Exhaust manifold constructions including thermal barrier coatings for opposed-piston engines

US11098634B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11098634-B2
Application numberUS-202016783067-A
CountryUS
Kind codeB2
Filing dateFeb 5, 2020
Priority dateAug 18, 2017
Publication dateAug 24, 2021
Grant dateAug 24, 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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Abstract

Official abstract text for this publication.

An exhaust manifold assembly with a thermal barrier coating for an opposed-piston engine reduces heat rejection to coolant, while increasing exhaust temperatures, fuel efficiency, and quicker exhaust after-treatment light-off. The exhaust manifold assembly can include a coating on the inside surface of the manifold assembly. The coated exhaust manifold assembly can ensure structural robustness of the exhaust manifold assembly over a larger range of operating temperatures.

First claim

Opening claim text (preview).

What is claimed is: 1. An opposed-piston engine comprising: an engine block; a plurality of cylinders disposed in the engine block, each cylinder including a cylinder wall having an interior surface defining a bore centered on a longitudinal axis of the cylinder and an intake port and an exhaust port formed in the cylinder wall near respective opposite ends of the cylinder, the intake and exhaust ports each including an array of port openings extending through the cylinder wall to the bore; an exhaust manifold assembly comprising at least one exhaust pipe, and, for each cylinder, a pair of runner portions forming a runner plenum in the engine block that surrounds the exhaust port openings of the cylinder, each runner portion connected to a respective runner, at least one runner connected to the at least one exhaust pipe; and, a coating layer on an inside surface of the exhaust manifold assembly that reduces heat transfer from exhaust gas to the engine block. 2. The opposed-piston engine of claim 1 , wherein the exhaust manifold assembly includes a base metal that comprises gray iron. 3. The opposed-piston engine of claim 1 , wherein the coating layer comprises a thermally insulating material. 4. The opposed-piston engine of claim 3 , wherein the thermally insulating material has a coefficient of thermal conductivity between 1 and 8 W/(m·K). 5. The opposed-piston engine of claim 3 , wherein the coating layer comprises any one of zirconia, alumina, a chrome-containing composition, a cobalt-containing composition, a nickel-containing composition, and an yttrium-containing composition, or any combination thereof. 6. The opposed-piston engine of claim 3 , wherein the coating layer is spray deposited or dip coating deposited onto the inside surface of the exhaust manifold assembly. 7. The opposed-piston engine of claim 1 , wherein the plurality of cylinders being disposed in an inline array. 8. The opposed-piston engine of claim 7 , wherein each cylinder comprises a liner retained in a tunnel in the cylinder block. 9. The opposed-piston engine of any one of claims 1 or 7 , wherein the at least one exhaust pipe being in fluid communication with one or more of: a turbine inlet; an EGR inlet; and an exhaust treatment system. 10. A method of making an exhaust manifold assembly for an opposed-piston engine with a plurality of cylinders disposed in an engine block, comprising: providing an exhaust manifold assembly comprising at least one exhaust pipe, and, for each cylinder, a pair of runner portions forming a runner plenum in the engine block that surrounds exhaust port openings of the cylinder, each runner portion connected to a respective runner, at least one runner connected to the at least one exhaust pipe: and, applying a coating layer comprising a material having a thermal conductivity between 1 and 8 W/(m·K) to an interior surface of the exhaust manifold. 11. The method of claim 10 , further comprising preparing the interior surface of the exhaust manifold assembly for application of the coating layer. 12. The method of either claim 10 or 11 , further comprising treating the exhaust manifold assembly after application of the coating layer.

Assignees

Inventors

Classifications

  • F01N13/00Primary

    Exhaust or silencing apparatus characterised by constructional features · CPC title

  • Engines with oppositely-moving reciprocating working pistons · CPC title

  • Selection of particular materials · CPC title

  • Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders (arranged oppositely relative to main shaft F02B75/24) · CPC title

  • for thermal insulation · CPC title

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What does patent US11098634B2 cover?
An exhaust manifold assembly with a thermal barrier coating for an opposed-piston engine reduces heat rejection to coolant, while increasing exhaust temperatures, fuel efficiency, and quicker exhaust after-treatment light-off. The exhaust manifold assembly can include a coating on the inside surface of the manifold assembly. The coated exhaust manifold assembly can ensure structural robustness …
Who is the assignee on this patent?
Achates Power Inc
What technology area does this patent fall under?
Primary CPC classification F01N13/00. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 24 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 9 related publications on this page (citations in our corpus or others sharing the same primary CPC).