Dual compressor turbocharger

US10378549B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10378549-B2
Application numberUS-201715486854-A
CountryUS
Kind codeB2
Filing dateApr 13, 2017
Priority dateOct 17, 2014
Publication dateAug 13, 2019
Grant dateAug 13, 2019

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A dual compressor turbocharger includes two compressors. One compressor supplies fuel pressure, and one compressor supplies air pressure. The dual compressor turbocharger includes a turbine driven by exhaust of an engine and a shaft coupled to the turbine. The first compressor is mounted on the shaft and includes a first inlet coupled to an air supply and a first outlet coupled to an air intake of the engine. The second compressor is mounted on the shaft and includes a second inlet coupled to a fuel supply and a second outlet coupled to a fuel supply rail of the engine.

First claim

Opening claim text (preview).

We claim: 1. An engine system comprising: a turbine driven indirectly by an engine; a shaft coupled to the turbine; a first compressor mounted on the shaft and having a first inlet coupled to an air supply and a first outlet coupled to an air intake of the engine; a second compressor mounted on the shaft having a second inlet coupled to a fuel supply and a second outlet coupled to a fuel supply rail of the engine; and a controller configured to generate a plurality of throttle control signals, each of the plurality of throttle control signals configured to control the flow of air to one of a plurality of cylinders. 2. The engine system of claim 1 , further comprising: a plurality of throttle plates downstream of an intake manifold, each of the plurality of throttle plates associated with a different cylinder of the plurality of cylinders. 3. The engine system of claim 2 , wherein at least one of the plurality of throttle plates is between a fuel injector and the intake valve for one of the plurality of cylinders. 4. The engine system of claim 2 , wherein at least one of the plurality of throttle plates is between a venturi and the intake valve for one of the plurality of cylinders. 5. The engine system of claim 2 , wherein at least one of the plurality of throttle plates is between a fuel injector and the intake manifold for one of the plurality of cylinders. 6. The engine system of claim 2 , wherein at least one of the plurality of throttle plates is between a venturi and the intake manifold for one of the plurality of cylinders. 7. The engine system of claim 1 , further comprising: a throttle actuator configured to apply forces to the plurality of throttle plates according to the plurality of throttle control signals. 8. The engine system of claim 1 , further comprising: a throttle position sensor configured to detect positions of the plurality of throttle plates. 9. The engine system of claim 1 , wherein the controller is configured to generate digital fuel injection drive signals including pulse trains, the digital fuel injection drive signals configured to release fuel from the fuel supply rail of the engine, wherein each of the plurality of digital fuel injection drive signals corresponding to an individual one of the plurality of cylinders. 10. The engine system of claim 9 , wherein the digital fuel injection drive signals are selected according to a type of gaseous fuel used by the engine. 11. The engine system of claim 1 , wherein the controller is configured to generate a pulse train as a digital fuel injection drive signal to release fuel from the fuel supply rail of the engine to a at least one of the plurality of cylinders. 12. The engine system of claim 1 , wherein the controller is configured to generate a dual compressor control signal for the dual compressor turbocharger based on sensor data. 13. An apparatus comprising: a communication interface electrically connected to a dual compressor turbocharger, the dual compressor turbocharger including a first compressor mounted to a shaft and coupled to an air supply and an air intake of the engine and including a second compressor mounted on the shaft and coupled to a fuel supply and a fuel supply rail of the engine; and a controller, wherein the controller is configured to generate a control signal for the dual compressor turbocharger based on sensor data and configured to generate a plurality of throttle control signals, each of the plurality of throttle control signals configured to control the flow of air to one of a plurality of cylinders. 14. The apparatus of claim 13 , further comprising: a plurality of throttle plates downstream of an intake manifold, each of the plurality of throttle plates associated with a different cylinder of the plurality of cylinders. 15. A method comprising: driving a turbine from exhaust of an engine; rotating a shaft coupled to the turbine; generating air pressure by a first compressor mounted on the shaft and having a first inlet coupled to an air supply and a first outlet coupled to an air intake of the engine; generating fuel pressure by a second compressor mounted on the shaft having a second inlet coupled to a fuel supply and a second outlet coupled to a fuel supply rail of the engine; drawing fuel from the fuel supply rail; and generating a plurality of throttle control signals, each of the plurality of throttle control signals configured to control the flow of air to one of a plurality of cylinders from the air intake of the engine to mix with the fuel drawn from the fuel supply rail. 16. The method of claim 15 , wherein the plurality of throttle control signals control a plurality of throttle plates downstream of an intake manifold, each of the plurality of throttle plates associated with a different cylinder of the plurality of cylinders. 17. The method of claim 16 , wherein at least one of the plurality of throttle plates is between a fuel injector and the intake valve for one of the plurality of cylinders or at least one of the plurality of throttle plates is between a venturi and the intake valve for one of the plurality of cylinders. 18. The method of claim 16 , wherein at least one of the plurality of throttle plates is between a fuel injector and the intake manifold for one of the plurality of cylinders or at least one of the plurality of throttle plates is between a venturi and the intake manifold for one of the plurality of cylinders. 19. The method of claim 15 , further comprising: determining a type of gaseous fuel used by the engine; and generating, based on the type of gaseous fuel, a digital pulse train for a fuel injection drive signal to release fuel from the fuel supply rail of the engine to at least one of the plurality of cylinders. 20. The method of claim 15 , further comprising: generating a dual compressor control signal for the dual compressor turbocharger based on sensor data.

Assignees

Inventors

Classifications

  • having a throttle position sensor (detection of actuation F02D11/106) · CPC title

  • Cross-Sectional Technologies · mapped topic

  • the fuel being gaseous (non-electrical control F02D19/02) · CPC title

  • Engines characterised by operating on gaseous fuels; Plants including such engines (engines characterised by the gas-air charge being ignited by compression ignition of an additional fuel F02B7/06; engines convertible from gas to other fuel consumption F02B69/04) · CPC title

  • Common rails · CPC title

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What does patent US10378549B2 cover?
A dual compressor turbocharger includes two compressors. One compressor supplies fuel pressure, and one compressor supplies air pressure. The dual compressor turbocharger includes a turbine driven by exhaust of an engine and a shaft coupled to the turbine. The first compressor is mounted on the shaft and includes a first inlet coupled to an air supply and a first outlet coupled to an air intake…
Who is the assignee on this patent?
Kohler Co
What technology area does this patent fall under?
Primary CPC classification F04D25/16. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 13 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).