Donor cylinder engine system implementing skip firing

US9631581B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9631581-B2
Application numberUS-201414298119-A
CountryUS
Kind codeB2
Filing dateJun 6, 2014
Priority dateJun 6, 2014
Publication dateApr 25, 2017
Grant dateApr 25, 2017

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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.

An engine system is disclosed. The engine system may have a first bank of cylinders, a second bank of cylinders, a first intake manifold, and a second intake manifold. The engine system may also have a first exhaust manifold connecting the first bank of cylinders to the first and second intake manifolds, a second exhaust manifold connecting the second bank of cylinders to the atmosphere, a plurality of injectors, and a controller. The controller may be configured to inhibit the plurality of injectors associated with a first cylinder subset of the first and second banks of cylinders from firing for a first period of time spanning multiple engine cycles. The controller may also be configured to selectively inhibit the plurality of injectors associated with a second cylinder subset of the first and second banks of cylinders from firing for a second period of time following the first period of time.

First claim

Opening claim text (preview).

What is claimed is: 1. An engine system, comprising: a first bank of cylinders; a second bank of cylinders; a first intake manifold associated with the first bank of cylinders; a second intake manifold associated with the second bank of cylinders; a first exhaust manifold connecting the first bank of cylinders to the first and second intake manifolds; a second exhaust manifold connecting the second bank of cylinders to the atmosphere; a plurality of injectors, each associated with a different cylinder in the first and second banks of cylinders; and a controller in communication with the plurality of injectors, the controller configured to: selectively inhibit the plurality of injectors associated with a first cylinder subset of the first and second banks of cylinders from firing for a first period of time spanning multiple engine cycles; and selectively inhibit the plurality of injectors associated with a second cylinder subset of the first and second banks of cylinders from firing for a second period of time spanning multiple engine cycles following the first period of time. 2. The engine system of claim 1 , wherein each of the first and second cylinder subsets includes an equal number of cylinders from each of the first and second banks of cylinders. 3. The engine system of claim 2 , wherein the controller is configured to allow the plurality of injectors to inject fuel in an order that alternates between the first and second banks of cylinders. 4. The engine system of claim 1 , wherein the first and second periods of time are about equal. 5. The engine system of claim 4 , wherein the first and second periods of time are determined based in part on achieving a desired thermal loading. 6. The engine system of claim 1 , wherein: the first bank of cylinders are in positions numbered sequentially 1-6; the second bank of cylinders are in positions numbered sequentially 7-12; and a normal load firing order of the engine system is 1-7-5-11-3-9-6-12-2-8-4-10. 7. The engine system of claim 6 , wherein the controller is configured to selectively inhibit the plurality of injectors from firing only during a low-load condition. 8. The engine system of claim 7 , wherein a low-load firing order of the first cylinder subset is 1-11-6-8. 9. The engine system of claim 8 , wherein a low-load firing order of the second cylinder subset is 7-3-12-4. 10. The engine system of claim 9 , wherein: the engine system further includes a third cylinder subset of the first and second banks of cylinders; and a low-load firing order of the third cylinder subset is 5-9-2-10. 11. The engine system of claim 10 , wherein the low-load firing order of each of the first, second, and third cylinder subsets results in every other firing being associated with exhaust gas recirculation donation. 12. The engine system of claim 11 , wherein the low-load firing order of each of the first, second, and third cylinder subsets results in the engine system being mechanically balanced. 13. The engine system of claim 1 , wherein a firing interval of the first and second cylinder subsets during a low-load condition is always between about 165-195° of crank angle. 14. The engine system of claim 3 , wherein a firing interval of the first bank of cylinders during a low-load condition is always about 360° of crank angle. 15. The engine system of claim 14 , wherein a firing interval of the second bank of cylinders during a low-load condition is always about 360° of crank angle. 16. The engine system of claim 1 , further including a turbine connected to the second exhaust manifold. 17. The engine system of claim 16 , further including a bypass passage connecting the first exhaust manifold to the second exhaust manifold. 