Methods for providing flammability protection for plastic optical fiber

US11243365B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11243365-B2
Application numberUS-201816193699-A
CountryUS
Kind codeB2
Filing dateNov 16, 2018
Priority dateNov 16, 2018
Publication dateFeb 8, 2022
Grant dateFeb 8, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

Methods for providing flammability protection for plastic optical fiber (POF) embedded inside avionics line replaceable units (LRUs) or other equipment used in airborne vehicles such as commercial or fighter aircrafts. A thin and flexible flammability protection tube is placed around the POF. In one proposed implementation, a very thin (100 to 250 microns in wall thickness) polyimide tube is placed outside and around the POF cable embedded inside an LRU or other equipment. The thin-walled polyimide tube does not diminish the flexibility of the POF cable.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for assembling a modular component, the method comprising: attaching an optical connector to a housing; installing a star coupler inside the housing; installing an optical-electrical media converter inside the housing; cutting a first specified length of tubing having an inner circular cylindrical surface and made of flame-resistant material to form a first protection tube; cutting a second specified length of tubing having an inner circular cylindrical surface and made of flame-resistant material to form a second protection tube; sliding the first protection tube onto a first plastic optical fiber cable comprising a single plastic optical fiber and a jacket that ensheathes the plastic optical fiber; sliding the second protection tube onto a second plastic optical fiber cable comprising a single plastic optical fiber and a jacket that ensheathes the plastic optical fiber; optically coupling the optical-electrical media converter to the star coupler by means of the first plastic optical fiber cable ensheathed by the first protection tube; and optically coupling the star coupler to the optical connector by means of the second plastic optical fiber cable ensheathed by the second protection tube. 2. The method as recited in claim 1 , wherein optically coupling the star coupler to the optical connector comprises crimping the optical connector onto the one end of the plastic optical fiber cable. 3. The method as recited in claim 1 , wherein optically coupling the star coupler to the optical connector comprises crimping the optical connector onto the second protection tube. 4. The method as recited in claim 1 , optically coupling the optical-electrical media converter to the star coupler comprises bonding one end of the first protection tube to the star coupler using epoxy or room temperature-vulcanizing adhesive. 5. The method as recited in claim 1 , further comprising: closing the housing of the modular unit after the optical-electrical media converter, star coupler, first and second plastic optical fiber cables, and optical connector have been placed inside; and installing the modular unit in an avionics system onboard an aircraft. 6. A modular component comprising: a housing; an optical connector attached to the housing; an optical-electrical media converter installed inside the housing, the optical-electrical media converter comprising a receptacle; a star coupler installed inside the housing; a first plastic optical fiber cable comprising a single plastic optical fiber and a jacket that ensheathes the plastic optical fiber and has an outer diameter, the first plastic optical fiber being connected to optically couple the star coupler to the optical-electrical media converter inside the housing; a second plastic optical fiber cable comprising a single plastic optical fiber and a jacket that ensheathes the plastic optical fiber and has an outer diameter, the second plastic optical fiber being connected to optically couple the star coupler to the optical connector; a first protection tube that ensheathes the jacket of the first plastic optical fiber cable and a second protection tube that ensheathes the jacket of the second plastic optical fiber cable, wherein each of the first and second protection tubes is made of a flame-resistant material, has an inner circular cylindrical surface with an inner diameter that is greater than the outer diameter of the jacket, and has one end that rests against the star coupler. 7. The modular component as recited in claim 6 , wherein the flame-resistant material is polyimide. 8. The modular component as recited in claim 6 , wherein each of the first and second protection tubes is flexible and has a wall thickness in a range of 100 to 250 microns. 9. The modular component as recited in claim 6 , wherein the optical connector is crimped to the second plastic optical fiber cable. 10. The modular component as recited in claim 6 , wherein the optical connector is crimped to the protection tube over the jacket and the one end of the protection tube is bonded to the star coupler. 11. A modular component comprising: a housing; first and second optical connectors attached to the housing; an optical-electrical media converter installed inside the housing; a transmit star coupler installed inside the housing and comprising a transmit optical mixer; a receive star coupler installed inside the housing and comprising a receive optical mixer; a first plastic optical fiber cable which is connected to optically couple the transmit optical mixer to the optical-electrical media converter; a second plastic optical fiber cable which is connected to optically couple the receive optical mixer to the optical-electrical media converter; a third plastic optical fiber cable which is connected to optically couple the transmit optical mixer to the first optical connector; a fourth plastic optical fiber cable which is connected to optically couple the receive optical mixer to the second optical connector, wherein each of the first through fourth plastic optical fiber cables is installed inside the housing and comprises a single plastic optical fiber and a jacket that ensheathes the plastic optical fiber and has an outer diameter; first through fourth protection tubes that respectively ensheathe the jacket of the first through fourth plastic optical fiber cables, wherein each of the first through fourth protection tubes is made of a flame-resistant material and has an inner circular cylindrical surface with an inner diameter that is greater than the outer diameter of the jacket. 12. The system recited in claim 11 , wherein each protection tube is flexible and has a wall thickness in a range of 100 to 250 microns. 13. The system recited in claim 11 , wherein the flame-resistant material is polyimide. 14. The system recited in claim 11 , wherein the first optical connector is crimped to one end of the third plastic optical fiber cable and one end of the third protection tube is bonded to the transmit optical mixer. 15. The system recited in claim 11 , wherein the first optical connector is crimped to the third protection tube over the jacket. 16. The system recited in claim 11 , further comprising a line replaceable unit that is electrically coupled to the optical-electrical media converter.

Assignees

Inventors

Classifications

  • Optical transmission, optical switches · CPC title

  • Star · CPC title

  • Devices including multiple stages, e.g., multi-stage optical amplifiers or dispersion compensators · CPC title

  • with one single optical waveguide (G02B6/4429, G02B6/4439, G02B6/4479 take precedence) · CPC title

  • Light guides · CPC title

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What does patent US11243365B2 cover?
Methods for providing flammability protection for plastic optical fiber (POF) embedded inside avionics line replaceable units (LRUs) or other equipment used in airborne vehicles such as commercial or fighter aircrafts. A thin and flexible flammability protection tube is placed around the POF. In one proposed implementation, a very thin (100 to 250 microns in wall thickness) polyimide tube is pl…
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification G02B6/02033. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Feb 08 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).