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A method and apparatus for controlling an air input in a rotary engine, including selectively controlling a plurality of inlet ports communicating with an internal combustion cavity of the engine, the ports located serially downstream of the exhaust port relative direction of a revolution of a rotor

A method and apparatus for controlling an air input in a rotary engine, including selectively controlling a plurality of inlet ports communicating with an internal combustion cavity of the engine, the ports located serially downstream of the exhaust port relative direction of a revolution of a rotor of the engine. The inlet ports are controlled to alter air intake at various engine operational stages, such as start up, idle, etc., to allow for varying operational requirements to be met. For example: when a power demand on the engine lower than a predetermined threshold, control may be effected by opening a primary inlet port and closing a secondary inlet port; and, when the power demand exceeds the predetermined threshold, control may be effected by opening the primary inlet port and opening the secondary inlet port, the secondary inlet port being located such as to be in communication with the exhaust port throughout portions of the revolution of the engine to purge exhaust gases of the engine.

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1. A method of controlling an air input in a rotary engine having a rotor received in an internal cavity of a housing and defining rotating chambers with variable volume, the rotary engine having a primary inlet port, an exhaust port, and a secondary inlet port, the secondary inlet port being in com

1. A method of controlling an air input in a rotary engine having a rotor received in an internal cavity of a housing and defining rotating chambers with variable volume, the rotary engine having a primary inlet port, an exhaust port, and a secondary inlet port, the secondary inlet port being in communication with the exhaust port through each of the rotating chambers throughout respective portions of the revolution of the rotor, the method comprising: controlling a communication between an air source and the secondary inlet ports while the primary inlet port communicates with the air source, including modulating a flow of the communication between the secondary inlet port and the air source by varying an opening of a valve through which the communication between the secondary inlet port and the air source is performed;wherein the secondary inlet port is located rearwardly of the primary inlet port and forwardly of the exhaust port thereof along a direction of a revolution of the rotor. 2. The method as defined in claim 1, wherein modulating the flow of the communication between the secondary inlet port and the air source includes modulating the flow between a first configuration where the valve is closed and the communication between the secondary inlet port and the air source is prevented, and a second configuration where the valve is completely open. 3. The method as defined in claim 1, wherein controlling the communication between the air source and the secondary inlet port while the primary inlet port communicates with the air source is performed after start-up of the engine, the method further comprising, during start-up of the engine, closing the communication between the primary inlet port and the air source outside of the internal cavity and opening the valve to allow the communication between the secondary inlet port and the air source. 4. The method as defined in claim 3, wherein closing the communication between the primary inlet port and the air source and allowing the communication between the secondary inlet port and the air source includes obtaining a volumetric compression ratio at least equal to a volumetric expansion ratio of the engine. 5. The method as defined in claim 1, including preventing communication between the primary inlet port and the exhaust port throughout each revolution of the rotor. 6. The method as defined in claim 1, including obtaining a volumetric compression ratio lower than a volumetric expansion ratio of the engine. 7. The method as defined in claim 1, further comprising controlling the communication between the air source and the primary inlet port, including modulating a flow of the communication between the primary inlet port and the air source, the flow between the primary inlet port and the air source being modulated by varying an opening of a primary valve through which the communication between the primary inlet port and the air source is performed. 8. The method as defined in claim 7, wherein the valve is a secondary valve, the method further comprising, during start-up of the engine, closing the primary valve to close the communication between the primary inlet port and the air source while opening the secondary valve to allow the communication between the secondary valve and the air source. 9. The method as defined in claim 1, wherein the flow of the communication between the secondary inlet port and the air source is modulated separately from a fuel flow to the rotating chambers. 10. A rotary engine comprising: a rotor body mounted for eccentric revolutions within a stator body to provide rotating chambers of variable volume in an internal cavity of the stator body;the stator body having at least a primary inlet port, a secondary inlet port and an exhaust port defined therein and communicating with the internal cavity, the secondary inlet port being located rearwardly of the primary inlet port and forwardly of the exhaust port along a direction of revolutions of the rotor body, the primary and secondary inlet ports being distinct from one another and spaced apart along the direction of the revolutions;the primary inlet port communicating with an air source through a primary valve; andthe secondary inlet port communicating with the air source through a secondary valve;wherein the relative positions of the primary inlet port and the exhaust port define a first volumetric compression ratio of the engine lower than a volumetric expansion ratio of the engine when the secondary valve prevents the communication between the air source and the secondary inlet port and the primary valve allows the communication between the air source and the primary net port; andwherein the relative position of the secondary inlet port and the exhaust port defines a second volumetric compression ratio higher than the first volumetric compression ratio when the primary valve prevents the communication between the air source and the primary inlet port and the secondary valve allows the communication between the air source and the secondary inlet port. 11. The engine as defined in claim 10, wherein the primary and secondary valves are operable independently of one another. 12. The engine as defined in claim 10, wherein the relative positions of the secondary inlet port and the exhaust port define the second volumetric compression ratio as at least substantially equal to the volumetric expansion ratio when the primary valve prevents the communication between the air source and the primary inlet port and the secondary valve allows the communication between the air source and the secondary inlet port. 13. The engine as defined in claim 10, wherein the secondary inlet port is located relative to the exhaust port so as to be in momentary communication with the exhaust port through each of the rotating chambers along a respective portion of each revolution of the rotor body. 14. The engine as defined in claim 10, wherein the rotor is configured and the primary inlet port and the exhaust port are located to prevent communication between the primary inlet port and the exhaust port through the rotating chambers in any rotor position. 15. The engine as defined in claim 10, wherein the secondary valve is selected from the group consisting of pneumatic valves, hydraulic valves and electric valves. 16. The engine as defined in claim 10, wherein the engine is a Wankel engine, with the stator body having walls defining the internal cavity having an epitrochoid shape with two lobes, and the rotor body having three circumferentially spaced apex portions, the rotor body being engaged to an eccentric portion of a shaft to perform orbital revolutions within the internal cavity with each of the apex portions remaining in sealing engagement with a peripheral one of the stator walls and separating three rotating chambers defined in the internal cavity around the rotor body. 17. The engine as defined in claim 10, wherein the communication of the secondary inlet port with the air source through the secondary valve is separate from of a fuel flow to the rotating chambers.