, wherein said fuel is introduced in a direction that is not parallel to said first direction, but is that less than a 90�� angle to said first direction. 8. A combustion system as in claim 7, wherein said fuel is introduced from both a first side and a second side, and wherein both said first side and said second side are at equal but opposite angles relative to said direction of said air. 9. A combustion system as in claim 1, further comprising a pipe carrying air to said conduit for airflow, said pipe including a suction hose. 10. A combustion system, comprising: a fuel injection block, including a first portion connected to receive air, and second and third portions, connected to receive fuel, and including fuel injectors therein of a type which convert the fuel to droplets, said second and third portions being symmetrically disposed relative to said first portion, said fuel injection block having an outlet; a reaction chamber, receiving the mixed air and fuel droplet portions from said fuel injection block, said reaction chamber having an outer surface which is heated to be hotter then a temperature of said fuel, and an inner surface which is cooled to cool said fuel; said reaction chamber further having an inner surface with a surface area that is reduced in an area of said cooling, and having a shape which causes minimal interruptions to laminar flow at a beginning end of said reduced surface area, and maximum disruptions to outer flow at an area of an ending end of said reduced surface area; a combustion device receiving fuel that has passed through said reaction chamber, and combusting said fuel to produce a heated exhaust gas; and wherein said heated exhaust gas is used to heat said outer surface of said reaction chamber. 11. A combustion system as in claim 10, wherein said fuel injectors are atomizers that atomize the input fuel. 12. A combustion system as in claim 10, wherein said fuel injectors form misting nozzles that form mist from the input fuel. 13. A combustion system as in claim 10, further comprising an exhaust pipe, carrying said heated exhaust gas, and wherein said reaction chamber is formed as a pipe that is coaxially within said exhaust pipe. 14. A combustion system as in claim 13, wherein said reaction chamber is formed within a pipe formed of a material capable of accepting a magnetic signature. 15. A combustion system as in claim 14, wherein said second and third portions are connected to pipes which provide fuel, and said pipes which provide fuel are formed of a material that is not capable of accepting a magnetic signature. 16. A combustion system as in claim 15, wherein said pipes which provide fuel are formed of copper. 17. A combustion system as in claim 10, wherein said inner surface of said combustion chamber includes a reaction rod having a convex end facing towards a fuel delivery direction, and a concave facing away from the fuel delivery direction. 18. A combustion system as in claim 17, wherein said reaction chamber is formed in the inside of a pipe, and said reaction rod is within said pipe, and forms a clearance between said reaction rod and said pipe of approximately 0.012 inches. 19. A method, comprising: introducing both fuel and air into a mixing chamber, one of the fuel and air being introduced from a first direction, and the other of fuel and air being introduced from a second direction, said introducing forming droplets of fuel in said mixing chamber; mixing said droplets of fuel with said air in said mixing chamber; introducing said mixed fuel and air to a reaction chamber, which is within a pipe that is capable of forming a magnetic signature, has an outer surface which is heated, and has an inner surface which is cooled; and using fuel which has passed through said reaction chamber for a combustion process, and using an exhaust gas from said combustion process to heat said outer surface of said reaction chamber. 20. A method as in claim 19, wherein said inner surface which is cooled is formed by an area with an obstruction inside said inner surface, and a vacuum applied to said inner surface.