The present invention relates to a rotary-style internal combustion power-plant, and an electric machine, comprising a compressor housing, wherein a compressor is housed, a electric machine housing, located adjacent to the compressor housing, wherein an electric machine is housed, a charge air coole
The present invention relates to a rotary-style internal combustion power-plant, and an electric machine, comprising a compressor housing, wherein a compressor is housed, a electric machine housing, located adjacent to the compressor housing, wherein an electric machine is housed, a charge air cooler housing, located adjacent to the electric machine housing, a combustion rotor housing located adjacent to the charge air cooler housing, a power take-off housing located adjacent to the combustion rotor housing, a combustion rotor located adjacent to a power take-off housing, an auxiliary pump housing (oil, coolant, and fuel) located adjacent to the combustion rotor; and turbine housing located adjacent to the auxiliary pump housing (oil and coolant), wherein the housings are manufactured as separate entities and are stacked along a singled axis.
대표청구항▼
1. An internal combustion power-plant, comprising: a combustion rotor housing provided with a combustion chamber bore and an axis, a combustion rotor provided with an axis, and a crankshaft provided with a lobe, an aperture, and an axis, the lobe provided with an axis spaced from the axis of the com
1. An internal combustion power-plant, comprising: a combustion rotor housing provided with a combustion chamber bore and an axis, a combustion rotor provided with an axis, and a crankshaft provided with a lobe, an aperture, and an axis, the lobe provided with an axis spaced from the axis of the combustion rotor housing, wherein the axis of the combustion chamber and the axis of the crankshaft are co-axial, and the combustion rotor axis and the lobe axis are co-axial;a compressor-turbine shaft extending through the aperture of the crankshaft, the compressor-turbine shaft includes a first end and a second end, a compressor wheel provided with a plurality of compressor fins, a turbine wheel provided with a plurality of turbine fins, and an axis about which the compressor-turbine shaft rotates, wherein the compressor wheel is located at the first end of the compressor-turbine shaft and the turbine wheel is located at the second end of the turbine shaft; anda compressor housing and a turbine housing, the compressor wheel located within the compressor housing and the turbine wheel located within the turbine housing, wherein the compressor-turbine shaft is coaxial with the crankshaft and the combustion rotor housing, and wherein the crankshaft and compressor-turbine shaft are uncoupled and rotate independently. 2. The internal combustion power-plant of claim 1, further comprising: a bearing surface on the compressor-turbine shaft, the bearing surface located between the first end of the compressor-turbine shaft and the second end of the compressor-turbine shaft. 3. The internal combustion power-plant of claim 2, further comprising: a groove positioned on the bearing surface of the compressor-turbine shaft. 4. The internal combustion power-plant of claim 1, further comprising: sprocket gear positioned on the crankshaft, the sprocket gear is provided with an axis that is co-axial with the compressor-turbine shaft and the crankshaft. 5. The internal combustion power-plant of claim 1, further comprising: an output port positioned on the compressor housing and an intake port positioned on the combustion rotor housing, wherein an intake charge passageway connects the output port with the intake port; andan exhaust port positioned on the combustion rotor housing and an turbine input port located on the turbine housing, wherein an exhaust passage way connects the exhaust port and the turbine input port. 6. The internal combustion power-plant of claim 5, further comprising: a bearing surface on the compressor-turbine shaft, the bearing surface located between the first end of the compressor-turbine shaft and the second end of the compressor-turbine shaft. 7. The internal combustion power-plant of claim 6, further comprising: a groove positioned on the bearing surface of the compressor-turbine shaft. 8. The internal combustion power-plant of claim 6, further comprising: an output port positioned the turbine housing, wherein exhaust gas is discharged through the output port. 9. A rotary-style internal combustion power-plant comprising: a combustion rotor housing provided with an epitrochoid-shaped combustion chamber bore and an axis, a three-sided combustion rotor provided with an axis, a crankshaft provided with an axis, an aperture, and a lobe, the lobe provided with an axis parallel to, and offset from, the crankshaft axis, wherein the lobe axis is co-axial with the combustion rotor axis, and the axis of the combustion chamber and the axis of the crankshaft are co-axial;a compressor-turbine-shaft within the aperture of the crankshaft, the compressor-turbine