Systems and methods for control of turbine-generator via valve deactivation in a split exhaust engine system

US9518506B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9518506-B2
Application numberUS-201414537697-A
CountryUS
Kind codeB2
Filing dateNov 10, 2014
Priority dateNov 10, 2014
Publication dateDec 13, 2016
Grant dateDec 13, 2016

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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.

Methods and systems are provided for reducing exhaust energy delivered to a turbine of a turbine-generator coupled to a split exhaust engine system in order to reduce turbine over-speed conditions and/or to reduce a generator output. In one example, a method may include deactivating a blowdown exhaust valve utilized to deliver a blowdown portion of exhaust energy to the turbine.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for operating an engine including an exhaust-driven turbine, the method comprising: determining engine operating conditions which comprise at least one of an actual turbine speed, an actual generator speed, and an actual generator output; in response to determining, with an engine controller, the actual turbine speed less than a threshold turbine speed, adjusting a first exhaust valve of a cylinder via a first actuator to deliver exhaust produced by combustion from the first exhaust valve of the cylinder to the exhaust-driven turbine via a first exhaust manifold; wherein the exhaust-driven turbine drives a generator; and adjusting a second exhaust valve of the cylinder via a second actuator to deliver exhaust produced by combustion from the second exhaust valve of the cylinder to an exhaust catalyst while bypassing the exhaust-driven turbine via a second exhaust manifold; and in response to determining, with the engine controller, the actual turbine speed greater than or equal to the threshold turbine speed, selectively deactivating the first exhaust valve via the first actuator. 2. The method of claim 1 , where the first exhaust valve is deactivated to a closed position, and further comprising: selectively deactivating the first exhaust valve, in response to determining, with the engine controller, the actual generator output greater than a threshold output; wherein the actual generator output includes one or more of a generator output voltage, a generator output current, or a generator output power. 3. The method of claim 1 , further comprising: determining, with the engine controller, a desired generator output; determining, with the engine controller, a difference between the actual generator output and the desired generator output; and in response to determining, with the engine controller, the difference between the actual generator output and the desired generator output greater than a threshold difference, selectively deactivating the first exhaust valve. 4. The method of claim 1 , further comprising: determining, with the engine controller, the threshold turbine speed based on a desired generator speed. 5. The method of claim 4 , wherein further comprising: determining, with the engine controller, the desired generator speed based on an engine speed, an engine load, and an amount of exhaust mass flow being delivered into the exhaust-driven turbine via the first exhaust valve. 6. The method of claim 1 , further comprising: in response to the actual turbine speed less than the threshold turbine speed, advancing a first exhaust valve opening timing of the first exhaust valve with respect to a second exhaust valve opening timing of the second exhaust valve at end of a power stroke. 7. The method of claim 6 , further comprising: in response to the actual turbine speed less than the threshold turbine speed, advancing a first exhaust valve closing timing of the first exhaust valve is advanced with respect to a second exhaust valve closing timing of the second exhaust valve at end of an exhaust stroke. 8. The method of claim 1 , further comprising: in response to the actual turbine speed greater than the threshold turbine speed, selectively deactivating the first exhaust valve of a number of cylinders of the engine. 9. The method of claim 8 , wherein further comprising: deactivating the first exhaust valve of the number of the cylinders of the engine based on one or more of a rate of change of the turbine speed, a difference between the actual generator output and a desired generator output greater than a threshold difference, an engine speed, and an engine load. 10. The method of claim 1 , further comprising: in response to the actual turbine speed greater than the threshold turbine speed, deactivating the first exhaust valve of the cylinder. 11. A method of operating an engine including a first exhaust passage directly coupled to a turbine driving a generator and a second exhaust passage directly coupled to an exhaust catalyst, an outlet of the turbine coupled to the catalyst via a third exhaust passage, the method comprising: determining engine operating conditions which comprise at least one of an actual turbine speed, an actual generator speed, and an actual generator output; in response to determining, with an engine controller, the actual turbine speed less than a threshold turbine speed, flowing exhaust gas produced by combustion to the turbine by operating a first exhaust valve of all cylinders, the first exhaust valve in each of said all cylinders selectively allowing the exhaust gas flow from the each of said all cylinders to the first exhaust passage via a first exhaust manifold; and flowing exhaust gas produced by combustion to the catalyst by operating a second exhaust valve of said all cylinders, the second exhaust valve in the each of said all cylinders selectively allowing the exhaust gas flow from the each of said all cylinders to the second exhaust passage via a second exhaust manifold; and in response to determining, with the engine controller, the speed of the turbine at or above the threshold speed, selectively deactivating the first exhaust valve of a number of cylinders while maintaining the first exhaust valve of a remaining number of the cylinders active; wherein the first exhaust valve of the each of said all cylinders is operated via a first actuator and the second exhaust valve of the each of said all cylinders is operated by a second actuator. 12. The method of claim 11 , further comprising: in response to the actual turbine speed being at or above the threshold speed, selectively deactivating the first exhaust valve of said all cylinders. 13. The method of claim 11 , further comprising: determining, with the controller, wherein the number of the cylinders based on one or more of a rate of change of the turbine speed, a difference between an actual generator output and a desired generator output greater than a threshold difference, an engine speed, and an engine load. 14. The method of claim 13 , further comprising: in response to determining, with the engine controller, the actual generator output greater than a threshold generator output, selectively deactivating the first exhaust valve of the number of the cylinders. 15. The method of claim 14 , further comprising: in response to determining, with the engine controller, a difference between an actual generator speed and a desired generator speed greater than a threshold generator speed, selectively deactivating the first exhaust valve of the number of the cylinders. 16. The method of claim 15 , further comprising: determining, with the engine controller, the desired generator speed based on an engine speed, an engine load, and an amount of exhaust mass flow being delivered into the turbine via the first exhaust valve. 17. The method of claim 13 , further comprising: in response to the actual turbine speed less than the threshold turbine speed, and the actual generator output less than the threshold generator output, advancing a timing of the first exhaust valve of said all cylinders with respect to a timing of the second exhaust valve of said all cylinders. 18. A system comprising: an engine cylinder; a first exhaust valve for delivering an initial portion of exhaust gas from the cylinder to a turbine-generator via a first exhaust passage; a second exhaust valve for delivering a latter portion of the exhaust gas from the cylinder to an exhaust catalyst located downstream o

Assignees

Inventors

Classifications

  • F01L1/28Primary

    characterised by the provision of coaxial valves; characterised by the provision of valves co-operating with both intake and exhaust ports · CPC title

  • specially adapted for four or more valves per cylinder · CPC title

  • for engines with variable valve actuation · CPC title

  • to increase temperature of the exhaust gas treating apparatus · CPC title

  • Independent control of two or more intake or exhaust valves respectively, i.e. one of two intake valves remains closed or is opened partially while the other is fully opened · CPC title

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What does patent US9518506B2 cover?
Methods and systems are provided for reducing exhaust energy delivered to a turbine of a turbine-generator coupled to a split exhaust engine system in order to reduce turbine over-speed conditions and/or to reduce a generator output. In one example, a method may include deactivating a blowdown exhaust valve utilized to deliver a blowdown portion of exhaust energy to the turbine.
Who is the assignee on this patent?
Ford Global Tech Llc
What technology area does this patent fall under?
Primary CPC classification F01L1/28. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 13 2016 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 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).