Rotary internal combustion engine with variable volumetric compression ratio

Patent metadata

Field	Value
Publication number	US-9828906-B2
Application number	US-201615363099-A
Country	US
Kind code	B2
Filing date	Nov 29, 2016
Priority date	Jul 28, 2011
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

A method of controlling an air intake flow in a rotary engine having primary and secondary inlet ports, including positioning the secondary inlet port rearwardly of the primary inlet port and forwardly of the exhaust port along a direction of a revolution of the rotor, and controlling air intake flows communicating between an air source and the primary and secondary inlet ports. During engine start-up, a primary valve is closed to prevent the intake air flow between the primary inlet port and the air source and a secondary valve is opened to allow the intake air flow between the secondary inlet port and the air source. A rotary engine defining different compression ratios through actuation of a valve is also discussed.

First claim

The invention claimed is:

1. A method of controlling an air intake flow 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, a secondary inlet port, a primary valve, a secondary valve and an exhaust port, the secondary inlet port being in communication with the exhaust port through each of the rotating chambers throughout respective portions of a revolution of the rotor, the method comprising:
positioning the secondary inlet port rearwardly of the primary inlet port and forwardly of the exhaust port along a direction of the revolution of the rotor;
controlling air intake flows communicating between an air source and the primary and secondary inlet ports, including:
during engine start-up, closing the primary valve to prevent the intake air flow between the primary inlet port and the air source and opening the secondary valve to allow the intake air flow between the secondary inlet port and the air source.

2. The method as defined in claim 1 , the method further comprising:
allowing the air intake flow between the primary inlet port and the air source by opening the primary valve while modulating the intake air flow between the secondary inlet port and the air source by varying an opening degree of the secondary valve after engine start-up.

3. The method as defined in claim 2 , wherein modulating the intake air flow between the secondary inlet port and the air source after engine start-up includes modulating the secondary valve between a completely closed position and a completely open position.

4. The method as defined in claim 1 , further comprising:
preventing air flow communication between the primary inlet port and the exhaust port throughout each revolution of the rotor.

5. The method as defined in claim 1 , wherein closing the primary valve to prevent the intake air flow between the primary inlet port and the air source and opening the secondary valve to allow the flow 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 rotary engine.

6. The method as defined in claim 2 , wherein allowing the intake air flow between the primary inlet port and the air source includes obtaining a volumetric compression ratio lower than a volumetric expansion ratio of the rotary engine.

7. The method as defined in claim 1 , further comprising, after engine start-up, modulating the intake air flow between the primary inlet port and the air source by varying an opening of the primary valve.

8. The method as defined in claim 1 , wherein the intake air flow between the secondary inlet port and the air source is modulated separately from a fuel flow to the rotating chambers.

9. 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; and
the secondary inlet port communicating with the air source through a valve;
wherein the relative positions of the primary inlet port and the exhaust port define a first volumetric compression ratio of the rotary engine when the valve prevents the communication between the air source and the secondary inlet port; and
wherein the relative positions of the secondary inlet port and the exhaust port define a second volumetric compression ratio higher than the first volumetric compression ratio when the valve is opened allowing the communication between the air source and the secondary inlet port.

10. The engine as defined in claim 9 , wherein the valve is a secondary valve, the primary inlet port communicating with the air source through a primary valve.

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 9 , wherein a position of the secondary inlet port relative to the exhaust port defines the second volumetric compression ratio as at least equal to a volumetric expansion ratio of the rotary engine.

13. The engine as defined in claim 9 , 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 9 , 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 9 , wherein the valve is selected from the group consisting of pneumatic valves, hydraulic valves and electric valves.

16. The engine as defined in claim 9 , 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 9 , wherein the communication of the secondary inlet port with the air source through the valve is separate from of a fuel flow to the rotating chambers.

Assignees

• Pratt & Whitney Canada

Inventors

• Thomassin Jean
• Julien Andre
• Schulz Edwin
• Lanktree Michael

Classifications

• F04C2240/80

  Other components · CPC title

• F04C29/0092

  Removing solid or liquid contaminants from the gas under pumping, e.g. by filtering or deposition; Purging; Scrubbing; Cleaning · CPC title

• F02B53/04

  Charge admission or combustion-gas discharge · CPC title

• F01C21/183

  Arrangements for supercharging the working space (similar arrangements for internal combustion engines F02B33/00, F02B27/00) · CPC title

• F01C21/18

  Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet · CPC title