Control of combustion engine shut down

US10954875B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10954875-B2
Application numberUS-201616334492-A
CountryUS
Kind codeB2
Filing dateOct 19, 2016
Priority dateOct 19, 2016
Publication dateMar 23, 2021
Grant dateMar 23, 2021

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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.

The abrupt cessation or run-away of a combustion engine may damage the combustion engine and pose a safety hazard to the surrounding environment. The combustion engine operational mode may be controlled, regulated or maintained by regulating the combustion mixture of the combustion engine. The oxidizer flow, a material or both of the combustion mixture may be regulate to create or form a combustion material that is outside a combustible range such that the combustion engine is placed or maintained in a spin-down operational mode. The material added to the combustion mixture may include a combustible, non-combustible, oxidizer, or exhaust material. A brake may also provide a secondary mechanism to maintain or place the combustion engine in a spin-down mode.

First claim

Opening claim text (preview).

What is claimed is: 1. A combustion engine system, comprising: a combustion engine; an intake vent disposed about the combustion engine; a control damper disposed about the intake vent, wherein the control damper controls oxidizer flow to the intake vent; and a combustion mixture, wherein the combustion mixture comprises a portion of oxidizer and a portion of fuel, wherein the portion of oxidizer is restricted by the control damper such that the combustion mixture is within a non-combustible range to maintain the combustion engine in a spin-down operational mode. 2. The combustion engine system of claim 1 , further comprising a sensor disposed about the control damper, wherein the sensor transmits one or more measurements associated with oxidizer flow to the intake vent to a control panel. 3. The combustion engine system of claim 2 , wherein the control panel is communicatively coupled to the control damper, and wherein the control panel adjusts a position of control damper based, at least in part, on the one or more measures associated with the oxidizer flow. 4. The combustion engine system of claim 1 , further comprising a brake disposed about the combustion engine, wherein the brake prevents the combustion engine from transition to a spin-up operational mode. 5. The combustion engine system of claim 1 , wherein the control damper comprises one of a butterfly-type valve, a knife-type valve or an iris-type valve. 6. The combustion engine system of claim 1 , wherein the combustion engine comprises a turbine engine. 7. A combustion engine system, comprising: a combustion engine; and a diffuser disposed about the combustion engine, wherein the diffuser controls addition of a material to a combustion mixture to regulate combustion of the combustion engine. 8. A combustion engine system of claim 7 , wherein the material comprises a combustible material, a non-combustible material, an oxidizer material, or an exhaust material. 9. A combustion engine system of claim 7 , further comprising: one or more sensors disposed about the combustion engine; and a control panel communicatively coupled to the one or more sensors, wherein the control panel receives one or more measurements associated with at least one of the combustion mixture or the material from one or more sensors. 10. A combustion engine system of claim 7 , further comprising a brake disposed about the combustion engine, wherein the brake prevents the combustion engine from transitioning to a spin-up operational mode. 11. A combustion engine system of claim 7 , further comprising: an exhaust vent disposed about the combustion engine; an intake vent disposed about the combustion engine; and a return exhaust flow path coupled to the exhaust vent and the intake vent, wherein the return exhaust flow path directs the material from the exhaust vent to the intake vent. 12. A combustion engine system of claim 7 , wherein the combustion engine comprises a turbine engine. 13. A method for controlling a combustion engine system, comprising: controlling a combustion mixture of a combustion engine, wherein controlling the combustion mixture comprises regulating one or more of an oxidizer flow or a material that is mixed with the combustion mixture; adjusting, by a diffuser, the combustion mixture such that the combustion mixture is outside a combustible range by adding the material to the combustion mixture; placing the combustion engine in a spin-down operational mode by the regulation of the one or more of oxidizer flow or the material; and maintaining the combustion engine in the spin-down operational mode. 14. The method for controlling the combustion engine system of claim 13 , further comprising restricting the oxidizer flow mixed in the combustion mixture such that the combustion mixture is outside a combustible range by positioning a control damper in a closed position or a partially closed position. 15. The method for controlling a combustion engine system of claim 13 , further comprising enriching the combustion mixture such that the combustion mixture is outside a combustible range by adding the material to the combustion mixture, wherein the material is a combustible material. 16. The method for controlling a combustion engine system of claim 13 , wherein the material is a non-combustible material. 17. The method for controlling a combustion engine system of claim 13 , wherein the material is an oxidizing material. 18. The method for controlling a combustion engine system of claim 13 , further comprising: wherein the material is an exhaust material from an exhaust vent of the combustion engine, and wherein adjusting the combustion mixture comprises: directing the exhaust from the exhaust vent to an intake vent of the combustion engine via a return exhaust flow path. 19. The method for controlling a combustion engine system of claim 13 , wherein controlling the combustion mixture comprises: receiving one or more measurements from one or more sensors; determining at least one of an amount of oxidizer or an amount of the material required to place the combustion engine in the spin-down operational mode; and adjusting the combustion mixture based, at least in part, on the one or more measurements. 20. The method for controlling a combustion engine system of claim 13 , wherein maintaining the combustion engine in the spin-down operational mode comprises engaging a brake to prevent the combustion engine from transition to a spin-up operational mode.

Assignees

Inventors

Classifications

  • F02D9/101Primary

    Special flap shapes, ribs, bores or the like · CPC title

  • the members being slidable transversely of conduit · CPC title

  • by throttling; by adjusting vanes · CPC title

  • by means of shiftable members or valves obturating part of the flow path · CPC title

  • by means of rotatable members, e.g. butterfly valves · CPC title

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What does patent US10954875B2 cover?
The abrupt cessation or run-away of a combustion engine may damage the combustion engine and pose a safety hazard to the surrounding environment. The combustion engine operational mode may be controlled, regulated or maintained by regulating the combustion mixture of the combustion engine. The oxidizer flow, a material or both of the combustion mixture may be regulate to create or form a combus…
Who is the assignee on this patent?
Halliburton Energy Services Inc
What technology area does this patent fall under?
Primary CPC classification F02D9/101. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Mar 23 2021 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).