Method of combusting fuel in a rotary internal combustion engine with pilot subchamber and ignition element

Patent metadata

Field	Value
Publication number	US-10968820-B2
Application number	US-201916574650-A
Country	US
Kind code	B2
Filing date	Sep 18, 2019
Priority date	Jun 5, 2013
Publication date	Apr 6, 2021
Grant date	Apr 6, 2021

Abstract

A rotary engine includes an insert having a pilot subchamber defined therein and communicating with the internal cavity of the engine. A pilot fuel injector has a tip in communication with the pilot subchamber. An ignition element extends into an element cavity defined through the insert adjacent the pilot subchamber. The element cavity is 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 is smaller than a portion of the ignition element adjacent the communication opening such as to prevent the portion of the ignition element from completely passing through the communication opening upon breaking off of the portion of the ignition element from a remainder of the ignition element. An outer body for a rotary engine and a method of combusting fuel in a rotary engine are also provided.

First claim

The invention claimed is:

1. 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 of the engine;
activating a portion of an ignition element received in the insert, the portion of the ignition element 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 upon breaking off of the portion of the ignition element from a remainder of the ignition element;
igniting the minor portion of the fuel in the subchamber by exposing the portion of the ignition element to the minor portion of the fuel through the communication opening;
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.

2. The method as defined in claim 1 , 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.

3. The method as defined in claim 1 , wherein the fuel is heavy fuel.

4. The method as defined in claim 1 , 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.

5. The method as defined in claim 1 , 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.

Assignees

• Pratt & Whitney Canada

Inventors

• Gaul Michael
• Julien Andre
• Villeneuve Bruno

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F01C1/22

  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 title

• F02B53/12 Primary

  Ignition · CPC title

• F02B55/08

  Outer members for co-operation with rotary pistons; Casings · CPC title

• F02B55/14

  Shapes or constructions of combustion chambers · CPC title