Precision air flow routing devices and method for thermal spray coating
US-11879173-B2 · Jan 23, 2024 · US
US9316173B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9316173-B2 |
| Application number | US-201414332586-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 16, 2014 |
| Priority date | Jul 16, 2013 |
| Publication date | Apr 19, 2016 |
| Grant date | Apr 19, 2016 |
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Official abstract text for this publication.
A cylinder liner for an engine block assembly of an internal combustion engine is provided. The cylinder liner includes a liner member formed of cast iron and presenting an outer surface. A first portion of the outer surface of the liner member is machined to a reduced outside diameter. An aluminum-based material is then thermally sprayed onto the machined first portion, while a second portion of the outer surface remains uncoated. The coated cylinder liner is then placed in a mold, and another aluminum-based material is cast around the coated cylinder liner to form the engine block assembly. During the casting process, the two aluminum-based materials form a strong intermetallic bond between the liner member and the engine block.
Opening claim text (preview).
What is claimed is: 1. A cylinder liner comprising, a liner member extending longitudinally from a top end to a bottom end and presenting a length between said top and bottom ends; said liner member including an inside surface extending around a center axis and an oppositely facing outside surface; said outside surface presenting a first outside diameter along a first portion of said length and a second outside diameter along a second portion of said length, said first outside diameter being less than said second outside diameter; and a bonding layer formed of an aluminum-based material applied to said outside surface along said first portion, wherein said bonding layer of an aluminum-based material is applied to said outside surface by thermal spraying. 2. The cylinder liner of claim 1 , wherein said liner member is formed of a metal material different from said aluminum-based material. 3. The cylinder liner of claim 1 , wherein said outside surface presents a plurality of depressions each having a depth of not greater than 1 millimeter along said first portion. 4. The cylinder liner of claim 1 , wherein said first portion is 10 to 50% of said length of said outside surface. 5. The cylinder liner of claim 1 , wherein said first portion of said outside surface is located adjacent to one of said ends of said liner member and said second portion extends from said first portion to the opposite end of said liner member. 6. The cylinder liner of claim 1 , wherein said liner member is formed of cast iron; said inside surface of said liner member extends circumferentially around said center axis and presents a cylindrical-shaped opening extending from said top end to said bottom end; said length of said liner member is from 100 millimeters to 150 millimeters; said first portion of said outside surface is 10 to 50% of said length of said liner member; said outside surface is machined a distance radially relative to said center axis to present said first outside diameter being less than said second outside diameter; said outside surface presents a plurality of depressions each having a depth of not greater than 1 millimeter along said first portion; said liner member has a thickness extending from said inside surface to said outside surface, said thickness is at least 1.8 millimeters along said first portion, and said thickness along said first portion is 10 to 15 millimeters less than said thickness along said second portion; said bonding layer covers said outside surface along said first portion entirely; said aluminum-based material of said bonding layer is an aluminum alloy; said aluminum alloy includes aluminum in an amount of 85 to 90 weight percent (wt. %), silicon in an amount of 10 to 15 wt. %, oxygen in an amount of 0.05 to 0.15 wt. %, and optionally Fe, Mg, Zn, and Mn in a total amount less than 1 wt. %, based on the total weight of said aluminum alloy; said bonding layer has a porosity of less than 5%, a thermal conductivity of 80 to 120 W/mK at 50 to 400° C., a thermal expansion coefficient of 20 to 24×10 −6 /K at 20 to 150° C., a tensile strength of at least 170 MPa, and an elastic modulus of 40 to 70 GPa; and said bonding layer has a thickness of not greater than 15 millimeters. 7. A method of manufacturing a cylinder liner, comprising the steps of: providing a liner member extending longitudinally from a top end to a bottom end and presenting a length between the top and bottom ends, the liner member including an inside surface extending around a center axis and an oppositely facing outside surface, the outside surface presenting a first outside diameter along a first portion of the length and a second outside diameter along a second portion of the length, and the first outside diameter being less than the second outside diameter; and applying a layer of an aluminum-based material to the outside surface along the first portion of the length, wherein the step of applying the layer of the aluminum-based material to the outside surface includes thermally spraying the aluminum-based material onto the outside surface. 8. The method of claim 7 , including reducing the first outside diameter along the first portion so that the first outside diameter is less than the second outside diameter. 9. The method of claim 7 , including shot-blasting the outside surface along the first portion to form a plurality of depressions each having a depth of not greater than 1 millimeter. 10. The method of claim 7 , wherein the liner member is formed of a metal material different from the aluminum-based material. 11. An engine block assembly, comprising: a plurality of cylinder liners, each cylinder liner including a liner member extending longitudinally from a top end to a bottom end and presenting a length between said top and bottom ends, said liner member including an inside surface extending around a center axis and an oppositely facing outside surface, said outside surface presenting a first outside diameter along a first portion of said length and a second outside diameter along a second portion of said length, and said first outside diameter being less than said second outside diameter; each of said cylinder liners including a layer of a first aluminum-based material applied to said outside surface along said first portion, wherein said layers of a first aluminum-based material are applied to said outside surfaces of said cylinder liners by thermal spraying; a block formed of a second aluminum-based material and presenting a plurality of bores each for receiving one of said cylinder liners; and said first aluminum-based material of said cylinder liners being bonded to said second aluminum-based material of said block. 12. The engine block assembly of claim 11 , wherein said first aluminum-based material of said cylinder liners is the same as said second aluminum-based material of said block. 13. The engine block assembly of claim 11 , wherein said liner member is formed of a metal material different from said aluminum-based materials of said layer and said block. 14. An engine block assembly, comprising: a plurality of cylinder liners, each cylinder liner including a liner member extending longitudinally from a top end to a bottom end and presenting a length between said top and bottom ends, said liner member including an inside surface extending around a center axis and an oppositely facing outside surface, said outside surface presenting a first outside diameter along a first portion of said length and a second outside diameter along a second portion of said length, and said first outside diameter being less than said second outside diameter: each of said cylinder liners including a layer of a first aluminum-based material applied to said outside surface along said first portion; a block formed of a second aluminum-based material and presenting a plurality of bores each for receiving one of said cylinder liners; and said first aluminum-based material of said cylinder liners being bonded to said second aluminum-based material of said block, wherein said block presents a cooling chamber spaced from each of said bores by said second aluminum-based material, said block includes an upper surface presenting a plurality of bridge areas, each bridge area is planar and located between adjacent bores, said block includes a plurality of cooling passages each extending from said cooling chamber and through a portion of said block between said bores for conveying cooling fluid from said cooling chamber. 15. A method of manufacturing an engine block assembly, comprising the steps of: providing a plurality of cyli
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