METAL-BASED PLUGS FOR ELECTROCHROMIC DEVICES

• US 20160077398A1
• Filed: 08/25/2015
• Published: 03/17/2016
• Est. Priority Date: 09/15/2014
• Status: Abandoned Application

• Current Assignee: Gentex Corporation
• Original Assignee: Gentex Corporation
• Inventors: Ash, Kevin L., Green, Kristopher R., Stephenson, Michael T.
• Application Number:
  US14/834,849
• Publication Number:
  US 20160077398A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G02F 1/161 Gaskets; Spacers; Sealing of cells; Filling or closing of cells

Abstract

An electrochromic device includes a first substrate having an electrically conductive material associated therewith, a second substrate having an electrically conductive material associated therewith, a chamber positioned in a center of the electrochromic device, an electrochromic medium contained within the chamber, at least one fill port extending between at least one of the first substrate and the second substrate and the chamber, at least one plug associated with the at least one fill port, and a metal sealing member disposed on a surface of the at least one of the first substrate and the second substrate. The metal sealing member configured to hermetically seal the at least one fill port.

Claims

1. An electrochromic device, comprising:

at least one fill port;

a primary plug material associated with the at least one fill port; and

a metal-based sealing member over-covering the primary plug material.

2. The electrochromic device of claim 1, wherein the metal-based sealing member comprises tin, a tin alloy, a tin solder, silver, a silver alloy, a silver solder, zinc, a zinc alloy, a zinc solder, antimony, an antimony alloy, an antimony solder, silver, a silver alloy, a silver solder, aluminum, an aluminum alloy, an aluminum solder, germanium, a germanium alloy, a germanium solder, titanium, a titanium alloy, a titanium solder, gold, a gold alloy, a gold solder, platinum, a platinum alloy, a platinum solder, copper, a copper alloy, a copper solder, palladium, a palladium alloy or a palladium solder.

3. The electrochromic device of claim 1, wherein the metal-based sealing member comprises tin.

4. The electrochromic device of claim 1, wherein the metal-based sealing member comprises tin, zinc, and silver.

5. The electrochromic device of claim 1, wherein the metal-based sealing member comprises 94.5±

1.0 wt % tin, 4.0±

1.0 wt % zinc, 1.0±

0.3 wt % antimony, 0.1±

0.2 wt % silver, 0.01±

0.003 wt % aluminum, 0.01±

0.003 wt % germanium, 0.005±

0.002 wt % silicon, and 0.005±

0.002 wt % titanium.

6. The electrochromic device of claim 1, wherein the metal-based sealing member comprises 90-100 wt % tin, 5 wt % antimony and 1-5 wt % zinc.

7. The electrochromic device of claim 1, wherein the metal-based sealing member comprises 94-96 wt % tin, 3-5 wt % antimony and 1-3 wt % zinc.

8. The electrochromic device of claim 1, wherein the metal-based sealing member comprises an indium and tin alloy.

9. The electrochromic device of claim 1, further comprising a second fill port, a second primary plug material associated with the second fill port;

and a second metal-based sealing member over-covering the second primary plug material.

10. The electrochromic device of claim 1, wherein the device is an electrochromic window.

11. The electrochromic device of claim 1, wherein the device is an electrochromic aircraft transparency.

12. The electrochromic device of claim 1, wherein the device is an electrochromic mirror.

13. An electrochromic aircraft transparency, comprising:

a first substrate having an electrically conductive material associated therewith;

a second substrate having an electrically conductive material associated therewith;

a chamber positioned in a center of the electrochromic device, the chamber defined by the first substrate, the second substrate and two edge seals provided between the first substrate and the second substrates;

an electrochromic medium contained within the chamber;

at least one fill port extending between at least one of the first substrate and the second substrate and the chamber;

at least one plug associated with the at least one fill port; and

a metal sealing member disposed on a surface of the at least one of the first substrate and the second substrate, the metal sealing member configured to hermetically seal the at least one fill port.

14. The electrochromic aircraft transparency of claim 13, wherein the metal sealing member comprises tin, a tin alloy, a tin solder, silver, a silver alloy, a silver solder, zinc, a zinc alloy, a zinc solder, antimony, an antimony alloy, an antimony solder, silver, a silver alloy, a silver solder, aluminum, an aluminum alloy, an aluminum solder, germanium, a germanium alloy, a germanium solder, titanium, a titanium alloy, a titanium solder, gold, a gold alloy, a gold solder, platinum, a platinum alloy, a platinum solder, copper, a copper alloy, a copper solder, palladium, a palladium alloy or a palladium solder.

15. The electrochromic aircraft transparency of claim 13, wherein the metal sealing member comprises tin.

16. The electrochromic aircraft transparency of claim 13, wherein the metal sealing member comprises 94.5±

1.0 wt % tin, 4.0±

1.0 wt % zinc, 1.0±

0.3 wt % antimony, 0.1±

0.2 wt % silver, 0.01±

0.003 wt % aluminum, 0.01±

0.003 wt % germanium, 0.005±

0.002 wt % silicon, and 0.005±

0.002 wt % titanium.

17. The electrochromic aircraft transparency of claim 13, wherein the metal sealing member comprises an indium and tin alloy.

18. The electrochromic aircraft transparency of claim 13, wherein the metal sealing member comprises 90-100 wt % tin, 5 wt % antimony and 1-5 wt % zinc.

19. The electrochromic aircraft transparency of claim 13, wherein the metal sealing member comprises 94-96 wt % tin, 3-5 wt % antimony and 1-3 wt % zinc.