Hot forming of curved mirrors without the need for a mandrel
US-2024018030-A1 · Jan 18, 2024 · US
US9950944B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9950944-B2 |
| Application number | US-201414463784-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 20, 2014 |
| Priority date | May 9, 2012 |
| Publication date | Apr 24, 2018 |
| Grant date | Apr 24, 2018 |
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A curved bullet-proof composite comprising: a glass or glass-ceramic external strike-face layer having been subjected to an ion exchange process and which is mechanically curved; at least one glass or glass-ceramic intermediate layer; an internal plastic layer; and an adhesive material between the strike-face layer, the at least one intermediate layer and the internal plastic layer.
Opening claim text (preview).
The invention claimed is: 1. A process for bending a bullet-proof composite comprised of one alkali aluminosilicate or soda-lime silicate glass strike-face layer which has been subjected to an ion exchange process to obtain enough flexibility to be mechanically curved, and having a thickness less or equal to 3mm, one or more glass or glass-ceramic intermediate layers, one internal plastic layer and an adhesive material between each of the above layers, comprising the steps of: (a) individually bending by means of gravity and temperature the glass or glass-ceramic intermediate layers; and (b) mechanically bending the glass strike-face layer and the internal plastic layer by laminating by heat and pressure the glass strike-face layer, the glass or glass-ceramic intermediate layers from step (a), the adhesive materials and the internal plastic layer; wherein the softening point temperature of the glass-strike face layer is higher than the softening point temperature of the glass or glass-ceramic intermediate layers of the bullet-proof composite; wherein the lamination temperature from step (b) is less than the bending temperature from step (a); and wherein the glass strike-face layer corresponds to the convex side of the bullet-proof composite. 2. The process of claim 1 , wherein the glass or glass-ceramic intermediate layers have been subjected to an ion exchange process. 3. The process of claim 1 , wherein a step (c) is carried out after step (a), and consists of painting around the glass strike-face layer with black organic or inorganic paint. 4. The process of claim 3 , wherein the painting with black organic paint or inorganic is done over the glass or glass-ceramic intermediate layers. 5. The process of claim 1 , wherein the step (b) of heat and pressure mechanically bending is performed at a pressure ranging from 0.68 to 1.03 MPa. 6. The process of claim 1 , wherein the step (b) of heat and pressure mechanically bending step is performed at a temperature ranging from 85° C. to 135° C.
with permanent bending or reshaping or surface deformation of self sustaining lamina · CPC title
Gravity bending involving applying local or additional heating, cooling or insulating means · CPC title
Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension · CPC title
of adhesive layers · CPC title
Gravity bending accelerated by applying mechanical forces, e.g. inertia, weights or local forces · CPC title
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