Rotary internal combustion engine with pilot subchamber and ignition element

• US 9,334,794 B2
• Filed: 06/05/2013
• Issued: 05/10/2016
• Est. Priority Date: 06/05/2013
• Status: Active Grant

• Current Assignee: Pratt & Whitney Canada Corporation (Rtx Corporation)
• Original Assignee: Pratt & Whitney Canada Corporation (Rtx Corporation)
• Inventors: Gaul, Michael, Julien, Andr, Villeneuve, Bruno
• Primary Examiner(s): Pereiro, Jorge
• Assistant Examiner(s): NEWTON, JASON TODD
• Application Number:
  US13/910,807
• Publication Number:
  US 20140360456A1
• Time in Patent Office: 1,070 Days
• Field of Search: 60/396, 60/366.2, 60/396.3, 60/396.4, 123/200, 123/205, 123/207, 123/208, 123/209, 123/210, 123/212, 123/214, 123/218, 123/231, 123/243, 123/273, 123/275, 123/284, 123/445
• US Class Current: 1/1
• CPC Class Codes: F01C 1/22 of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member
• CPC Class Codes: F02B 19/108 with fuel injection at least into pre-combustion chamber, i.e. injector mounted directly in the pre-combustion chamber
• CPC Class Codes: F02B 19/12 with positive ignition engines with non-timed positive ignition, and with incandescent chambers F02B9/08
• CPC Class Codes: F02B 2053/005 Wankel engines
• CPC Class Codes: F02B 53/02 Methods of operating
• CPC Class Codes: F02B 53/10 Fuel supply; Introducing fuel to combustion space
• CPC Class Codes: F02B 53/12 Ignition
• CPC Class Codes: F02B 55/08 Outer members for co-operation with rotary pistons; Casings
• CPC Class Codes: F02B 55/14 Shapes or constructions of combustion chambers
• CPC Class Codes: F02M 53/02 with fuel-heating means, e.g. for vaporising
• CPC Class Codes: F02P 19/02 electric, e.g. layout of circuits of apparatus having glowing plugs
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A rotary engine including an insert in one of the walls of the outer body having a pilot subchamber defined therein communicating with the internal cavity of the engine. An ignition element extends in an element cavity defined through the insert adjacent the subchamber. A portion of the element is in communication with the subchamber through a communication opening defined in the insert between the element cavity and the subchamber. The communication opening has a cross-section smaller than a corresponding cross-section of the portion of the element. An outer body for a rotary engine and a method of combusting fuel in a rotary engine are also provided.

Claims

1. A rotary engine comprising:

an outer body having a plurality of interconnected walls defining an internal cavity;

a rotor body rotatable within the internal cavity in sealing engagement with the plurality of interconnected walls of the outer body and defining at least one chamber of variable volume in the internal cavity around the rotor body;

an insert in one of the plurality of interconnected walls of the outer body, the insert having a pilot subchamber defined therein communicating with the internal cavity;

a main fuel injector having a tip in communication with the internal cavity at a location spaced apart from the insert;

a pilot fuel injector having a tip in communication with the pilot subchamber; and

an ignition element extending into an element cavity defined through the insert adjacent the pilot subchamber, a central longitudinal axis of the ignition element extending through the insert without passing through the subchamber, the element cavity being in communication with the pilot subchamber through a communication opening defined in the insert between the element cavity and the pilot subchamber, the communication opening being smaller than a portion of the ignition element received in the insert in the element cavity adjacent the communication opening to prevent the portion of the ignition element from completely passing through the communication opening.

2. The engine as defined in claim 1, wherein the portion of the ignition element includes a tip thereof partly received through the communication opening.

3. The engine as defined in claim 1, wherein the portion of the ignition element is cylindrical and a circumferential part thereof extends within the pilot subchamber through the communication opening.

4. The engine as defined in claim 1, wherein the insert is made of a material having one or both of greater high temperature properties and lower thermal conductivity than that of the one of the plurality of interconnected walls.

5. The engine as defined in claim 1, wherein the ignition element is a heating element and the portion of the ignition element is heatable.

6. The engine as defined in claim 1, wherein the pilot subchamber has a shape forming a reduced cross-section adjacent the communication thereof with the internal cavity.

7. The rotary engine as defined in claim 1, wherein the ignition element is elongated and extends within the element cavity without protruding into the pilot subchamber.

8. The rotary engine as defined in claim 1, wherein the rotor body defines three apex portions and is engaged to an eccentric portion of a shaft to rotate and perform orbital revolutions within the internal cavity, the internal cavity having an epichotroid shape defining two lobes.

9. An outer body for a rotary engine comprising:

two axially spaced apart end walls;

a peripheral wall extending between the end walls and defining an internal cavity therewith for receiving a rotor therein;

an insert in the peripheral wall of the outer body, the insert having a subchamber defined therein in communication with the internal cavity;

the outer body further having;

a pilot injector hole defined therethrough in communication with the subchamber and sized to receive a pilot fuel injector, and

a main fuel injector hole defined therethrough in communication with the internal cavity, spaced apart from the insert and sized to receive a main fuel injector; and

an ignition element received in the insert, a central longitudinal axis of the ignition element extending through the insert without passing through the subchamber, the ignition element in communication with the subchamber through an opening sized to prevent a portion of the ignition element extending in the insert adjacent the opening from completely passing through the opening.

10. The outer body as defined in claim 9, wherein the portion of the ignition element includes a tip thereof partly received through the opening.

11. The outer body as defined in claim 9, wherein the portion of the ignition element is cylindrical and a circumferential part thereof extends within the subchamber through the communication opening.

12. The outer body as defined in claim 9, wherein the insert is made of a material having one or both of greater high temperature properties and lower thermal conductivity than that of the peripheral wall.

13. The outer body as defined in claim 9, wherein the ignition element is a heating element and the portion of the ignition element is heatable.

14. The outer body as defined in claim 9, wherein the subchamber has a shape forming a reduced cross-section adjacent the communication thereof with the internal cavity.

15. The outer body as defined in claim 9, wherein the element is elongated and extends within the insert without protruding into the subchamber.

16. A method of combusting fuel in a rotary engine having a rotor rotating in a cavity, the method comprising:

injecting a minor portion of the fuel into a subchamber defined in an insert located in a peripheral wall of the engine;

activating a portion of an ignition element received in the insert, a central longitudinal axis of the ignition element extending through the insert without passing through the subchamber, the portion of the ignition element being located adjacent a communication opening defined through the insert and communicating with the subchamber, the communication opening being sized to prevent the portion of the ignition element from completely passing therethrough;

exposing the portion of the ignition element to the minor portion of the fuel in the subchamber through the communication opening;

igniting the minor portion of the fuel in the subchamber with the portion of the ignition element;

circulating the ignited minor portion of the fuel from the subchamber to the cavity; and

injecting a remaining portion of the fuel into the cavity independently of and spaced apart from the subchamber.

17. The method as defined in claim 16, wherein the ignition element is a heating element, the method further including heating a wall of the subchamber with the portion of the ignition element, and igniting the minor portion of the fuel in the subchamber with the heated wall.

18. The method as defined in claim 16, wherein the fuel is heavy fuel.

19. The method as defined in claim 16, wherein exposing the portion of the ignition element to the minor portion of the fuel in the subchamber is performed with the portion of the ignition element being located completely outside of the subchamber.

20. The method as defined in claim 16, wherein exposing the portion of the ignition element to the minor portion of the fuel in the subchamber is performed with the portion of the ignition element protruding in the subchamber through the communication opening.