LAMINATE FOR REDUCING FLOW RESISTANCE AND MANUFACTURING METHOD THEREFOR
20180346840 ยท 2018-12-06
Assignee
Inventors
- Jeung Sang Go (Busan, KR)
- Hyun-jong Paik (Busan, KR)
- Kyung Chun KIM (Busan, KR)
- Sang Youl Yoon (Busan, KR)
Cpc classification
F15D1/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C10M111/04
CHEMISTRY; METALLURGY
C10M101/00
CHEMISTRY; METALLURGY
B05D5/08
PERFORMING OPERATIONS; TRANSPORTING
B05D5/02
PERFORMING OPERATIONS; TRANSPORTING
B32B3/26
PERFORMING OPERATIONS; TRANSPORTING
B32B5/18
PERFORMING OPERATIONS; TRANSPORTING
F15D1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C10M107/24
CHEMISTRY; METALLURGY
International classification
C10M111/04
CHEMISTRY; METALLURGY
B05D1/00
PERFORMING OPERATIONS; TRANSPORTING
C10M101/00
CHEMISTRY; METALLURGY
Abstract
There is provided a flow-resistance reducing laminate comprising: a substrate; and a flow-resistance reducing layer formed on the substrate, wherein the flow-resistance reducing layer has a surface portion facing a liquid, wherein a flow interface is formed between the liquid and the laminate upon relative movement between the liquid and the laminate, wherein the flow-resistance reducing layer is configured such that an air layer defines the flow interface.
Claims
1. A flow-resistance reducing laminate comprising: a substrate; and a flow-resistance reducing layer formed on the substrate, wherein the flow-resistance reducing layer has a surface portion facing a liquid, wherein a flow interface is formed between the liquid and the laminate upon relative movement between the liquid and the laminate, wherein the flow-resistance reducing layer is configured such that an air layer defines the flow interface.
2. The flow-resistance reducing laminate of claim 1, wherein the surface portion of the flow-resistance reducing layer has a plurality of cavities defined therein, wherein when the surface portion faces the liquid, the air is filled in the cavities, wherein the shape of each of the cavities is configured such that when the flow interface is formed, the air filled in each cavity is kept trapped therein.
3. The flow-resistance reducing laminate of claim 2, wherein each cavity has a spherical shape having an open portion defined therein toward the liquid, wherein a length of the open portion of the cavity toward the liquid is smaller than a radius of the spherical cavity so that the air filled in the cavity is kept trapped therein.
4. The flow-resistance reducing laminate of claim 2, wherein each cavity has a cylindrical shape having a rounded edge and having a first depth and having an opened portion; or each cavity has a rectangular cross-section shape having rounded corners and edges and having the first depth and an opened portion, wherein a relationship between a length of the open portion of the cavity toward the liquid and the first depth is defined so that the air filled in the cavity is kept trapped therein.
5. The flow-resistance reducing laminate of claim 1, wherein the flow-resistance reducing layer includes a support layer in contact with the substrate, wherein a plurality of hollow micro-capsules is dispersed in the support layer or in a surface portion of the support layer, wherein each hollow micro-capsule is partially open to define a corresponding cavity.
6. The flow-resistance reducing laminate of claim 2 or 5, wherein an inner face of each cavity surface is water repellent to form the air layer.
7. The flow-resistance reducing laminate of claim 6, wherein a shell of each hollow micro-capsule has gas-blocking property to allow expansion; or the shell is brittle to enable rupture thereof at a notch point thereof by expansion.
8. A method of manufacturing a sheet having a plurality of cavities defined in a surface portion thereof, the method comprising: providing a plurality of micro-capsules carrying a thermally expandable material therein, wherein each capsule has a shell surrounding the thermally expandable material; dispersing the plurality of micro-capsules in a support layer; floating at least some of the hollow micro-capsules upwardly into a surface portion of the support layer such that said at least some of the micro-capsules are exposed upwardly; expanding the thermally expandable material contained in the shells by heating the exposed micro-capsules; and rupturing an exposed portion of the shell of each micro-capsule by the expansion to hollow each capsule to form a corresponding cavity.
