Rotary internal combustion engine with pilot subchamber and ignition element

• US 10,006,359 B2
• Filed: 05/02/2016
• Issued: 06/26/2018
• Est. Priority Date: 06/05/2013
• Status: Active Grant

• Current Assignee: Pratt & Whitney Canada Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Pratt & Whitney Canada Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Gaul, Michael, Julien, Andre, Villeneuve, Bruno
• Primary Examiner(s): NEWTON, JASON TODD
• Application Number:
  US15/143,974
• Publication Number:
  US 20160245165A1
• Time in Patent Office: 785 Days
• Field of Search: 60 396, 60 3662, 60 3963, 60 3964, 123200, 123205, 123207, 123208, 123209, 123210, 123212, 123214, 123218, 123231, 123243, 123273, 123275, 123284, 123445
• 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. The insert has a pilot subchamber defined therein communicating with the internal cavity and includes a subchamber wall surrounding the pilot subchamber. A main fuel injector is in communication with the internal cavity at a location spaced apart from the insert. A pilot fuel injector is in communication with the pilot subchamber. A heating element extends within the subchamber wall completely outside of the pilot subchamber, in heat transfer communication with the subchamber wall. 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 walls surrounding an internal cavity;

a rotor body rotatable within the internal cavity and cooperating with the walls of the outer body to define at least one chamber of variable volume;

an insert in one of the walls of the outer body, the insert having a pilot subchamber defined therein communicating with the internal cavity and including a subchamber wall surrounding the pilot subchamber;

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

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

a heating element extending within the subchamber wall completely outside of the pilot subchamber, the heating element being in heat transfer communication with the subchamber wall, the heating element being elongated and extending along a straight axis.

2. The engine as defined in claim 1, wherein the axis is parallel to a longitudinal axis of the insert.

3. The engine as defined in claim 1, wherein the subchamber wall forms an indent protruding within the pilot subchamber, and the heating element extends within the subchamber wall against the indent.

4. The engine as defined in claim 1, wherein the heating element includes a heatable wire received in a ceramic outer layer.

5. The engine as defined in claim 1, wherein the heating element extends closer to the pilot subchamber than to an outer surface of the insert.

6. 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 walls of the outer body.

7. 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 epitrochoid shape defining two lobes.

8. An outer body for a Wankel engine comprising:

interconnected walls surrounding an internal cavity having an epitrochoid shape, the internal cavity configured to sealingly engage a rotor receivable therein;

an insert in one of the interconnected walls, the insert having a pilot subchamber defined therein in communication with the cavity, the insert having a pilot injector hole defined therein in communication with the pilot subchamber and sized to receive a tip of a pilot fuel injector; and

a heating element extending within the insert completely outside of the pilot subchamber, the heating element being in heat transfer communication with a wall of the pilot subchamber, the heating element being elongated and extending along a straight axis.

9. The outer body as defined in claim 8, wherein the axis is parallel to a longitudinal axis of the insert.

10. The outer body as defined in claim 8, wherein the wall of the pilot subchamber forms an indent protruding within the pilot subchamber, and the heating element extends within the wall of the pilot subchamber against the indent.

11. The outer body as defined in claim 8, wherein the heating element includes a heatable wire received in a ceramic outer layer.

12. The outer body as defined in claim 8, wherein the heating element extends closer to the pilot subchamber than to an outer surface of the insert.

13. The outer body as defined in claim 8, 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 interconnected walls.

14. 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 pilot subchamber defined in an insert located in a wall of the rotary engine;

heating a portion of the insert defining a wall of the pilot subchamber by activating a heating element received in the insert of the rotary engine adjacent the pilot subchamber, the heating element extending in the insert without extending in the pilot subchamber, the heating element being elongated and extending along an axis;

igniting the fuel in the pilot subchamber with the portion of the insert defining the wall of the pilot subchamber;

circulating the ignited fuel from the pilot subchamber to the cavity of the rotary engine; and

injecting a remainder of the fuel into the cavity of the rotary engine independently from the pilot subchamber.

15. The method as defined in claim 14, wherein the fuel is heavy fuel.

16. The method as defined in claim 14, wherein the heating element is activated in a discrete manner.

17. A rotary engine comprising:

an outer body having walls surrounding an internal cavity;

a rotor body rotatable within the internal cavity and cooperating with the walls of the outer body to define at least one chamber of variable volume;

an insert in one of the walls of the outer body, the insert having a pilot subchamber defined therein communicating with the internal cavity and including a subchamber wall surrounding the pilot subchamber;

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

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

a heating element extending within the subchamber wall completely outside of the pilot subchamber, the heating element being in heat transfer communication with the subchamber wall;

wherein the subchamber wall forms an indent protruding within the pilot subchamber, and the heating element extends within the subchamber wall against the indent.

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

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

heating a portion of the insert defining a wall of the pilot subchamber by activating a heating element received in the insert of the rotary engine adjacent the pilot subchamber, the heating element extending in the insert without extending in the pilot subchamber;

igniting the heavy fuel in the pilot subchamber with the heated wall of the pilot subchamber;

circulating the ignited heavy fuel from the pilot subchamber to the cavity of the rotary engine; and

injecting a remainder of the heavy fuel into the cavity of the rotary engine independently from the pilot subchamber.