A Turbocombustion engine for conversation of combustible fuel to rotating energy includes a cylinder, piston, connecting rod and crankshaft system for suction and compression and a rotor for expansion and exhaust. Combustible fuel is compressed within a combustion chamber separate from the cylinder
A Turbocombustion engine for conversation of combustible fuel to rotating energy includes a cylinder, piston, connecting rod and crankshaft system for suction and compression and a rotor for expansion and exhaust. Combustible fuel is compressed within a combustion chamber separate from the cylinder and the combustion force applied directly to the rim of the rotor as in turbines with much larger capacity than the cylinder, converting the entire combustion force at maximum torque to rotating energy. The combustion chamber also includes a variable compression ratio system that constantly adjusts the compression ratio within the combustion chamber for optimum performance of the engine under all variables.
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What I claim is: 1. A turbocombustion engine, comprising: a non-rotational housing having a combustion chamber, and means for compressing air, fuel, or air-fuel mixture to the combustion chamber, the compressing means being separated from the combustion chamber; a rotor disposed to an exterior of s
What I claim is: 1. A turbocombustion engine, comprising: a non-rotational housing having a combustion chamber, and means for compressing air, fuel, or air-fuel mixture to the combustion chamber, the compressing means being separated from the combustion chamber; a rotor disposed to an exterior of said housing and placed to rotate coaxially around the exterior of said housing; and means for allowing a combustion force generated from the combustion chamber to cause the rotor to rotate coaxially around the exterior of said housing. 2. The turbocombustion engine of claim 1 wherein the compressing means is driven by the rotor. 3. The turbocombustion engine of claim 1 wherein the means for allowing a combustion force to the rotor to rotate coaxially around the exterior of said housing comprises means for sealing the combustion chamber when the compressor is delivering air, fuel, or air-fuel mixture to the combustion chamber and opening the combustion chamber to allow the combustion force to rotate the rotor. 4. The turbocombustion engine of claim 1 wherein the rotor includes means for delivering air, fuel, or air-fuel mixture to the compressing means at the same time the combustion force is applied to the rotor to rotate coaxially around the exterior of said housing. 5. The turbocombustion engine of claim 1 wherein the rotor includes means for outputting exhaust from the combustion chamber as delivering air, fuel, or air-fuel mixture to the combustion chamber. 6. The turbocombustion engine of claim 1 further comprising means for adjusting the capacity of the combustion chamber to vary the compression ratio. 7. The turbocombustion engine of claim 1 further comprising means for cooling the turbocombustion engine. 8. A turbocombustion engine comprising; a housing, wherein the housing is non-rotational and comprising a combustion chamber, and a compressor being separated from the combustion chamber, the compressor being configured to deliver air, fuel, or air-fuel mixture to the combustion chamber; and a rotor being to accommodate said housing and rotate coaxially around the exterior of said housing, wherein said rotor is arranged with the combustion chamber so that a combustion force generated from the combustion chamber causes the rotor to rotate coaxially around the exterior of said housing. 9. The turbocombustion engine of claim 8 wherein the compressor is configured to deliver air to the combustion chamber, and the combustion chamber is configured to receive fuel. 10. The turbocombustion engine of claim 8 wherein the compressor comprises a cylinder, a piston, a connecting rod and a crankshaft driven by the rotor, the crankshaft being configured to move the piston in the cylinder to deliver air, fuel, or air-fuel mixture to the combustion chamber. 11. The turbocombustion engine of claim 10 wherein the cylinder is further configured to receive air, fuel or air-fuel mixture, the piston being configured to deliver the cylinder content to the combustion chamber. 12. The turbocombustion engine of claim 11 further comprising a first gear position to rotate with the rotor, a second gear positioned to rotate with the crankshaft, and the first and the second gear are relatively engaged. 13. The turbocombustion engine of claim 11 further comprising a chain, the axle of the crankshaft, and the axle of the rotor are relatively engaged by said chain. 14. The turbocombustion engine of claim 8 further comprising a cap that closes to seal the combustion chamber when the compressor is delivering air, fuel, or air-fuel mixture to the combustion chamber, and opens to allow the combustion force to rotate the rotor coaxially around the exterior of said housing. 15. The turbocombustion engine of claim 14 wherein the cap is opened by the combustion force generated in the combustion chamber and closed by the rotation of the rotor coaxially rotates around the exterior of said housing. 16. The turbocombustion engine of claim 14 wherein the compressor includes a cylinder valve that allows one-way flow of air, fuel, or air-fuel mixture into the compressor during the combustion in the combustion chamber. 17. The turbocombustion engine of claim 16 wherein a cylinder valve is controlled by the cap to allow one-way flow of air, fuel, or air-fuel mixture into the compressor. 