Optical effects for aerodynamic microstructures

US9751618B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9751618-B2
Application numberUS-201514705547-A
CountryUS
Kind codeB2
Filing dateMay 6, 2015
Priority dateMay 6, 2015
Publication dateSep 5, 2017
Grant dateSep 5, 2017

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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.

Aerodynamic microstructures having sub-microstructure are disclosed herein. One disclosed example apparatus includes an aerodynamic microstructure defining an external surface of a vehicle, and a pattern of sub-microstructures superimposed on the microstructure to convey a representation of an image.

First claim

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What is claimed is: 1. An apparatus comprising: an aerodynamic microstructure defining an external surface of a vehicle; a first pattern of sub-microstructures superimposed on the microstructure, the first pattern having a first reflective property; and a second pattern of sub-microstructures superimposed on the microstructure, the second pattern having a second reflective property different from the first reflective property, wherein sub-microstructures of the first pattern of sub-microstructures have at least one of a different size or a different orientation from sub-microstructures of the second pattern of sub-microstructures, the first and the second patterns superimposed on the microstructure to convey a representation of a graphic. 2. The apparatus as defined in claim 1 , wherein the sub-microstructures of the second pattern of sub-microstructures have different shapes compared to the sub-microstructures of the first pattern of sub-microstructures. 3. The apparatus as defined in claim 1 , wherein the first and the second sub-microstructure patterns include relatively flat portions of the external surface. 4. The apparatus as defined in claim 1 , wherein spacings between sub-microstructures of the first and the second sub-microstructure patterns are approximately equal to a wavelength of light. 5. The apparatus as defined in claim 1 , wherein surfaces of sub-microstructures of the first and the second sub-microstructure patterns are coated with a reflective coating. 6. The apparatus as defined in claim 1 , wherein spacings between sub-microstructures of the first and the second sub-microstructure patterns are less than about 0.4 microns. 7. The apparatus as defined in claim 1 , further comprising a color layer proximate the external surface. 8. A method comprising: providing a first group of sub-microstructures having a first reflective property on an external surface of a microstructure; and providing a second group of sub-microstructures having a second reflective property on or proximate the external surface, the second reflective property different from the first reflective property, wherein sub-microstructures of the first group of sub-microstructures have at least one of a different size or a different orientation from sub-microstructures of the second group of sub-microstructures to create an optical effect. 9. The method as defined in claim 8 , wherein the external surface spans a plurality of microstructures. 10. The method as defined in claim 8 , wherein providing the first or the second groups of the sub-microstructures comprises embossing sub-microstructures onto the external surface. 11. The method as defined in claim 8 , further comprising aligning a tool to provide the first group of sub-microstructures and re-aligning or moving the tool to provide the second group of sub-microstructures. 12. The method as defined in claim 8 , wherein distances between sub-microstructures of the first or second sub-microstructure groups are between about 0.4 and 0.7 microns. 13. A method comprising: providing a first group of sub-microstructures having a first reflective property on an external surface of a microstructure; and providing a second group of sub-microstructures having a second reflective property on or proximate the external surface, the second reflective property different from the first reflective property, wherein sub-microstructures of the first group of sub-microstructures have at least one of a different size or a different orientation from sub-microstructures of the second group of sub-microstructures to create an optical effect. 14. The method as defined in claim 13 , wherein providing the sub-microstructures comprises directing a tool to provide sub-microstructures of differing dimensions at different positions on the surface. 15. The method as defined in claim 13 , wherein sub-microstructures of the first and the second sub-microstructure patterns have one or more of a parabolic shape, a triangular shape, a grooved shape, a sinusoidal shape, a cone shape, a cylindrical shape, or a plurality of indentations. 16. The method as defined in claim 13 , wherein distances between sub-microstructures of the first and the second sub-microstructure patterns are between about 0.4 and 0.7 microns. 17. An apparatus comprising: an aerodynamic microstructure defining an external surface of an aircraft, comprising: a first sub-microstructure group superimposed on the aerodynamic microstructure, the first sub-microstructure group having a first reflective property; and a second sub-microstructure group superimposed on the aerodynamic microstructure, the second sub-microstructure group having a second reflective property, the second reflective property different from the first reflective property, wherein sub-microstructures of the first sub-microstructure group have at least one of a different size or a different orientation from sub-microstructures of the second sub-microstructure group, a combination of the first and the second sub-microstructure groups to convey a representation of a graphic. 18. The apparatus as defined in claim 17 , wherein the sub-microstructures of the second sub-microstructure group have different shapes compared to the sub-microstructures of the first group of sub-microstructures. 19. The apparatus as defined in claim 17 , further comprising a flat portion of the aerodynamic microstructure to at least partially convey the representation.

Assignees

Inventors

Classifications

  • on synthetic resin layer or on natural or synthetic rubber layer · CPC title

  • B42D25/324Primary

    Reliefs · CPC title

  • produced by reflected light, e.g. matt surfaces, lustrous surfaces · CPC title

  • the advertising matter being arranged on the aircraft · CPC title

  • Translucent · CPC title

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Frequently asked questions

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What does patent US9751618B2 cover?
Aerodynamic microstructures having sub-microstructure are disclosed herein. One disclosed example apparatus includes an aerodynamic microstructure defining an external surface of a vehicle, and a pattern of sub-microstructures superimposed on the microstructure to convey a representation of an image.
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B42D25/324. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Sep 05 2017 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 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).