Laminate
US-2024336047-A1 · Oct 10, 2024 · US
US2016101594A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016101594-A1 |
| Application number | US-201514879035-A |
| Country | US |
| Kind code | A1 |
| Filing date | Oct 8, 2015 |
| Priority date | Oct 8, 2014 |
| Publication date | Apr 14, 2016 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A self-transforming structure is formed from a flexible, fibrous composite having a weave pattern of fibers woven at intersecting angles, the weave pattern having a boundary and one or more axes for the fibers, and an added material coupled to the flexible, fibrous composite to form a structure, wherein the flexible, fibrous composite and the added material have different expansion or contraction rates in response to an external stimulus to cause the structure to self-transform, and wherein the added material has a grain pattern oriented relative the weave pattern of the flexible, fibrous composite. Applications of the self-transforming structures include aviation, automotive, apparel/footwear, furniture, and building materials. One particular example is for providing adaptive control of fluid flow, such as in a jet engine air inlet.
Opening claim text (preview).
1 . A self-transforming structure comprising: a) a flexible, fibrous composite having a boundary and fibers along one or more axes that form a weave pattern; and b) an added material having a grain pattern, the added material coupled to the flexible, fibrous composite to form a structure, wherein the flexible, fibrous composite and the added material have different expansion or contraction rates in response to an external stimulus to cause the structure to self-transform, and wherein the grain pattern of the added material is oriented relative the weave pattern of the flexible, fibrous composite, the self-transformation of the structure responsive to the external stimulus being thereby predictable. 2 . The self-transforming structure of claim 1 , wherein the flexible, fibrous composite is carbon fiber, glass fiber, basalt fiber, liquid crystal polymers, and hybrids thereof. 3 . The self-transforming structure of claim 1 , wherein the weave pattern of the flexible, fibrous composite is biaxial. 4 . The self-transforming structure of claim 3 , wherein the grain pattern of the added material is orthogonal to an axis of a fiber of the flexible, fibrous composite. 5 . The self-transforming structure of claim 3 , wherein the grain pattern of the added material is 45° to an axis of a fiber of the flexible, fibrous composite. 6 . The self-transforming structure of claim 3 , wherein the grain of the added material is oriented at a 45° angle to a boundary of the flexible, fibrous composite. 7 . The self-transforming structure of claim 3 , wherein the grain of the added material is orthogonal to a boundary of the flexible, fibrous composite. 8 . The self-transforming structure of claim 3 , wherein the length of the boundary of the added material is shorter than the length of the boundary of the flexible, fibrous composite. 9 . The self-transforming structure of claim 3 , wherein the length of the boundary of the added material is the same as the length of the boundary of the flexible, fibrous composite. 10 . The self-transforming structure of claim 3 , wherein the fibers of the flexible, fibrous added material are oriented at 45° angles relative to the boundary of the flexible, fibrous composite. 11 . The self-transforming structure of claim 3 , wherein the fibers of the flexible, fibrous added material are orthogonal to the boundary of the flexible, fibrous composite. 12 . The self-transforming structure of claim 3 , wherein the flexible, fibrous composite is square, rectangular, round, or an arbitrary shape. 13 . The self-transforming structure of claim 3 , wherein the flexible, fibrous composite is rectangular. 14 . The self-transforming structure of claim 3 , wherein: a) the grain of the added material is orthogonal to an axis of a fiber of the flexible, fibrous composite; b) the grain of the added material is oriented at 45° relative to the boundary of the flexible, fibrous composite; c) the length of the boundary of the added material is shorter than the length of the boundary of the flexible, fibrous composite; and d) the fibers of the flexible, fibrous composite are oriented at 45° relative to the boundary of the flexible, fibrous composite. 15 . The self-transforming structure of claim 3 , wherein: a) the grain of the added material is orthogonal to an axis of a fiber of the flexible, fibrous composite; b) the grain of the added material is oriented at 45° relative to the boundary of the flexible, fibrous composite; c) the length of the boundary of the added material is the same as the length of the boundary of the flexible, fibrous composite; and d) the fibers of the flexible, fibrous composite are oriented at 45° relative to the boundary of the flexible, fibrous composite. 16 . The self-transforming structure of claim 3 , wherein: a) the grain of the added material is orthogonal relative to an axis of a fiber of the flexible, fibrous composite; b) the grain of the added material is orthogonal relative to the boundary of the flexible, fibrous composite; c) the length of the boundary of the added material is shorter than the length of the boundary of the flexible, fibrous composite; and d) the fibers of the flexible, fibrous composite are orthogonal relative to the boundary of the flexible, fibrous composite. 17 . The self-transforming structure of claim 3 , wherein: a) the grain of the added material is oriented at a 45° angle relative to an axis of a fiber of the flexible, fibrous composite; b) the grain of the added material is orthogonal relative to the boundary of the flexible, fibrous composite; c) the length of the boundary of the added material is the same length as the boundary of the flexible, fibrous composite; and d) the fibers of the flexible, fibrous composite are oriented at a 45° angle relative to the boundary of the flexible, fibrous composite. 18 . The self-transforming structure of claim 14 , further comprising a parallel grains of the added material on opposite sides of the flexible, fibrous composite. 19 . The self-transforming structure of claim 6 , wherein: a) the grain of the added material is orthogonal to an axis of a fiber of the flexible, fibrous composite; b) the grain of the added material is oriented at 45° relative to the boundary of the flexible, fibrous composite; c) the length of the boundary of the added material is the same as the length of the boundary of the flexible, fibrous composite; and d) the fibers of the flexible, fibrous composite are oriented at 45° relative to the boundary of the flexible, fibrous composite, and wherein the added material provides equal forces in two directions, thereby providing bi-stability. 20 . The self-transforming structure of claim 1 , wherein the weave pattern of the flexible, fibrous composite is triaxial. 21 - 41 . (canceled)
Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.] · CPC title
comprising polyamides · CPC title
including components having same physical characteristic in differing degree · CPC title
next to a fibrous or filamentary layer · CPC title
as the main or only constituent of a layer, {which is} next to another layer of {the same or of} a {different material (next to a layer of a particular substance B32B9/045; next to a bituminous or tarry layer B32B11/046; next to a water setting substance layer B32B13/12; next to a metal layer B32B15/08; next to a glass layer B32B17/10; next to a layer formed of natural mineral fibres or particles B32B19/045; next to a wood layer B32B21/08; next to a cellulosic plastic layer B32B23/08; next to a natural or synthetic rubber layer B32B25/08)} · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.