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US 10,801,394 B2Granted
Rotary engine with pilot subchambers
AssigneePratt & Whitney Canada Corp.
InventorsSerge Dussault, Andre Julien, Michael Lanktree, Edwin Schulz
Life of this patent
Estimating the term…
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.
Claims19
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.
4 more elements
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.
4 more elements
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.
4 more elements
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 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.
4 more elements
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 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.
4 more elements
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, 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;
- 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.
4 more elements
Dependencies are inferred from the claim text.