Band-gap tunable elastic optical multilayer fibers
US-2015362669-A1 · Dec 17, 2015 · US
US9846276B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9846276-B2 |
| Application number | US-201615098891-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 14, 2016 |
| Priority date | Apr 14, 2015 |
| Publication date | Dec 19, 2017 |
| Grant date | Dec 19, 2017 |
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A fiber grating device of low cost and arbitrary length is formed on a portion of a portion or the entirety of a highly elastic fiber optic core having a low Young's modulus of elasticity by causing elongation of the fiber optic core and forming or depositing a hard skin or cladding on the elongated fiber optic core. When the stress is then released, the hard skin or cladding buckles (including elastic or plastic deformation or both) to form wrinkles at the interface of the fiber optic core and the hard skin or cladding which are oriented circumferentially and highly uniform in height and spacing which can be varied at will by choice of materials, stretching, and thickness and composition of the cladding. Since the elastic elongation of the fiber optic core portion may be 200% or greater, an unprecedented measurement range is provided.
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Having thus described our invention, what we claim as new and desire to secure by Letters Patent is as follows: 1. A method of forming a fiber optic device, said method comprising the steps of: applying an axial force to at least a portion of an elastically deformable fiber optic core of an optical fiber to produce an elongation, forming or applying a hard shell or overlayer on said at least a portion of an elastically deformable fiber optic core of an optical fiber, said elastically deformable fiber optic core having a low modulus of elasticity and capable of withstanding a strain elongation of 200% or more; said hard shell or overlayer having a modulus of elasticity at least twice the modulus of elasticity of the core and having finite axial buckling force threshold within the level of stress to achieve 200% elongation of the core; and permitting contraction of the elastically deformable fiber optic core to form wrinkles at an interface of said fiber optic core and said hard shell or cladding, wherein the wrinkles are configured to function as a grating; wherein the elastically deformable fiber optic core and the hard shell or overlayer encasing said elastically deformable fiber optic core are configured to elongate when subjected to a longitudinal stress; and wherein spectral effects and interference patterns change with height and periodicity of the undulations or wrinkles, longitudinal stress causing elongation of the elastically deformable fiber optic core cause the undulations or wrinkles to be diminished in height and increased in separation, thus changing both the degree of scattering and effects on the spectrum of the light transmitted through the fiber optic core. 2. The method as recited in claim 1 , including the further step of irradiating said elastically deformable fiber optic core using ultraviolet light or a plasma to form said hard shell or overlayer from material of said elastically deformable fiber optic core. 3. An optical device, comprising: an elastically deformable fiber optic core; a hard shell or overlayer encasing said elastically deformable fiber optic core, said hard shell or overlayer having a thickness approaching one half or less of an unstressed diameter of the core, the hard shell or overlayer having undulations or wrinkles substantially uniform in both height and period along at least a portion of the fiber optic core length, the undulations or wrinkles forming a Brag diffraction grating; said elastically deformable fiber optic core having a low modulus of elasticity and capable of withstanding a strain elongation of 200% or more; said hard shell or overlayer having a modulus of elasticity at least twice the modulus of elasticity of the core and having finite axial buckling force threshold within the level of stress to achieve 200% elongation of the core; wherein the elastically deformable fiber optic core and the hard shell or overlayer encasing said elastically deformable fiber optic core are configured to elongate when subjected to a longitudinal stress; and wherein spectral effects and interference patterns change with height and periodicity of the undulations or wrinkles, longitudinal stress causing elongation of the elastically deformable fiber optic core cause the undulations or wrinkles to be diminished in height and increased in separation, thus changing both the degree of scattering and effects on the spectrum of the light transmitted through the fiber optic core. 4. The fiber optic device as recited in claim 3 , wherein the wrinkles of said hard skin or cladding are configured to function as a Bragg grating which varies with elongation of the elastically deformable fiber optic core and the hard shell or overlayer encasing when subjected to a longitudinal stress. 5. The optical device of claim 3 , further comprising: a light source configured for transmitting light through said elastically deformable fiber optic core; and an optical detector configured to receive light transmitted through said elastically deformable fiber optic core, wherein a distance traversed by light from the light source to the optical detector varies with elongation of the the elastically deformable fiber optic core and the hard shell or overlayer encasing said elastically deformable fiber optic core elongate when subjected to a longitudinal stress. 6. The optical device of claim 5 , wherein said optical detector is configured at one end of the elastically deformable fiber optic core to receive light which passes through the elastically deformable fiber optic core from said light source configured at an opposite end of said elastically deformable fiber optic core. 7. The optical device of claim 5 , wherein said optical detector is configured to receive light which passes through the elastically deformable fiber optic core from said light source and which light is reflected back through said elastically deformable fiber optic core.
Mechanically induced gratings, e.g. having microbends (G02B6/02066 takes precedence; mode converters G02B6/14) · CPC title
Manufacturing methods · CPC title
based on illuminating or irradiating an amplitude mask, i.e. a mask having a repetitive intensity modulating pattern · CPC title
using photoelastic elements · CPC title
Gratings having a surface relief structure, e.g. repetitive variation in diameter of core or cladding · CPC title
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