Active airpath bypass system

US9765734B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9765734-B2
Application numberUS-201414581811-A
CountryUS
Kind codeB2
Filing dateDec 23, 2014
Priority dateDec 23, 2014
Publication dateSep 19, 2017
Grant dateSep 19, 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.

Methods and systems are provided for regulating airflow through a charge air cooler integrated in an intake assembly. In one example, an engine intake assembly comprises a plenum having an integrated charge air cooler (CAC), a first header seal positioned around a circumference of a first CAC header, and a first rotatably movable seal positioned in a bypass passage of the plenum. The first movable seal interfaces via sliding contact with the first header seal and adjusting a position of the first movable seal may vary the amount of airflow through the bypass passage.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method, comprising: adjusting a position of a first seal disposed between an interior wall of a plenum and an exterior wall of a charge air cooler (CAC) to vary air flow through the CAC, the CAC integrated within the plenum, the plenum coupled to engine cylinder intake runners; and during the adjusting, sliding the first seal past a second seal disposed entirely around a first CAC header while maintaining contact with the second seal. 2. The method of claim 1 , wherein the adjusting is based on a temperature of charge air entering the CAC. 3. The method of claim 2 , wherein the adjusting includes adjusting the position of the first seal into a first position where charge air bypasses internal cooling tubes of the CAC and flows around an exterior of the CAC when the charge air entering the plenum is below a threshold temperature, and adjusting the position of the first seal into a second position where charge air flows only through the internal cooling tubes of the CAC and not through a bypass passage disposed between the interior wall of the plenum and the exterior wall of the CAC when the charge air entering the plenum is above the threshold temperature. 4. The method of claim 3 , wherein adjusting the position of the first seal into the first position includes: rotating the first seal in a first direction to move a first end of the first seal away from and out of sealing contact with the exterior wall of the CAC; and flowing charge air through the bypass passage and past the first seal. 5. The method of claim 4 , wherein adjusting the position of the first seal into the second position includes: rotating the first seal in a second direction, opposite the first direction, to move the first end of the first seal toward and into sealing contact with the exterior wall of the CAC and move a second end of the first seal, the second end opposite the first end relative to a rotational axis of the first seal, toward and into sealing contact with the interior wall of the plenum; and flowing charge air through the internal cooling tubes of the CAC only and not through the bypass passage. 6. The method of claim 1 , further comprising flowing coolant through a first coolant inlet of the plenum, through a second coolant inlet of the CAC, through internal coolant tubes of the CAC, out of the CAC through a first coolant outlet of the CAC, and out of a second coolant outlet of the plenum, wherein the first coolant inlet of the plenum and the second coolant inlet of the CAC are aligned and in sealing contact with one another through a first face seal, and wherein the first coolant outlet of the CAC and the second coolant outlet of the plenum are aligned and in sealing contact with one another through a second face seal. 7. The method of claim 1 , wherein the adjusting is performed by an actuator coupled to a rotatable actuating rod, the rotatable actuating rod directly coupled to the first seal and extending along a length of the plenum, the actuator in communication with a controller, and wherein the sliding the first seal past the second seal while maintaining contact with the second seal includes rotating the actuating rod to rotate and slide a first edge of the first seal along an interior face of the second seal and rotate and slide a second edge of the first seal along an interior face of a third seal, the third seal disposed entirely around a second CAC header, the first CAC header and second CAC header positioned at opposite ends of the CAC and plenum.

Assignees

Inventors

Classifications

  • Air intakes; Induction systems · CPC title

  • by bypassing charging air · CPC title

  • for cooling ({F02M31/005 takes precedence; use of cold F02M17/52;} cooling of charging-air or of scavenging-air F02B29/04) · CPC title

  • by bypassing, e.g. partially, intake air from pump inlet to pump outlet · CPC title

  • special shapes or arrangements of plenum chambers; Constructional details · CPC title

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What does patent US9765734B2 cover?
Methods and systems are provided for regulating airflow through a charge air cooler integrated in an intake assembly. In one example, an engine intake assembly comprises a plenum having an integrated charge air cooler (CAC), a first header seal positioned around a circumference of a first CAC header, and a first rotatably movable seal positioned in a bypass passage of the plenum. The first mova…
Who is the assignee on this patent?
Ford Global Tech Llc
What technology area does this patent fall under?
Primary CPC classification F02M35/10052. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Sep 19 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).