Control system for turbo-compound system

US10047666B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10047666-B2
Application numberUS-201415024642-A
CountryUS
Kind codeB2
Filing dateNov 7, 2014
Priority dateDec 4, 2013
Publication dateAug 14, 2018
Grant dateAug 14, 2018

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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 object is to enable low fuel-consumption operation of an engine by controlling a back pressure and a power generation amount taking account of a trade-off relationship between deterioration of fuel efficiency due to an increase in pumping loss due to a back-pressure rise of the engine and improvement of fuel efficiency due to recovery of exhaust energy by a turbo compound.

First claim

Opening claim text (preview).

The invention claimed is: 1. A control system for a turbo-compound system, comprising: an exhaust turbocharger including an exhaust turbine driven by exhaust gas from an engine and a compressor compressing intake air and supplying the compressed air to the engine; a turbine generator including a power generation turbine driven by the exhaust gas from the engine and a generator connected to the power generation turbine; a storage unit storing electric power generated by the turbine generator; an engine controller configured to control operation of the engine; wherein the engine controller is configured to determine a target boost pressure based on an engine rotation speed and engine load of the engine and to include a power-generation-mode determination unit which determines a command power generation mode, based on the target boost pressure and remaining charge of the storage unit, to one of: a maximum regeneration mode to cause the turbine generator to perform regeneration operation at a maximum capacity without limiting power generation of the turbine generator; a no-regeneration mode to stop power generation of the turbine generator; and a low fuel-consumption mode; a turbo controller configured to receive the target boost pressure and the command power generation mode from the engine controller at a predetermined communication cycle; wherein the turbo controller includes a control computation part and a sensor-signal input part; wherein the control computation part includes: a boost-pressure control unit which controls a boost pressure of the exhaust turbocharger based on the command of the target boost pressure from the engine controller; a power-generation-mode setting unit which sets a power generation mode based on the command of the power generation mode from the engine controller; a power-generation-amount control unit which controls a power generation amount of the turbine generator in accordance with the setting mode of the power-generation mode setting unit; and a back-pressure control unit configured to control at least one of a bypass control valve bypassing the exhaust gas being introduced into the exhaust turbine and a variable nozzle mechanism restricting the exhaust gas being introduced into the exhaust turbine; and wherein the sensor-signal input part is configured to read in a sensor signal from a back-pressure sensor for detecting a pressure of the exhaust gas flowing into the exhaust turbine; and wherein the turbo controller is configured to control the power generation-amount control unit and the back-pressure control unit to achieve at least a recovery amount of exhaust energy recovered by the turbine generator is greater than an increase in a fuel consumption due to an increase in pumping loss due to a back-pressure rise caused in response to rotation of the turbine generator, during the low-fuel-consumption mode. 2. The control system for a turbo-compound system according to claim 1 , wherein the turbo controller has a back-pressure/power-generation-amount map in which a relationship between the back pressure and the power generation amount of the turbine generator is set in advance, the power generation amount being such that low fuel-consumption is sustainable with respect to the back pressure, and is configured to control the power-generation-amount control unit and the back-pressure control unit based on the back-pressure/power-generation-amount map. 3. The control system for a turbo-compound system according to claim 1 , wherein the back-pressure control unit is configured to control the bypass control valve, and wherein the power-generation-amount control unit is configured to control a converter connected to the turbine generator. 4. The control system for a turbo-compound system according to claim 3 , further comprising: an electric compressor disposed on a downstream side, with respect to a flow of air supply, of a compressor of the exhaust turbocharger. 5. The control system for a turbo-compound system according to claim 1 , wherein the back-pressure control unit is configured to control a variable nozzle mechanism to restrict the exhaust gas being supplied into turbine blades of the exhaust turbine, and wherein the power-generation-amount control unit is configured to control a converter connected to the turbine generator. 6. The control system for a turbo-compound system according to claim 1 , wherein the turbo turbo-compound system further comprises an electric compressor, wherein the back-pressure control unit further comprises an additional bypass control valve for bypassing the exhaust gas being supplied to a power generation turbine of the turbine generator rotated by the exhaust gas from the engine, and wherein the power-generation-amount control unit further comprises a converter connected to the turbine generator. 7. The control system for a turbo-compound system according to claim 1 , wherein the turbo controller is configured to, during the low fuel-consumption mode, control the boost pressure of the exhaust turbocharger to achieve the target boost pressure by the boost pressure control unit and to control the power generation-amount control unit and the back-pressure control unit based on the pressure of exhaust gas flowing into the exhaust turbine when the target boost pressure is achieved.

Assignees

Inventors

Classifications

  • Several control loops, either as alternatives or simultaneous · CPC title

  • the rotational speed of pump or exhaust drive being limited · CPC title

  • using at least a proportional, integral or derivative controller · CPC title

  • the devices using kinetic energy · CPC title

  • Battery correction, i.e. corrections as a function of the state of the battery, its output or its type · CPC title

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Frequently asked questions

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What does patent US10047666B2 cover?
An object is to enable low fuel-consumption operation of an engine by controlling a back pressure and a power generation amount taking account of a trade-off relationship between deterioration of fuel efficiency due to an increase in pumping loss due to a back-pressure rise of the engine and improvement of fuel efficiency due to recovery of exhaust energy by a turbo compound.
Who is the assignee on this patent?
Mitsubishi Heavy Ind Ltd
What technology area does this patent fall under?
Primary CPC classification F02B37/18. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 14 2018 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 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).