Internal combustion engine and method for manufacturing the same

US10408174B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10408174-B2
Application numberUS-201315039010-A
CountryUS
Kind codeB2
Filing dateNov 27, 2013
Priority dateNov 27, 2013
Publication dateSep 10, 2019
Grant dateSep 10, 2019

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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.

There is provided an internal combustion engine in which respective combustion states of cylinders can be uniformized with a simple configuration. A central axis (CL1) of a connecting part (7) of one of air supply ports (5) inclines with a predetermined inclination angle in a direction away from an air supply inlet (3) with respect to a y direction orthogonal to an x direction in which an air supply manifold 1 extends, and an inclination angle of the connecting part (7) of the one of the air supply ports (5) is larger than an inclination angle of the connecting part (7) of other air supply ports (5) located on a side closer to the air supply inlet (3) than the one of the air supply ports (5).

First claim

Opening claim text (preview).

The invention claimed is: 1. An internal combustion engine comprising: an air supply manifold extending in one direction; a plurality of cylinders arranged at a predetermined interval in the one direction in which the air supply manifold extends; a plurality of swirl chambers connected to ends of the respective cylinders to form swirls; and an air supply port including a connecting part arranged on one side surface of the air supply manifold and a swirl chamber introduction part that connects the connecting part and the swirl chamber in a downstream side of the connecting part, a plurality of air supply ports being provided with respect to the air supply manifold, wherein an air supply inlet for supplying air into the air supply manifold is provided on an end of the air supply manifold, air that is supplied from the air supply inlet to the air supply manifold flows along the one direction in which the air supply manifold extends, connecting parts of respective air supply ports are arranged on the one side surface of the air supply manifold along the one direction in which the air supply manifold extends at an interval in the one direction, a central axis of the connecting part of one of the air supply ports inclines with a predetermined inclination angle in a direction away from the air supply inlet with respect to an orthogonal direction orthogonal to the one direction in which the air supply manifold extends, and the inclination angle of the central axis of the connecting part of the one of the air supply ports provided on the air supply manifold is larger than an inclination angle of the central axis of the connecting part of other air supply ports located on a side closer to the air supply inlet than the one of the air supply ports. 2. The internal combustion engine according to claim 1 , wherein the inclination angles are sequentially set such that the inclination angle of the connecting part of the air supply port located farther from the air supply inlet is greater than the inclination angles of the central axis of the air supply ports located closer to the air supply inlet. 3. The internal combustion engine according to claim 1 , wherein the connecting parts are manufactured by an air supply manifold mold for forming the air supply manifold, and the swirl chamber introduction parts are manufactured by a cylinder head mold for forming the swirl chambers and the ends of the cylinders. 4. A method for manufacturing an internal combustion engine, the internal combustion engine including: an air supply manifold extending in one direction; a plurality of cylinders arranged at a predetermined interval in the one direction in which the air supply manifold extends; a plurality of swirl chambers connected to ends of the respective cylinders to form swirls; and an air supply port including a connecting part arranged on one side surface of the air supply manifold and a swirl chamber introduction part that connects the connecting part and the swirl chamber in a downstream side of the connecting part, a plurality of air supply ports being provided with respect to the air supply manifold, wherein an air supply inlet for supplying air into the air supply manifold is provided on an end of the air supply manifold, air that is supplied from the air supply inlet to the air supply manifold flows along the one direction in which the air supply manifold extends, connecting parts of respective air supply ports are arranged on the one side surface of the air supply manifold along the one direction in which the air supply manifold extends at an interval in the one direction, a central axis of the connecting part of one of the air supply ports inclines with a predetermined inclination angle in a direction away from the air supply inlet with respect to an orthogonal direction orthogonal to the one direction in which the air supply manifold extends, the inclination angle of the central axis of the connecting part of the one of the air supply ports provided on the air supply manifold is larger than an inclination angle of the central axis of the connecting part of other air supply ports located on a side closer to the air supply inlet than the one of the air supply ports, the method comprising: a connecting part manufacturing step of manufacturing the connecting parts by an air supply manifold mold for forming the air supply manifold; a swirl chamber introduction part manufacturing step of manufacturing the swirl chamber introduction parts by a cylinder head mold for forming the swirl chamber and the ends of the cylinder; and an air supply port manufacturing step of connecting the connecting parts and the swirl chamber introduction parts to manufacture the air supply ports. 5. The internal combustion engine according to claim 2 , wherein the air supply ports are formed by connecting the connecting parts and the swirl chamber introduction parts located on sides closer to the swirl chambers than the connecting parts, the connecting parts are manufactured by an air supply manifold mold for forming the air supply manifold, and the swirl chamber introduction parts are manufactured by a cylinder head mold for forming the swirl chambers and the ends of the cylinders.

Assignees

Inventors

Classifications

  • characterised by the charge distribution between the cylinders/combustion chambers or its homogenisation · CPC title

  • Moulding, casting or the like · CPC title

  • Intake runners · CPC title

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

  • of intake channels · CPC title

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Frequently asked questions

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What does patent US10408174B2 cover?
There is provided an internal combustion engine in which respective combustion states of cylinders can be uniformized with a simple configuration. A central axis (CL1) of a connecting part (7) of one of air supply ports (5) inclines with a predetermined inclination angle in a direction away from an air supply inlet (3) with respect to a y direction orthogonal to an x direction in which an air s…
Who is the assignee on this patent?
Mitsubishi Heavy Ind Engine & Turbocharger Ltd
What technology area does this patent fall under?
Primary CPC classification F02M35/10262. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Sep 10 2019 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).