Air Duct Arrangement and Cooler

US2018094571A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2018094571-A1
Application numberUS-201715725865-A
CountryUS
Kind codeA1
Filing dateOct 5, 2017
Priority dateOct 5, 2016
Publication dateApr 5, 2018
Grant date

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The invention relates to an air duct arrangement ( 100 ), in particular a charge air duct for a turbocharged engine, having an inlet air duct ( 60 ), a cooler ( 10 ) with an inlet ( 37 ) and an outlet ( 38 ), the cooler ( 10 ) having at least one air flow path portion ( 12, 14, 16, 18 ) extending between the inlet ( 37 ) and the outlet ( 38 ) along a longitudinal elongation ( 66 ) of the cooler ( 10 ) and having an outlet aperture ( 13, 15, 17, 19 ), and at least two runners ( 22, 24, 26, 28 ) of an air intake manifold ( 20 ) of an engine ( 40 ). The cooler ( 10 ) is arranged between the inlet air duct ( 60 ) and the runners ( 22, 24, 26, 28 ). Each runner ( 22, 24, 26, 28 ) has an inlet aperture ( 23, 25. 27, 29 ) and the outlet ( 38 ) of the cooler ( 10 ) is providing connection interfaces ( 73, 75, 77, 79 ) for the inlet apertures ( 23, 25. 27, 29 ) of the runners ( 22, 24, 26, 28 ).

First claim

Opening claim text (preview).