shaft includes a first end and a second end, a compressor wheel provided with a plurality of compressor fins, a turbine wheel provided with a plurality of turbine fins, and an axis about which the compressor-turbine shaft rotates, wherein the compressor wheel is located at the first end of the compressor-turbine shaft and the turbine wheel is located at the second end of the turbine shaft; anda compressor housing and a turbine housing, the compressor wheel located within the compressor housing and the turbine wheel located within the turbine housing, wherein the compressor-turbine shaft is coaxial with the crankshaft and the combustion rotor housing, and wherein the crankshaft and compressor-turbine shaft are uncoupled and rotate independently. 10. The rotary-style internal combustion power-plant of claim 9, further comprising: a bearing surface on the compressor-turbine shaft, the bearing surface located between the first end of the compressor-turbine shaft and the second end of the compressor-turbine shaft. 11. The rotary-style internal combustion power-plant of claim 10, further comprising: a groove positioned on the bearing surface of the compressor-turbine shaft. 12. The rotary-style internal combustion power-plant of claim 9, further comprising: a sprocket gear positioned on the crankshaft, the sprocket gear is provided with an axis that is co-axial with the compressor-turbine shaft and the crankshaft. 13. The rotary-style internal combustion power-plant of claim 9, further comprising: an output port positioned on the compressor housing and an intake port positioned on the combustion rotor housing, wherein an intake charge passageway connects the output port with the intake port; andan exhaust port positioned on the combustion rotor housing and an turbine input port located on the turbine housing, wherein an exhaust passage way connects the exhaust port and the turbine input port. 14. The rotary-style internal combustion power-plant of claim 13, further comprising: a bearing surface on the compressor-turbine shaft, the bearing surface located between the first end of the compressor-turbine shaft and the second end of the compressor-turbine shaft. 15. The rotary-style internal combustion power-plant of claim 14, further comprising: a groove positioned on the bearing surface of the compressor-turbine shaft. 16. The rotary-style internal combustion power-plant of claim 15, further comprising: an output port positioned the turbine housing, wherein exhaust gas is discharged through the output port. 17. A rotary-style power-plant, comprising: a combustion rotor housing provided with a combustion chamber bore and an axis;a combustion rotor provided with an axis; a crankshaft provided with a lobe, an aperture, and an axis, the lobe provided with an axis spaced from the crankshaft axis, wherein the crankshaft and the combustion chamber bore are co-axial, and the combustion rotor and the lobe are co-axial;a sprocket gear, the sprocket gear is positioned coaxially with the crankshaft;a compressor-turbine shaft extending through the aperture of the crankshaft, the compressor-turbine shaft includes a first end, a second end, and a bearing surface;a compressor wheel provided with a plurality of compressor fins and an axis about which the compressor wheel rotates;a turbine wheel provided with a plurality of turbine fins and an axis about which the compressor-turbine shaft rotates, wherein the compressor wheel is located at the first end of the compressor-turbine shaft and the turbine wheel is located at the second end of the compressor-turbine shaft;a compressor housing, the compressor wheel located within the compressor housing;a turbine housing, the turbine wheel located within the turbine housing, wherein the compressor-turbine shaft is coaxial with the crankshaft and the combustion rotor housing; anda power takeoff housing, the sprocket gear is located within the power takeoff housing, wherein the crankshaft and compressor-turbine shaft are uncoupled and rotate independently. 18. A rotary-style power-plant of claim 17, further comprising: a groove positioned on the bearing surface of the compressor-turbine shaft. 19. A rotary-style power-plant of claim 17, wherein the sprocket gear is positioned on the crankshaft. 20. A rotary-style power-plant of claim 17, further comprising: an output port positioned on the compressor housing and an intake port positioned on the combustion rotor housing, wherein an intake charge passageway connects the output port with the intake port; andan exhaust port positioned on the combustion rotor housing and an turbine input port located on the turbine housing, wherein an exhaust passage way connects the exhaust port and the turbine input port.
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이 특허에 인용된 특허 (14)
Whurr John (Derby GB2), Aircraft compound cycle propulsion engine.
Plante, Jean-Sebastien; Rancourt, David; Picard, Mathieu, Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall.
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