9. The method of claim 8, wherein when the micro-capsules are dispersed in the support layer, the micro-capsules are in close contact with each other, such that each of the capsule has a cylindrical shape having a rounded edge or a rectangular cross-section shape having rounded corners and edges.
10. The method of claim 8, wherein the support layer includes a liquid-phase or gel-phase support layer precursor, wherein dispersing the plurality of micro-capsules in the support layer includes dispersing the plurality of micro-capsules in the liquid-phase or gel-phase support layer precursor, wherein heating the exposed micro-capsules includes curing the liquid-phase or gel-phase support layer precursor.
11. The method of claim 8, wherein the support layer includes a liquid-phase or gel-phase support layer precursor, wherein dispersing the plurality of micro-capsules in the support layer includes dispersing the plurality of micro-capsules in the liquid-phase or gel-phase support layer precursor, wherein heating the exposed micro-capsules includes curing the liquid-phase or gel-phase support layer precursor, wherein the method further comprises applying the liquid-phase or gel-phase support layer precursor having the plurality of micro-capsules dispersed therein onto a surface of a substrate.
12. The method of claim 8, wherein the shell of each micro-capsule is water-repellent.
13. The method of claim 8, wherein the thermally expandable material is un-permeable through the shell of the micro-capsule such that the shell is ruptured by the thermal expansion of the thermally expandable material.
14. The method of claim 8, wherein the shell of the micro-capsule is brittle such that the shell is ruptured by the thermal expansion of the thermally expandable material.
15. The method of claim 8 or 10, wherein the shell of the micro-capsule is non-dissolved into the support layer or the support layer precursor.
16. The method of claim 8, wherein the thermally expandable material surrounded by the shell includes a thermally expandable gas, oil and/or liquid.
17. The method of claim 8, wherein the thermally expandable material surrounded by the shell has a lower specific gravity than a material of the support layer.
18. A self-cleaning sheet comprising the flow-resistance reducing laminate of claim 1.
19. A soundproof sheet comprising the flow-resistance reducing laminate of claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTIONS
[0041] Examples of various embodiments are illustrated and described further below. It will be understood that the description herein is not intended to limit the claims to the specific embodiments described. On the contrary, it is intended to cover alternatives, modifications, and equivalents as may be included within the spirit and scope of the present disclosure as defined by the appended claims. The same reference numbers in different figures denote the same or similar elements, and as such perform similar functionality.
[0042] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms a and an are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms comprises, comprising, includes, and including when used in this specification, specify the presence of the stated features, integers, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, operations, elements, components, and/or portions thereof.
[0043] Unless otherwise defined, all terms including technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this inventive concept belongs. It will be further understood that terms, such as those defined in commonly used dictionaries, should be interpreted as having a meaning that is consistent with their meaning in the context of the relevant art and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein.
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[0045] The cavity 130 in accordance with the present invention may be configured to define the recessed space having a circular shape (see
[0046] As seen from
[0047] Further, as illustrated in
[0048] In particular, it is desirable that the surface forming this cavity may be water repellent so that the cavity maintains air therein and the air layer forms well as the fluid moves.
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[0050] The flow-resistance reducing layer, having a support layer 120 designated as paint in
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Example 1
[0053] The oil-contained micro-capsule and PVA (polyvinyl alcohol) were dispersed at a ratio of 1:1. The micro-capsules were well dispersed in the PVA. This capsule-dispersed PVA was spin-coated onto the silicon surface. The specific gravity of the oil was smaller than the specific gravity of the PVA, so that the micro-capsule floated toward the PVA surface, and the PVA was cured after a certain time. See the SEM picture of
[0054] While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the following claims.