Rotary internal combustion engine with exhaust purge

Patent metadata

Field	Value
Publication number	US-9926842-B2
Application number	US-201414549783-A
Country	US
Kind code	B2
Filing date	Nov 21, 2014
Priority date	Jul 28, 2011
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

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.

First claim

The invention claimed is:

1. 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.

2. The engine as defined in claim 1 , wherein the engine is a Wankel engine, with the stator body 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, each of the apex portions remaining in sealing engagement with a peripheral one of the stator walls and separating the chambers.

3. The engine as defined in claim 1 , wherein the inlet port and purge port are in communication with the air source through a common intake duct.

4. The engine as defined in claim 1 , wherein the purge port is defined by a purge line forming a communication with an adjacent one of the chambers, the adjacent one of the chambers being in communication with the inlet port.

5. The engine as defined in claim 1 , wherein the exhaust port is a primary exhaust port, the stator body having a secondary exhaust port defined therein in proximity of the primary exhaust port with the secondary exhaust port being located forwardly of the primary exhaust port and rearwardly of the purge port along the direction of the eccentric revolutions, the rotor also preventing communication between the purge port and the primary exhaust port in all rotor positions.

6. The engine as defined in claim 1 , wherein the purge port communicates with the air source through a valve.

7. 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.

8. The engine as defined in claim 7 , wherein the rotary engine is a Wankel engine, with the stator body 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, the rotor performing 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 the chambers.

9. The engine as defined in claim 7 , wherein the primary and secondary inlet ports are in communication with the compressor through a common intake duct.

10. The engine as defined in claim 7 , wherein the secondary inlet port is defined by a purge line forming a communication with an adjacent one of the chambers, the adjacent one of the chambers being in communication with the primary inlet port.

11. The engine as defined in claim 7 , wherein the exhaust port is a primary exhaust port, the stator body having a secondary exhaust port defined therein in proximity of the primary exhaust port with the secondary exhaust port being located forwardly of the primary exhaust port and rearwardly of the secondary inlet port along the direction of the eccentric revolutions, and for each of the chambers, each of the eccentric revolutions of the rotor includes a primary exhaust portion where the chamber contains the primary exhaust port, the primary exhaust portion and the purge portions being non-overlapping.

12. The engine as defined in claim 7 , wherein the secondary inlet port communicates with the compressor through a valve.

13. 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.

14. The method as defined in claim 13 , further comprising, after the purging of the combustion gases, closing a communication of the chamber with the secondary exhaust port prior to filling the chamber with air through the inlet port.

15. The method as defined in claim 13 , wherein the purging of the combustion gases includes circulating the air from an air source through a duct also communicating with the inlet port.

16. The method as defined in claim 13 , wherein the purging of the combustion gases includes circulating the air through a conduit communicating with an adjacent chamber of the engine receiving the air from the inlet port.

17. The method as defined in claim 13 , wherein the purging of the combustion gases includes opening a valve regulating a communication between the purge port and an air source.

Assignees

• Pratt & Whitney Canada

Inventors

• Fontaine Mike
• Julien Andre
• Thomassin Jean

Classifications

• F04C2/12

  of other than internal-axis type · CPC title

• F01C11/006

  of dissimilar working principle · CPC title

• F04C2240/80

  Other components · CPC title

• F01C21/08

  Rotary pistons (reciprocating pistons in general F16J) · CPC title

• Y10S60/901

  Exhaust treatment special to rotary internal combustion engines · CPC title