18. An engine system, comprising: a first bank of cylinders; a second bank of cylinders; a first intake manifold associated with the first bank of cylinders; a second intake manifold associated with the second bank of cylinders; a first exhaust manifold connecting the first bank of cylinders to the first and second intake manifolds; a second exhaust manifold connecting the second bank of cylinders to the atmosphere; a plurality of injectors, each associated with a different cylinder in the first and second banks of cylinders; and a controller in communication with the plurality of injectors, the controller configured to: selectively inhibit the plurality of injectors associated with a first cylinder subset of the first and second banks of cylinders from firing for a first period of time spanning multiple engine cycles during a low-load condition; selectively inhibit the plurality of injectors associated with a second cylinder subset of the first and second banks of cylinders from firing for a second period of time spanning multiple engine cycles following the first period of time during the low-load condition; and selectively inhibit the plurality of injectors associated with a third cylinder subset of the first and second banks of cylinders from firing for a third period of time spanning multiple engine cycles following the second period of time during the low-load condition, wherein: a firing interval of the first, second, and third cylinder subsets during the low-load condition is always between about 165-195° of crank angle; and a separate firing interval of each of the first and second cylinder banks during the low-load condition is always about 360° of crank angle. 19. The engine system of claim 18 , wherein: each of the first, second, and third cylinder subsets includes two cylinders from each of the first and second banks of cylinders; the first bank of cylinders are in positions numbered sequentially 1-6; the second bank of cylinders are in positions numbered sequentially 7-12; a normal load firing order of the engine system is 1-7-5-11-3-9-6-12-2-8-4-10; a low-load firing order of the first cylinder subset is 1-11-6-8; a low-load firing order of the second cylinder subset is 7-3-12-4; and a low-load firing order of the third cylinder subset is 5-9-2-10. 20. A method of operating an engine system having multiple cylinders arranged into a first donor bank sequentially numbered 1-6 and a second non-donor bank sequentially numbered 7-12, comprising: firing the multiple cylinders during a normal load condition according to the following pattern: 1-7-5-11-3-9-6-12-2-8-4-10; selectively firing for a first period of time spanning multiple engine cycles during a low-load condition only a first subset of two cylinders from each of the first donor and second non-donor banks according to the following pattern: 1-11-6-8; selectively firing for a second period of time spanning multiple engine cycles during the low-load condition following the first period of time only a second subset of two cylinders from each of the first donor and second non-donor banks according to the following pattern: 7-3-6-8; and selectively firing for a third period of time spanning multiple engine cycles during the low-load condition following the second period of time only a third subset of two cylinders from each of the first donor and second non-donor banks according to the following pattern: 5-9-2-10, wherein: a firing interval of the first, second, and third subsets during the low-load condition is always between about 165-195° of crank angle; and a separate firing interval of each of the first and second cylinder banks during the low-load condition is always about 360° of crank angle.

Assignees

Inventors

Classifications

  • F02M26/05Primary

    High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor · CPC title

  • with cylinders in V, fan, or star arrangement · CPC title

  • in which a main EGR passage is branched into multiple passages · CPC title

  • in which exhaust from only one cylinder or only a group of cylinders is directed to the intake of the engine · CPC title

  • with cylinders arranged in parallel banks · CPC title

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Frequently asked questions

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What does patent US9631581B2 cover?
An engine system is disclosed. The engine system may have a first bank of cylinders, a second bank of cylinders, a first intake manifold, and a second intake manifold. The engine system may also have a first exhaust manifold connecting the first bank of cylinders to the first and second intake manifolds, a second exhaust manifold connecting the second bank of cylinders to the atmosphere, a plur…
Who is the assignee on this patent?
Electro Motive Diesel Inc
What technology area does this patent fall under?
Primary CPC classification F02M26/05. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 25 2017 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).