Method for estimating the efficiency loss of a turbocharger for an engine

US11959429B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11959429-B2
Application numberUS-202117797751-A
CountryUS
Kind codeB2
Filing dateFeb 1, 2021
Priority dateFeb 6, 2020
Publication dateApr 16, 2024
Grant dateApr 16, 2024

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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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Abstract

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The present disclosure relates to improvements in turbocharger efficiency and more particularly to a method and system for estimating the efficiency loss of a turbocharger. The method comprises the steps of monitoring a plurality of operating parameters and determining a compressor exit temperature according to a first calibration map based on these operating parameters. An estimate of instantaneous turbocharger efficiency loss according to a second calibration map is then determined, based on the compressor exit temperature. The instantaneous turbocharger efficiency loss is used to determine an estimate of cumulative turbocharger efficiency loss during engine service. The estimate of cumulative turbocharger efficiency loss is compared with a first predetermined efficiency loss threshold and a first signal is generated if the first predetermined efficiency loss threshold is exceeded.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for estimating the efficiency loss of a turbocharger for an engine, said method comprising the steps of:— monitoring a plurality of operating parameters; determining a compressor exit temperature according to a first calibration map based on the plurality of operating parameters; determining an estimate of instantaneous turbocharger efficiency loss according to a second calibration map based on the compressor exit temperature; determining a NOx concentration in engine exhaust gas at the compressor outlet temperature according to a NOx concentration map for the estimate of instantaneous turbocharger efficiency loss; using the determined instantaneous turbocharger efficiency loss to determine an estimate of cumulative turbocharger efficiency loss during engine service; comparing the estimate of cumulative turbocharger efficiency loss with a first predetermined efficiency loss threshold; generating a first signal if the first predetermined efficiency loss threshold is exceeded. 2. The method as claimed in claim 1 , further comprising:— a controller configured to control operation of the engine and/or the turbocharger to operate in a safe regime when the first signal is generated. 3. The method as claimed in claim 1 , wherein the plurality of operating parameters comprise engine speed, fuel injection quantity, barometric pressure and ambient temperature. 4. The method as claimed in claim 1 , wherein if the first predetermined efficiency loss threshold is exceeded, the estimate of cumulative turbocharger efficiency loss is compared with a second predetermined efficiency loss threshold, which is higher than the first predetermined efficiency loss threshold and, if the estimate of cumulative turbocharger efficiency loss exceeds the second predetermined efficiency loss threshold, a second signal is generated. 5. The method as claimed in claim 1 , further comprising the steps of:— comparing the determined NOx concentration with a predetermined NOx threshold; and providing a second signal only if both the determined NOx concentration exceeds predetermined NOx threshold and the estimate of cumulative turbocharger efficiency loss a exceeds the second predetermined efficiency loss threshold. 6. The method as claimed in claim 1 , further comprising the step of:— determining from a third calibration map the presence of any predetermined operating conditions; and excluding the step of comparing the determined NOx concentration with a predetermined NOx threshold if any such predetermined operating conditions are present. 7. The method as claimed in claim 6 , wherein engine speed and fuel injection quantity are used by the third calibration map as input parameters for the determination whether any predetermined operating conditions are present. 8. The method as claimed in claim 7 , wherein the predetermined operating conditions include an engine operation or fault mode where there is a known elevated NOx condition. 9. The method as claimed in claim 1 , wherein the first and/or second signal triggers a first and/or second alert respectively and/or a change in engine and/or turbocharger operation. 10. The system configured to implement the method for estimating the efficiency loss of an engine turbocharger as claimed in claim 1 , comprising:— an engine; a turbocharger; a plurality of sensors monitoring said plurality of operating parameters; a controller configured to receive signals relating to said plurality of engine operating parameters, said controller comprising a memory configured to store said calibration map(s), wherein the controller is configured to generate said signal(s).

Assignees

Inventors

Classifications

  • for control of turbo-charged or super-charged engines (control of the pumps per se F02B37/12) · CPC title

  • Control of the pumps · CPC title

  • Other safety measures for, or other control of, pumps · CPC title

  • Controlling engines characterised by their being supercharged · CPC title

  • of the exhaust gases emitted by the engine · CPC title

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What does patent US11959429B2 cover?
The present disclosure relates to improvements in turbocharger efficiency and more particularly to a method and system for estimating the efficiency loss of a turbocharger. The method comprises the steps of monitoring a plurality of operating parameters and determining a compressor exit temperature according to a first calibration map based on these operating parameters. An estimate of instanta…
Who is the assignee on this patent?
Caterpillar Inc
What technology area does this patent fall under?
Primary CPC classification F02D41/0007. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 16 2024 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).