What is claimed is: 1 . A charge air duct for a turbocharged engine, comprising: an inlet air duct ( 60 ); a cooler ( 10 ) having an inlet ( 37 ) and an outlet ( 38 ), the cooler ( 10 ) having at least one air flow path portion ( 12 , 14 , 16 , 18 ) along a longitudinal elongation ( 66 ) of the cooler ( 10 ) and having an outlet aperture ( 13 , 15 , 17 , 19 ); and at least two runners ( 22 , 24 , 26 , 28 ) of an air intake manifold ( 20 ) of an engine ( 40 ); wherein the cooler ( 10 ) is arranged between the inlet air duct ( 60 ) and the runners ( 22 , 24 , 26 , 28 ); wherein each runner ( 22 , 24 , 26 , 28 ) has an inlet aperture ( 23 , 25 . 27 , 29 ); wherein the outlet ( 38 ) of the cooler ( 10 ) provides connection interfaces ( 73 , 75 , 77 , 79 ) for the inlet apertures ( 23 , 25 . 27 , 29 ) of the runners ( 22 , 24 , 26 , 28 ). 2 . The charge air duct according to claim 1 , wherein the cooler ( 10 ) is configured to provide an air flow being predominantly parallel to the longitudinal elongation ( 66 ) between the inlet ( 37 ) and the outlet ( 38 ) of the cooler ( 10 ). 3 . The charge air duct according to claim 2 , wherein at least two air flow path portions ( 12 , 14 , 16 , 18 ) are provided between the inlet ( 37 ) and the outlet ( 38 ) of the cooler ( 10 ); and at least one of the air flow path portions ( 12 , 14 , 16 , 18 ) is connected with its outlet aperture ( 13 , 15 , 17 , 19 ) to the inlet aperture ( 23 , 25 . 27 , 29 ) of one of the runners ( 22 , 24 , 26 , 28 ). 4 . The charge air duct according to claim 2 , further including air guiding walls ( 30 , 32 , 34 , 36 ) arranged in the cooler ( 10 ), such that an air flow from the inlet air duct ( 60 ) through the cooler ( 10 ) is split and guided along separate air flow path portions ( 12 , 14 , 16 , 18 ) through the cooler ( 10 ) to the connection interfaces ( 73 , 75 , 77 , 79 ) for the runners ( 22 , 24 , 26 , 28 ). 5 . The charge air duct according to claim 4 , wherein a length ( 62 ) of the air guiding wall ( 30 , 32 , 34 , 36 ) is in a range of zero to a total length ( 64 ) of the air flow path portions ( 12 , 14 , 16 , 18 ). 6 . The charge air duct according to claim 4 , wherein the air guiding wall has a shape configured to provide a smooth air flow into the respective runner ( 22 , 24 , 26 , 28 ). 7 . The charge air duct according to claim 1 , wherein an outlet aperture ( 61 ) of the inlet air duct ( 60 ) covers the inlet ( 37 ) of the cooler ( 10 ). 8 . The charge air duct according claim 7 , wherein the outlet aperture ( 61 ) of the inlet air duct ( 60 ) covers inlet apertures ( 83 , 85 , 87 , 89 ) of the air flow path portions ( 12 , 14 , 16 , 18 ). 9 . The charge air duct according to claim 1 , wherein the inlet air duct ( 60 ) provides at least two gas flow channels ( 67 , 68 , 69 , 70 ) at least partially along its longitudinal elongation. 10 . The charge air duct according to claim 9 , wherein the gas flow channels ( 67 , 68 , 69 , 18 ) correspond to the inlet apertures ( 83 , 85 , 87 , 89 ) of the air flow path portions ( 12 , 14 , 16 , 18 ). 11 . The charge air duct according to claim 1 , wherein the inlet apertures ( 23 , 25 , 27 , 29 ) of the runners ( 22 , 24 , 26 , 28 ) are connected to the connection interfaces ( 73 , 75 , 77 , 79 ) at the outlet ( 38 ) of the cooler ( 10 ) in a rigid and/or gas-tight manner. 12 . The charge air duct according to claim 11 , wherein the inlet apertures ( 23 , 25 , 27 , 29 ) of the runners ( 22 , 24 , 26 , 28 ) are sealed with gaskets ( 54 ) to the connection interfaces ( 73 , 75 , 77 , 79 ) at the outlet ( 38 ) of the cooler ( 10 ). 13 . The charge air duct according to claim 11 , wherein the runners ( 22 , 24 , 26 , 28 ) are fixed to the connection interfaces ( 73 , 75 , 77 , 79 ) at the outlet ( 38 ) of the cooler ( 10 ) by one of gluing, welding, press fit. 14 . The charge air duct according to claim 1 , wherein the air path of the cooler ( 10 ) is composed of parallel air flow path portions ( 12 , 14 , 16 , 18 ). 15 . The charge air duct according to claim 1 , wherein the runners ( 22 , 24 , 26 , 28 ) are at least partially made with a shape decomposition inside the cooler ( 10 ). 16 . The charge air duct according to claim 1 , wherein the cooler ( 10 ) is a water charge air cooler. 17 . A cooler ( 10 ) for a charge air duct ( 100 ) according to claim 1 , wherein the cooler ( 10 ) has an inlet ( 37 ) and an outlet ( 38 ) and a longitudinal elongation ( 66 ) between the inlet ( 37 ) and the outlet ( 38 ), wherein an air flow path is provided between the inlet ( 37 ) and the outlet ( 38 ). 18 . The cooler according to claim 17 , wherein at least two air flow path portions ( 12 , 14 , 16 , 18 ) are arranged in parallel and providing an air flow predominantly in parallel with the longitudinal elongation ( 66 ). 19 . The cooler according to claim 18 , wherein the at least two air flow path portions ( 12 , 14 , 16 , 18 ) are separated at least partially by air guiding walls ( 30 , 32 , 34 , 36 ). 20 . The cooler according to claim 19 , wherein at least one of the air guiding walls ( 30 , 32 , 34 , 36 ) is shorter than the total length ( 66 ) of the air flow path portions ( 12 , 14 , 16 , 18 ). 21 . The cooler according to claim 19 , wherein at least one of the air guiding walls ( 30 , 32 , 34 , 36 ) is as long as the total length ( 66 ) of the air flow path portions ( 12 , 14 , 16 , 18 ).

Assignees

Inventors

Classifications

  • Multiple heat exchangers arranged in parallel or in series · CPC title

  • the conduits having a non-circular cross-section · CPC title

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

  • F02B29/045Primary

    Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly · CPC title

  • Charged air coolers · CPC title

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What does patent US2018094571A1 cover?
The invention relates to an air duct arrangement ( 100 ), in particular a charge air duct for a turbocharged engine, having an inlet air duct ( 60 ), a cooler ( 10 ) with an inlet ( 37 ) and an outlet ( 38 ), the cooler ( 10 ) having at least one air flow path portion ( 12, 14, 16, 18 ) extending between the inlet ( 37 ) and the outlet ( 38 ) along a longitudinal elongation ( 66 ) of the cooler…
Who is the assignee on this patent?
Mann & Hummel Gmbh
What technology area does this patent fall under?
Primary CPC classification F02B29/045. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Apr 05 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).