High temperature transponders

• US 10,424,837 B2
• Filed: 05/05/2017
• Issued: 09/24/2019
• Est. Priority Date: 09/14/2012
• Status: Active Grant

• Current Assignee: Veriteq Acquisition Corporation (VeriTeQ Corp.)
• Original Assignee: JAMM Technologies, Inc. (Establishment Labs Holdings, Inc.)
• Inventors: Mejia, Ezequiel
• Primary Examiner(s): Levi, Dameon E
• Assistant Examiner(s): Lotter, David E
• Application Number:
  US15/587,828
• Publication Number:
  US 20170256850A1
• Time in Patent Office: 872 Days
• CPC Class Codes: G06K 7/10336 the antenna being of the near field type, inductive coil
• CPC Class Codes: H01Q 1/002 Protection against seismic waves, thermal radiation or other disturbances, e.g. nuclear explosion; Arrangements for improving the power handling capability of an antenna
• CPC Class Codes: H01Q 1/22 by structural association with other equipment or articles
• CPC Class Codes: H01Q 1/40 Radiating elements coated with or embedded in protective material
• CPC Class Codes: H01Q 7/06 with core of ferromagnetic material H01Q7/02 takes precedence

Abstract

The present invention provides, in alternative embodiments, high temperature transponders that can withstand high temperature shocks and can maintain their physical and electrical characteristics following high temperature exposure, and methods of making said transponders.

Claims

1. A transponder, comprising:

an antenna assembly, comprising;

a core having a length ranging from 5 mm to 20 mm;

an insulated wire disposed around the core in a coil, the insulated wire having a first end and a second end; and

an integrated circuit chip, wherein the first end and the second end of the insulated wire are each connected to the integrated circuit chip;

a capsule enclosing the antenna assembly and defining a space between the capsule and the antenna assembly; and

a high temperature adhesive disposed within the space and covering at least 50% of the insulated wire, wherein the adhesive is cured and fixes a position of the antenna assembly relative to the capsule.

2. The transponder of claim 1, wherein the antenna assembly and the high temperature adhesive of the transponder are together configured to withstand temperatures ranging from 165°

C. to 195°

C. without losing functionality of the transponder.

3. The transponder of claim 2, wherein the transponder has a working frequency of 134 kHz.

4. The transponder of claim 1, wherein the insulated wire comprises copper and is wound uniformly around the core from 800 to 1000 times.

5. The transponder of claim 1, wherein the chip includes two metal inlay portions embedded within the chip, and wherein the first end and the second end of the insulated wire are each connected to a respective one of the two metal inlay portions by at least one of thermal compression, laser welding, crimp connection, soldering, or a connection adhesive.

6. The transponder of claim 5, wherein the metal inlay portions comprise gold.

7. The transponder of claim 1, wherein the chip comprises a complementary metal-oxide-semiconductor (CMOS) integrated circuit storing an identification code.

8. The transponder of claim 1, wherein the transponder is configured for inclusion in a medical implant and to withstand temperatures ranging from 150°

C. to 210°

C. during manufacture of the implant.

9. The transponder of claim 1, wherein the high temperature adhesive covers at least 75% of the insulated wire.

10. The transponder of claim 1, wherein at least a portion of the core has a width ranging from 0.5 mm to 5 mm.

11. The transponder of claim 1, wherein a diameter of the insulated wire ranges from 0.10 mm to 0.50 mm, and wherein the core comprises ferrite.

12. A transponder, comprising:

an antenna assembly, including;

a core;

an insulated wire coiled around the core, the insulated wire having a first end and a second end; and

an integrated circuit chip electrically coupled to the first end and the second end of the insulated wire;

a capsule enclosing the antenna assembly and defining a space between the capsule and the antenna assembly; and

a high temperature adhesive completely covering the insulated wire and filling the space between the capsule and the antenna assembly.

13. The transponder of claim 12, wherein the core has a length ranging from 5 mm to 20 mm and a width ranging from 0.5 mm to 5 mm.

14. The transponder of claim 12, wherein the high temperature adhesive comprises a glue or epoxy material configured to withstand temperatures ranging from 180°

C. to 270°

C. without evaporating or expanding.

15. The transponder of claim 12, wherein the transponder is configured for shock resistance, and the high temperature adhesive does not become brittle after heating and cooling.

16. The transponder of claim 12, wherein the high temperature adhesive is a light-curing acrylate adhesive.

17. A transponder comprising:

an antenna assembly including;

a core having a width ranging from 0.5 mm to 5 mm;

an insulated wire wound around the core, the wire having a first end and a second end; and

an integrated circuit chip comprising two portions of a metal or metal alloy embedded into a surface of the integrated circuit chip, wherein the first and second ends of the wire are each connected to one of the two portions; and

an adhesive covering at least 75% of the insulated antenna wire, wherein the adhesive withstands temperatures ranging from 180°

C. to 270°

C. without evaporating or expanding.

18. The transponder of claim 17, further comprising a capsule enclosing the antenna assembly and defining a space adjacent to the antenna assembly, and wherein the adhesive fills at least 75% of the space adjacent to the antenna assembly.

19. The transponder of claim 18, wherein the transponder is configured to withstand 4 to 8 hour cycles of temperatures between 165 and 195°

C. (±

15°

C.).

20. The transponder of claim 17, wherein a length of the core runs perpendicular to the width and ranges from 5.0 mm to 20 mm.