18. The turbocombustion engine of claim 16 further comprises a valve support, wherein said valve support is controlled by the cap and positioned to open and close the valve. 19. The turbocombustion engine of claim 18 wherein the valve support is spring loaded. 20. The turbocombustion engine of claim 14 wherein the compressor comprises a crankshaft driven by the rotor, and a cam engaged with the crankshaft, wherein the cam is being configured to control the cap. 21. The turbocombustion engine of claim 20 wherein the compressor includes a cylinder valve that allows one way flow of air, fuel or air-fuel mixture into the compressor during combustion in the combustion chamber, the cylinder valve being controlled by the cam. 22. The turbocombustion engine of claim 21 further comprising a camshaft, the cap and the cylinder valve being controlled by the cam through the camshaft. 23. The turbocombustion engine of claim 8 wherein the rotor includes a channel configured to receive air, fuel or air-fuel mixture and deliver to the compressor as the combustion force is applied to the rotor. 24. The turbocombustion engine of claim 23 wherein the channel is further configured to receive air, fuel or air-fuel mixture the compressor being configured to deliver air, fuel, or air-fuel mixture to the combustion chamber. 25. The turbocombustion engine of claim 23 wherein the compressor comprises a cylinder and a piston configured to move in the cylinder to deliver air, fuel, or air-fuel mixture to the combustion chamber, the capacity of the channel being grater than the capacity of the cylinder. 26. The turbocombustion engine of claim 8 wherein the rotor includes a channel configured to output exhaust from the combustion chamber as the compressor is delivering air, fuel or air-fuel mixture to the combustion chamber. 27. The turbocombustion engine of claim 8 wherein the housing includes an intake port that allows one-way flow of air, fuel or air-fuel mixture into the compressor, an exhaust port that allows one-way flow of exhaust output from the combustion chamber, and a partition separating the intake port from the exhaust port. 28. The turbocombustion engine of claim 8 wherein the capacity of the combustion chamber is adjustable to vary the compression ratio. 29. The turbocombustion engine of claim 28 wherein the combustion chamber includes a cylinder having a piston and wherein the capacity of the combustion chamber is adjusted by moving the piston in the cylinder. 30. The turbocombustion engine of claim 8 wherein the rotor includes a channel configured to deliver air, fuel or air-fuel mixture to the compressor, and output exhaust from the combustion chamber, the rotor and channel are separately structured and configured to engage one another. 31. The turbocombustion engine of claim 8 wherein the rotor includes a channel configured to deliver air, fuel or air-fuel mixture to the compressor, and output exhaust from the combustion chamber, and a lateral seal configured to seal the channel using the centrifugal force generated by the rotating rotor. 32. The turbocombustion engine of claim 31 wherein the seal comprises a seal portion configured to slidably engage the housing, a pivoting portion held in place by the rotor, and a weight portion configured to urge the seal portion toward the housing in response to the centrifugal force generated by rotating rotor. 33. The turbocombustion engine of claim 8 wherein the rotor comprises a plurality of paddles to cool the rotor. 34. The turbocombustion engine of claim 8 wherein the housing includes a plurality of paddles to cool the housing. 35. A turbocombustion engine, comprising: a plurality of units, wherein each of said plurality of units further comprising: a non-rotational housing having a combustion chamber and a compressor being separated from the combustion chamber, wherein the compressor is configured to deliver air, fuel, or air-fuel mixture to the combustion chamber, and a rotor disposed on an outside of said housing to rotate coaxially around the exterior of said housing, wherein said rotor is arranged with the combustion chamber of each of the units so that a combustion force generated in the combustion chamber by each of the units causes the rotor to rotate coaxially around the exterior of said housing. 36. A turbocombustion engine comprising: a rotor; a housing, wherein said housing is non-rotational and includes a cylinder, a combustion chamber separate from the cylinder but in communication with said cylinder, an intake port, an exhaust port and a partition separating the intake port from the exhaust port; said housing further is formed to receive the rotor: a crankshaft rotatively held in place; a connecting rod pivotally attached to said crankshaft; a piston pivotally attached to said connecting rod; wherein said rotor is formed to accommodate to an exterior of said housing and disposed to rotate coaxially on the exterior of said housing at equal rotation with the crankshaft; and a cap pivotally sealed in place to close and open the combustion chamber; wherein said rotor includes a channel that extends to near half of its circumference and formed to accommodate the cap; wherein said cylinder further includes a cylinder valve to allow one-way flow of the channel content to the cylinder; and wherein said combustion chamber further includes a chamber-valve to allow one-way flow of the cylinder content to said combustion chamber.
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