Rotary engine with pilot subchambers

Patent metadata

Field	Value
Publication number	US-10801394-B2
Application number	US-201715825691-A
Country	US
Kind code	B2
Filing date	Nov 29, 2017
Priority date	Nov 29, 2017
Publication date	Oct 13, 2020
Grant date	Oct 13, 2020

Abstract

A rotary engine including at least two pilot subchambers each in parallel fluid communication with the internal cavity, so that each pilot subchamber is in fluid communication with the combustion chambers as the rotor rotates. Each of the at least two pilot subchambers in fluid communication with a corresponding pilot fuel injector. At least one ignition source is configured for igniting fuel in the pilot subchambers. A compound engine assembly and a method of combusting fuel in a rotary engine are also discussed.

First claim

The invention claimed is:

1. A rotary engine comprising:
a rotor sealingly received within an internal cavity of a housing to define a plurality of combustion chambers;
an intake port and an exhaust port in use in fluid communication with the combustion chambers as the rotor rotates;
at least two pilot subchambers in parallel fluid communication with the internal cavity, the at least two pilot subchambers in use in fluid communication with the combustion chambers as the rotor rotates, the at least two pilot subchambers having intersecting cross-sections, the at least two pilot subchambers together defining a common volume having a multi-lobe configuration;
a main fuel injector in use in fluid communication with the combustion chambers as the rotor rotates, the main fuel injector located upstream of the at least two pilot subchambers with respect to a direction of rotation of the rotor;
at least one pilot fuel injector in fluid communication with the at least two pilot subchambers; and
at least one ignitor in heat exchange relationship with the at least two pilot subchambers.

2. The rotary engine as defined in claim 1 , wherein the at least two pilot subchambers are each in fluid communication with the internal cavity via at least one respective transfer hole.

3. The rotary engine as defined in claim 1 , wherein the at least one pilot fuel injector includes a common pilot fuel injector in fluid communication with the at least two pilot subchambers.

4. The rotary engine as defined in claim 1 , wherein the at least one ignitor includes a first ignitor in heat exchange relationship with at least one of the at least two pilot subchambers.

5. The rotary engine as defined in claim 1 , wherein the at least two pilot subchambers are spaced apart from one another, and are in fluid communication with each other only via the fluid communication with the at least one pilot fuel injector and the fluid communication with the internal cavity.

6. The rotary engine as defined in claim 1 , wherein the at least two pilot subchambers include at least three pilot subchambers.

7. The rotary engine as defined in claim 1 , further comprising a source of heavy fuel in fluid communication with the main fuel injector and the at least one pilot fuel injector.

8. The rotary engine as defined in claim 1 , wherein the ignitor is a glow plug.

9. The rotary engine as defined in claim 1 , wherein the rotary engine is a Wankel engine, the housing including a peripheral wall cooperating with two spaced apart end walls to define the internal cavity, the peripheral wall defining two lobes, the rotor having three circumferentially-spaced apex portions in sealing engagement with the peripheral wall and separating the combustion chambers.

10. The rotary engine as defined in claim 9 , wherein the at least two pilot subchambers are each in fluid communication with the internal cavity via at least one respective transfer hole defined through the peripheral wall.

11. The rotary engine as defined in claim 1 , wherein a volume of one of the combustion chamber varies between a minimum volume and a maximum volume with a difference between the maximum volume and the minimum volume defining a displacement volume, the at least two pilot subchambers having a total volume of at least 0.5% of the displacement volume and at most 3.5% of the displacement volume.

12. The rotary engine as defined in claim 1 , wherein a volume of one of the combustion chambers varies between a minimum volume and a maximum volume, a combustion volume being defined as a sum of the minimum volume and of a total volume of the at least two pilot subchambers, the total volume of the at least two pilot subchambers being at least 5% of the combustion volume and at most 25% of the combustion volume.

13. The rotary engine as defined in claim 1 , wherein the at least two pilot subchambers are defined in an insert received in a wall of the housing, the insert made of a material having a greater heat resistance than a material of the wall of the housing.

14. A compound engine assembly including:
the rotary engine as defined in claim 1 ,
a compressor in fluid communication with the intake port of the rotary engine, and
a turbine in fluid communication with the exhaust port of the rotary engine, the turbine having a turbine shaft compounded with an engine shaft drivingly engaged to the rotor.

15. A rotary engine comprising:
a rotor sealingly received within an internal cavity of a housing to define a plurality of combustion chambers;
an intake port and an exhaust port in use in fluid communication with the combustion chambers as the rotor rotates;
at least three pilot subchambers in parallel fluid communication with the internal cavity, the at least three pilot subchambers in fluid communication with the combustion chambers;
a main fuel injector in use in fluid communication with the combustion chambers as the rotor rotates, the main fuel injector located upstream of the at least two pilot subchambers with respect to a direction of rotation of the rotor;
at least one pilot fuel injector in fluid communication with the at least two pilot subchambers; and
at least one ignitor in heat exchange relationship with the at least two pilot subchambers.

16. A Wankel engine comprising:
a rotor sealingly received within an internal cavity of a housing to define a plurality of combustion chambers, the housing including a peripheral wall cooperating with two spaced apart end walls to define the internal cavity, the peripheral wall defining two lobes, the rotor having three circumferentially-spaced apex portions in sealing engagement with the peripheral wall and separating the combustion chambers;
an intake port and an exhaust port in use in fluid communication with the combustion chambers as the rotor rotates;
at least two pilot subchambers in parallel fluid communication with the internal cavity, the at least two pilot subchambers in fluid communication with the combustion chambers, wherein the at least two pilot subchambers are each in fluid communication with the internal cavity via at least one respective transfer hole defined through the peripheral wall;
a main fuel injector in use in fluid communication with the combustion chambers as the rotor rotates, the main fuel injector located upstream of the at least two pilot subchambers with respect to a direction of rotation of the rotor;
at least one pilot fuel injector in fluid communication with the at least two pilot subchambers; and
at least one ignitor in heat exchange relationship with the at least two pilot subchambers.

17. A rotary engine comprising:
a rotor sealingly received within an internal cavity of a housing to define a plurality of combustion chambers;
an intake port and an exhaust port in use in fluid communication with the combustion chambers as the rotor rotates;
at least two pilot subchambers in parallel fluid communication with the internal cavity, the at least two pilot subchambers in use in fluid communication with the combustion chambers as the rotor rotates;
a main fuel injector in use in fluid communication with the combustion chambers as the rotor rotates, the main fuel injector located upstream of the at least two pilot subchambers with respect to a direction of rotation of the rotor;
at least one pilot fuel injector in fluid communication with the at least two pilot subchambers; and
at least one ignitor in heat exchange relationship with the at least two pilot subchambers, wherein a volume of one of the combustion chamber varies between a minimum volume and a maximum volume wit

Assignees

• Pratt & Whitney Canada

Inventors

• Dussault Serge
• Julien Andre
• Lanktree Michael
• Schulz Edwin

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F01C21/18

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

• F02B53/02

  Methods of operating · CPC title

• F02B19/1095 Primary

  with more than one pre-combustion chamber (a stepped form of the main combustion chamber above the piston is to be considered as a pre-combustion chamber if this stepped portion is not a squish area) · CPC title

• F02B53/12

  Ignition · CPC title