Process for extending operating temperature range of gigabit plastic optical fiber

Patent metadata

Field	Value
Publication number	US-10998976-B2
Application number	US-201916551282-A
Country	US
Kind code	B2
Filing date	Aug 26, 2019
Priority date	Aug 26, 2019
Publication date	May 4, 2021
Grant date	May 4, 2021

Abstract

A process to enhance the performance of plastic optical fiber to operate with a high data rate (e.g., at least 1 gigabit per second) at high temperature (e.g., 100 degrees Celsius) for airplane avionic systems. Gigabit plastic optical fiber has a core including a dopant that enables data transmission at gigabit rates. The enhancement process uses rapid thermal cooling of the gigabit plastic optical fiber to stabilize the polymer matrix of the fiber. This rapid cooling treatment blocks dopant diffusion in a high-temperature environment, thereby avoiding degradation of the fiber's bandwidth and optical loss characteristic. Such degradation typically occurs in gigabit plastic optical fiber having core and cladding made of transparent carbon-hydrogen bond-free perfluorinated polymer.

First claim

The invention claimed is:

1. A process for extending the operating temperature range of plastic optical fiber, the method comprising:
(a) placing a loop of plastic optical fiber inside a thermal chamber, which plastic optical fiber has a core with dopant distributed in a polymer matrix such that the plastic optical fiber has a high-data-rate capability at a first temperature but not at a second temperature which is higher than the first temperature;
(b) decreasing a temperature inside the thermal chamber until a third temperature lower than the first temperature is reached;
(c) maintaining the third temperature inside the thermal chamber for a first period of time sufficient to cause the plastic optical fiber to develop the high-data-rate capability at the second temperature;
(d) increasing the temperature inside the thermal chamber until a fourth temperature lower than the first temperature and higher than the third temperature is reached;
(e) maintaining the fourth temperature inside the thermal chamber during a second period of time subsequent to the first period of time; and
(f) removing the loop of plastic optical fiber from the thermal chamber,
wherein the third temperature is in a range of −55 to −65 degrees Celsius.

2. The process as recited in claim 1 , wherein the fourth temperature is room temperature.

3. The process as recited in claim 1 , wherein the second temperature is 100 degrees Celsius.

4. The process as recited in claim 1 , wherein the plastic optical fiber is graded-index plastic optical fiber having a core and a cladding made of a transparent carbon-hydrogen bond-free perfluorinated polymer.

5. The process as recited in claim 1 , wherein following completion of steps (a) through (f), the plastic optical fiber has a data rate capability up to 10 gigabits per second at 100 degrees Celsius.

6. The process as recited in claim 5 , further comprising installing the plastic optical fiber in an avionics network system onboard an aircraft after step (f).

7. A process for extending the operating temperature range of plastic optical fiber, the method comprising:
(a) placing a portion of a length of plastic optical fiber inside a thermal chamber and opposing ends of the plastic optical fiber outside the thermal chamber, wherein the plastic optical has a core with dopant distributed in a polymer matrix such that the plastic optical fiber has a high-data-rate capability at a first temperature but not at a second temperature which is higher than the first temperature;
(b) decreasing a temperature inside the thermal chamber until a third temperature lower than the first temperature is reached;
(c) maintaining the third temperature inside the thermal chamber for a first period of time sufficient to cause the plastic optical fiber to develop the high-data-rate capability at the second temperature;
(d) increasing the temperature inside the thermal chamber until a fourth temperature lower than the first temperature and higher than the third temperature is reached;
(e) maintaining the fourth temperature inside the thermal chamber during a second period of time subsequent to the first period of time; and
(f) removing the plastic optical fiber from the thermal chamber,
wherein the third temperature is in a range of −55 to −65 degrees Celsius.

8. The process as recited in claim 7 , further comprising:
(g) optically coupling an optical transceiver to the opposing ends of the plastic optical fiber; and
(h) electrically coupling a bit-error-rate tester to the optical transceiver,
wherein steps (g) and (h) are performed after step (a) and before step (b).

9. The process as recited in claim 8 , further comprising:
(i) testing the bit error rate of the plastic optical fiber at the high data rate.

10. The process as recited in claim 9 , wherein step (i) is performed after step (h) and before step (b).

11. The process as recited in claim 9 , wherein step (i) is performed after step (e) and before step (f).

12. The process as recited in claim 7 , wherein the second temperature is 100 degrees Celsius.

13. The process as recited in claim 7 , wherein the plastic optical fiber is graded-index plastic optical fiber having a core and a cladding made of a transparent carbon-hydrogen bond-free perfluorinated polymer.

14. The process as recited in claim 7 , wherein following completion of steps (a) through (f), the plastic optical fiber has a data rate capability up to 10 gigabits per second at 100 degrees Celsius.

15. The process as recited in claim 14 , further comprising installing the plastic optical fiber in an avionics network system onboard an aircraft after step (f).

16. A method for transmitting data comprising:
(a) placing a plastic optical fiber inside a thermal chamber, which plastic optical fiber has a core with dopant distributed in a polymer matrix such that the plastic optical fiber has a high-data-rate capability at a first temperature but not at a second temperature which is higher than the first temperature;
(b) decreasing a temperature inside the thermal chamber until a third temperature lower than the first temperature is reached;
(c) maintaining the third temperature inside the thermal chamber for a first period of time sufficient to cause the plastic optical fiber to develop the high-data-rate capability at the second temperature;
(d) increasing the temperature inside the thermal chamber until a fourth temperature lower than the first temperature and higher than the third temperature is reached;
(e) maintaining the fourth temperature inside the thermal chamber during a second period of time subsequent to the first period of time; and
(f) removing the plastic optical fiber from the thermal chamber;
(g) optically coupling a first transceiver to a first end of the plastic optical fiber;
(h) electrically coupling a first electrical device to the first transceiver;
(i) optically coupling a second transceiver to a second end of the plastic optical fiber;
(j) electrically coupling a second electrical device to the second transceiver;
(k) sending electrical signals representing data from the first electrical device to the first transceiver;
(l) transmitting laser light from the first transceiver into the plastic optical filter, which laser light represents the data from the first electrical device;
(m) photodetecting the laser light at the second transceiver into electrical signals representing the data from the first electrical device; and
(n) receiving the electrical signals representing the data from the first electrical device at the second electrical device,
wherein the third temperature is in a range that includes an upper limit of −55 degrees Celsius.

17. The method as recited in claim 16 , wherein the plastic optical fiber is graded-index plastic optical fiber having a core and a cladding made of a transparent carbon-hydrogen bond-free perfluorinated polymer.

18. The method as recited in claim 16 , wherein the first and second electrical devices are line replaceable units of an avionics network system onboard an airplane.

19. The method as recited in claim 16 , wherein the second temperature is 100 degrees Celsius.

20. The method as recited in claim 16 , wherein following completion of steps (a) through (f), the plastic optical fiber has a data rate capability up to 10 gigabits per second at 100 degrees Celsius.

Assignees

• Boeing Co

Inventors

• Chan Eric Y
• Koshinz Dennis G
• Nguyen Kim Quan Anh

Classifications

• G02B6/02038 Primary

  with core or cladding having graded refractive index · CPC title

• B29D11/00711

  by shrinking the sleeve or cladding onto the core · CPC title

• B29C71/02

  Thermal after-treatment {(B29C71/0063 and B29C71/0072 take precedence)} · CPC title

• G02B1/046

  characterised by the core material · CPC title

• B29D11/00663

  Production of light guides · CPC title