# US 8,464,556 B2 · Microstructured optical fibers and methods

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- Number: US 8,464,556 B2
- Document ID: US8464556B2
- Status: Granted
- Kind: B2
- Application number: 12/151,170
- Filed: 2008-05-05
- Published: 2008-11-13
- Granted: 2013-06-18
- Earliest claimed: 2007-05-08
- Assignees: Corning Incorporated
- Applicants: Dana Craig Bookbinder; Robert Brett Desorcie; Mark Alan McDermott; Pushkar Tandon
- Inventors: Dana Craig Bookbinder; Robert Brett Desorcie; Mark Alan McDermott; Pushkar Tandon
- Web page: https://patentgrep.com/patent/US8464556B2

## CPC

- C03B 37/0142: {Reactant deposition burners}
- C03B 37/01446: {Thermal after-treatment of preforms, e.g. dehydrating, consolidating, sintering (C03B37/01853 takes precedence)}
- C03B 37/0146: {Furnaces therefor, e.g. muffle tubes, furnace linings}
- C03B 37/01466: {Means for changing or stabilising the diameter or form of tubes or rods (C03B37/01861 takes precedence)}
- C03B 37/02781: {Hollow fibres, e.g. holey fibres}
- C03B 2203/14: Non-solid, i.e. hollow products, e.g. hollow clad or with core-clad interface
- C03B 2203/42: Photonic crystal fibres, e.g. fibres using the photonic bandgap PBG effect, microstructured or holey optical fibres
- C03B 2205/44: Monotoring or regulating the preform feed rate
- C03B 2205/72: Controlling or measuring the draw furnace temperature
- C03B: MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES

## Abstract

Method of making a microstructured optical fiber. Silica glass based soot is deposited on a substrate to form at least a portion of an optical fiber preform by traversing a soot deposition burner with respect to said substrate at a burner traverse rate greater than 3 cm/sec, thereby depositing a layer of soot having a thickness less than 20 microns for each of a plurality of burner passes. At least a portion of the soot preform is then consolidated inside a furnace to remove greater than 50 percent of the air trapped in said soot preform, said consolidating taking place in a gaseous atmosphere containing krypton, nitrogen, or mixtures thereof under conditions which are effective to trap a portion of said gaseous atmosphere in said preform during said consolidation step, thereby forming a consolidated preform which when viewed in cross section will exhibit at least 50 voids therein.

## Claims

### Claim 1

A method of making an optical fiber comprising depositing silica glass based soot on a substrate to form at least a portion of an optical fiber preform by traversing a soot deposition burner with respect to said substrate at a burner traverse rate greater than 3 cm/sec, thereby depositing a layer of soot having a thickness less than 20 microns for each of a plurality of burner passes; and consolidating said at least a portion of the soot preform inside a furnace to remove greater than 50 percent of the air trapped in said soot preform, said consolidating taking place in a gaseous atmosphere containing krypton, argon, SO2, or mixtures thereof under conditions which are effective to trap a portion of said gaseous atmosphere in said preform during said consolidation step, thereby forming a consolidated preform which when viewed in cross section will exhibit at least 50 voids therein.

### Claim 2 (depends on 1)

The method of claim 1, wherein said preform when viewed in cross section will exhibit at least 10,000 voids therein.

### Claim 3 (depends on 1)

The method of claim 1, wherein said consolidating taking place in a gaseous atmosphere further comprising helium.

### Claim 4 (depends on 1)

The method of claim 1, wherein said consolidating taking place in a gaseous atmosphere which comprises krypton.

### Claim 5 (depends on 1)

The method of claim 1, wherein said soot deposited in said depositing step comprises a portion of the cladding region of the optical fiber preform.

### Claim 6 (depends on 1)

The method of claim 1, wherein said burner traverse rate in said depositing step is greater than 7 cm/sec.

### Claim 7 (depends on 6)

The method of claim 6, wherein said depositing step comprises depositing a layer of soot having a thickness less than 10 microns for each of a plurality of burner passes.

### Claim 8 (depends on 6)

The method of claim 6, wherein said depositing step comprises depositing a layer of soot having a thickness less than 15 microns for each of a plurality of burner passes.

### Claim 9 (depends on 1)

The method of claim 1, wherein said burner traverse rate in said depositing step is greater than 10 cm/sec.

### Claim 10 (depends on 1)

The method of claim 1, wherein said depositing step comprises depositing a layer of soot having a thickness less than 15 microns for each of a plurality of burner passes.

### Claim 11 (depends on 1)

The method of claim 1, further comprising, subsequent to said consolidation step and prior to a step of drawing the preform into an optical fiber, drawing the consolidated preform having voids therein into a cane to thereby reduce the diameter of the consolidated preform having voids therein to a outer preform diameter which is greater than 5 mm, under conditions which are effective to cause said voids to expand in diameter during the redraw step.

### Claim 12 (depends on 11)

The method of claim 11, wherein said drawing the preform into cane step comprises drawing said preform at a speed of greater than 5 cm per minute while exposing the preform to a temperature between about 1650-1775° C.

### Claim 13 (depends on 11)

The method of claim 11, wherein said drawing the preform into cane step comprises drawing said preform at a speed of greater than 7 cm per minute while exposing the preform to a temperature between about 1650-1775° C.

### Claim 14 (depends on 11)

The method of claim 11, further comprising drawing said fiber at a draw tension between 250 and 300 grams.

### Claim 15 (depends on 1)

The method of claim 1, further comprising drawing said fiber at a draw tension greater than 200 g.

### Claim 16 (depends on 1)

The method of claim 1, further comprising drawing said fiber at a draw tension between 250 and 300 grams.
