Rotary internal combustion engine with exhaust purge
AssigneePratt & Whitney Canada Corp.
InventorsMike Fontaine, Andre Julien, Jean Thomassin
Life of this patent
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Abstract
In one aspect, described is a rotary engine having a purge port located rearwardly of the inlet port and forwardly of the exhaust port along a direction of the revolutions of the rotor, the purge port being in communication with the exhaust port through each of the chambers along a respective portion of each revolution, and the inlet and outlet ports being relatively located such that a volumetric compression ratio of the engine is lower than a volumetric expansion ratio of the engine.
Claims17
A rotary engine comprising:
- a stator body having walls defining an internal cavity;
- a rotor body mounted for eccentric revolutions within the internal cavity, the rotor and stator bodies cooperating to provide chambers of variable volume when the rotor body moves relative to the stator body;
- at least an inlet port, an exhaust port and a purge port defined in the stator body and communicating with the cavity, the inlet port and purge port being in communication with an air source, the purge port being located rearwardly of the inlet port and forwardly of the exhaust port relative to a direction of the eccentric revolutions of the rotor body;
- wherein the purge port momentarily communicates with the exhaust port through each of the chambers when the rotor body is positioned in a respective portion of each of the revolutions of the rotor body;
- and
- wherein the inlet and exhaust ports are located relative to one another such that the rotor body prevents communication between the inlet and exhaust ports throughout the eccentric revolutions of the rotor body.
A compound engine system comprising:
- a compressor;
- a turbine;
- and
- a rotary engine, the rotary engine including:
- a stator body having walls defining an internal cavity,
- a rotor body mounted for eccentric revolutions within the cavity, the rotor and stator bodies cooperating to provide chambers of variable volume when the rotor moves relative to the stator,
- spaced apart primary and secondary inlet ports and an exhaust port defined in the stator body and communicating with the internal cavity, the primary and secondary inlet ports communicating with the compressor and the exhaust port communicating with the turbine, the secondary inlet port being located rearwardly of the primary inlet port and forwardly of the exhaust port relative to a direction of the eccentric revolutions;
- wherein for each of the chambers, each of the eccentric revolutions of the rotor body includes an exhaust portion where the chamber contains the exhaust port, a purge portion being part of the exhaust portion where the chamber contains both the secondary inlet port and the exhaust port, and a primary intake portion where the chamber contains the primary inlet port, the exhaust portion and the primary intake portion being non-overlapping such that the rotor body prevents communication between the inlet and exhaust ports through the chambers in any rotor position.
A method of operating a rotary engine, the method comprising, through each orbital revolution and rotary motion of a rotor of the engine and for each chamber thereof:
- filling the chamber with air through an inlet port;
- compressing the air by reducing a volume of the chamber;
- mixing the compressed air with fuel and combusting a resulting air-fuel mixture;
- expanding combustion gases from the combustion by increasing a volume of the chamber;
- expulsing the combustion gases through a primary exhaust port;
- closing a communication of the chamber with the primary exhaust port;
- and
- purging the combustion gases through a secondary exhaust port distinct from the primary exhaust port with air entering the chamber through a purge port distinct and spaced apart from the inlet port.
Dependencies are inferred from the claim text.