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Switchable window

  • US 10,197,882 B2
  • Filed: 07/10/2015
  • Issued: 02/05/2019
  • Est. Priority Date: 07/11/2014
  • Status: Active Grant
First Claim
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1. A switchable window for an aircraft, helicopter, or space vehicle, the switchable window comprising:

  • an outer pane construction subjected to sunlight; and

    an inner pane construction having an electrically switchable film for changing a color or transmittance of the switchable window, the outer pane construction covering at least an irradiated part of the inner pane construction, whereinthe outer pane construction absorbs IR radiation of the sunlight, and absorbs UV radiation of the sunlight,the outer pane construction comprises at least one transparent pane,the at least one transparent pane comprises;

    an IR absorber including nanoparticles of hexaboride, andan UV absorber including a chromophore,the outer pane construction and the inner pane construction are arranged with a spacing therebetween, andthe at least one transparent pane of the outer pane construction includes a polymethylmethacrylate (PMMA) pane having a transmission of visible light LT greater than 80% and a total solar energy transmission TSE lower than or equal to 55% resulting in a transmission ratio LT/TSE greater than or equal to 1.45.

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