Systems and methods for conducting vehicle evaporative emissions test diagnostic procedures

US11187192B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11187192-B2
Application numberUS-201815894655-A
CountryUS
Kind codeB2
Filing dateFeb 12, 2018
Priority dateFeb 12, 2018
Publication dateNov 30, 2021
Grant dateNov 30, 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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  7. Citations and related patents

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Abstract

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Methods and systems are provided for conducting diagnostics to indicate whether a fuel system and/or an evaporative emissions system of a vehicle has a source of undesired evaporative emissions, or not. A method comprises conducting such a diagnostic via evacuating the fuel system to a target vacuum, then sealing the fuel system from atmosphere and monitoring a pressure bleed-up in the fuel system, and dynamically adjusting a pressure bleed-up threshold responsive to one or more conditions that impact the pressure bleed-up during the diagnostic, and indicating undesired evaporative emissions responsive to the pressure bleed-up reaching the adjusted pressure bleed-up threshold. In this way, interpretation of the results of such a diagnostic may be more robust, completion rates may improve, and engine operation may be improved.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method, comprising: conducting a test diagnostic via evacuating a fuel system and an evaporative emissions system of a vehicle to a variable vacuum target, then, once at the variable vacuum target, sealing the fuel system and the evaporative emissions system from atmosphere and monitoring a pressure bleed-up in the fuel system and the evaporative emissions system and indicating a presence of undesired evaporative emissions stemming from the fuel system and/or the evaporative emissions system in response to the pressure bleed-up reaching or exceeding a pressure bleed-up threshold, wherein the pressure bleed-up threshold is dynamically adjusted in response to an indication of one or more conditions that impact the pressure bleed-up, and wherein the variable vacuum target is determined, before the pressure bleed-up, as a function of one or more of ambient temperature, a fuel level of fuel stored in a fuel tank of the fuel system, and/or a loading state of a fuel vapor storage canister that traps and stores fuel vapors stemming from the fuel system, wherein sealing the fuel system and the evaporative emissions system from atmosphere and monitoring the pressure bleed-up in the fuel system and the evaporative emissions system includes monitoring two separate pressure bleed-ups including a fuel system pressure bleed-up and an evaporative emissions system pressure bleed-up, wherein dynamically adjusting the pressure bleed-up threshold includes dynamically adjusting a fuel system pressure bleed-up threshold independently of an evaporative emissions system pressure bleed-up threshold, and wherein indicating the presence of undesired evaporative emissions stemming from the fuel system and/or the evaporative emissions system in response to the pressure bleed-up reaching or exceeding the pressure bleed-up threshold comprises indicating the presence of undesired evaporative emissions stemming from the evaporative emissions system in response to the evaporative emissions system pressure bleed-up reaching or exceeding the evaporative emissions system pressure bleed-up threshold, and indicating the presence of undesired evaporative emissions stemming from the fuel system in response to the fuel system pressure bleed-up reaching or exceeding the fuel system pressure bleed-up threshold. 2. The method of claim 1 , wherein dynamically adjusting the pressure bleed-up threshold includes adjusting the pressure bleed-up threshold in response to a sudden drop in pressure in the fuel system and/or the evaporative emissions system d u ring the pressure bleed-up, the pressure bleed-up threshold adjusted to a level more negative than a previous pressure bleed-up threshold, and wherein the fuel system is fluidically coupled to the evaporative emissions system upon sealing the fuel system and the evaporative emissions system. 3. The method of claim 2 , further comprising, prior to conducting the test diagnostic, learning via a controller routes commonly traveled by the vehicle in order to determine the one or more conditions that impact the pressure bleed-up; wherein the one or more conditions that impact the pressure bleed-up comprise one or more learned events including fuel slosh events and/or altitude changes; and wherein dynamically adjusting the pressure bleed-up threshold further includes adjusting the pressure bleed-up threshold as a function of the one or more learned events, and wherein the variable vacuum target is further a function of the one or more learned events. 4. The method of claim 2 , further comprising, at a time prior to and with in a threshold duration of conducting the test diagnostic, with the vehicle stationary, venting the fuel system and then sealing the fuel system and monitoring pressure in the sealed fuel system for a predetermined duration, in order to determine a reid vapor pressure of a fuel stored in the fuel system; and wherein dynamically adjusting the pressure bleed-up threshold includes adjusting the pressure bleed-up threshold as a function of the reid vapor pressure of the fuel stored in the fuel system, and wherein the variable vacuum target is further a function of the reid vapor pressure of the fuel stored in the fuel system. 5. The method of claim 1 , wherein sealing the fuel system and the evaporative emissions system from atmosphere and monitoring the pressure bleed-up in the fuel system and the evaporative emissions system includes monitoring a single pressure bleed-up under conditions where the fuel system is fluidically coupled to the evaporative emissions system upon sealing the fuel system and the evaporative emissions system, and wherein dynamically adjusting the pressure bleed-up threshold includes dynamically adjusting a single pressure bleed-up threshold; and where each pressure bleed-up threshold is a function of the one or more conditions. 6. The method of claim 1 , wherein the variable vacuum target is determined based on a route the vehicle is travelling including learned conditions including a fuel slosh event. 7. The method of claim 6 , wherein the variable vacuum target is further determined based when the one or more fuel slosh events are predicted to occur during the pressure bleed-up. 8. The method of claim 7 , wherein the variable vacuum target is determined based on a number of fuel slosh events predicted to occur during the pressure bleed-up. 9. The method of claim 1 , wherein the variable vacuum target is determined based on a predicted altitude change on a route the vehicle is traveling. 10. The method of claim 9 , wherein the predicted altitude change is predicted to occur during the pressure bleed-up, and the variable target vacuum is increased as the altitude change increases. 11. The method of claim 1 , wherein the variable vacuum target is determined independent from a predicted altitude change on a route the vehicle is traveling, the predicted altitude change comprising a decrease in altitude.

Assignees

Inventors

Classifications

  • the venting is actuated by specific signals or positions of particular parts · CPC title

  • with vapor recovery means · CPC title

  • Valve arrangements in the vent line · CPC title

  • adapted to avoid loss of fuel or fuel vapour, e.g. with vapour recovery systems · CPC title

  • characterised by venting means · CPC title

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What does patent US11187192B2 cover?
Methods and systems are provided for conducting diagnostics to indicate whether a fuel system and/or an evaporative emissions system of a vehicle has a source of undesired evaporative emissions, or not. A method comprises conducting such a diagnostic via evacuating the fuel system to a target vacuum, then sealing the fuel system from atmosphere and monitoring a pressure bleed-up in the fuel sys…
Who is the assignee on this patent?
Ford Global Tech Llc
What technology area does this patent fall under?
Primary CPC classification F02M25/0818. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 30 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 11 related publications on this page (citations in our corpus or others sharing the same primary CPC).