CA2385604A1 - Method and apparatus for manufacturing optical fiber components - Google Patents
Method and apparatus for manufacturing optical fiber components Download PDFInfo
- Publication number
- CA2385604A1 CA2385604A1 CA002385604A CA2385604A CA2385604A1 CA 2385604 A1 CA2385604 A1 CA 2385604A1 CA 002385604 A CA002385604 A CA 002385604A CA 2385604 A CA2385604 A CA 2385604A CA 2385604 A1 CA2385604 A1 CA 2385604A1
- Authority
- CA
- Canada
- Prior art keywords
- fiber
- substrate
- center wavelength
- grating
- cwl
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/02—Optical fibres with cladding with or without a coating
- G02B6/02057—Optical fibres with cladding with or without a coating comprising gratings
- G02B6/02076—Refractive index modulation gratings, e.g. Bragg gratings
- G02B6/02123—Refractive index modulation gratings, e.g. Bragg gratings characterised by the method of manufacture of the grating
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/02—Optical fibres with cladding with or without a coating
- G02B6/02057—Optical fibres with cladding with or without a coating comprising gratings
- G02B6/02076—Refractive index modulation gratings, e.g. Bragg gratings
- G02B6/02171—Refractive index modulation gratings, e.g. Bragg gratings characterised by means for compensating environmentally induced changes
- G02B6/02176—Refractive index modulation gratings, e.g. Bragg gratings characterised by means for compensating environmentally induced changes due to temperature fluctuations
- G02B6/0218—Refractive index modulation gratings, e.g. Bragg gratings characterised by means for compensating environmentally induced changes due to temperature fluctuations using mounting means, e.g. by using a combination of materials having different thermal expansion coefficients
Abstract
A method and apparatus for manufacturing fiber-optic devices to precise CWL
specifications by plasticizing one attachment end (18) of a mounted fiber-optic device and finely adjusting the fiber tension while monitoring the CWL.
In one embodiment, the method of manufacturing an optical fiber component to a precise CWL includes the step of affixing the ends (18, 20) of a fiber component (12) under tension to a substrate (16) to approximate a desired CWL.
Subsequently, one end of the fiber (21) is gripped with a movable clamp (36) and the adjacent attachment (20) plasticized while the tension on the fiber is adjusted until the CWL is within a desired range. The attachment (20) is rehardened while the tension on the fiber is maintained by the movable clamp (36).
specifications by plasticizing one attachment end (18) of a mounted fiber-optic device and finely adjusting the fiber tension while monitoring the CWL.
In one embodiment, the method of manufacturing an optical fiber component to a precise CWL includes the step of affixing the ends (18, 20) of a fiber component (12) under tension to a substrate (16) to approximate a desired CWL.
Subsequently, one end of the fiber (21) is gripped with a movable clamp (36) and the adjacent attachment (20) plasticized while the tension on the fiber is adjusted until the CWL is within a desired range. The attachment (20) is rehardened while the tension on the fiber is maintained by the movable clamp (36).
Description
METHOD AND APPARATUS FOR
MANUFACTURING OPTICAL FIBER COMPONENTS
BACKGROUND OF INVENTION
S
1. Field of the Invention The present invention relates to relates generally to the manufacturing of optical fiber components and particularly to a method and apparatus for precisely controlling the optical path length of an optical fiber component.
MANUFACTURING OPTICAL FIBER COMPONENTS
BACKGROUND OF INVENTION
S
1. Field of the Invention The present invention relates to relates generally to the manufacturing of optical fiber components and particularly to a method and apparatus for precisely controlling the optical path length of an optical fiber component.
2. Technical Background Optical fiber based devices are widely utilized as components for optical communications due to their relatively low insertion loss and low cost.
Foremost of optical fiber components are fiber Bragg gratings (FBG) which are typically made by ultraviolet (UV) wavelength energy exposure. Once an FBG is mounted to a substrate and annealed, it is no longer photosensitive and cannot be further tuned.
Thus, it is necessary to empirically predict the final frequency of such a grating which can lead to a significant error resulting in gratings which are not within specifications.
Due to the uncertainty of the wavelength shift resulting from the attachment process and annealing, the center wavelength (CWL) of a packaged fiber Bragg grating can vary as much as +/- 60 picometers from the desired CWL. Such a wavelength error combined with a wavelength drift of, for example, distributed feedback lasers, which may be from +/- 50 picometers, and the residual temperature dependence of +/-picometers imposes a highly stringent requirement on the design of, for example, 50 GHz fiber Bragg gratings.
A typical attachment process for a fiber Bragg grating is to bond one end of the fiber to a substrate, tension the fiber by an empirically determined amount, and bonding the opposite end of the fiber. Fig. 1 shows the distribution of the CWL for samples manufactured by this process. Since the total available margin is only +/-40 picometers, only a fraction (20 % to 30 % ) of the gratings can be employed.
Precise control of optically tuned fiber-optic devices with a CWL within less than +/- 15 picometers is desired to minimize cross-talk between adjacent communication channels of a system. In order to maintain the CWL of a tuned fiber-optic device, such as a fiber Bragg grating, a 13-eucryptite substrate has been employed having a coefficient of temperature expansion of - 7.5 ppm/°C
to compensate for the refractive index change of the fiber with temperature variations.
With such substrates, the CWL shift due to temperature changes over a range of from 0°C to 70°C has been reduced to +/- 15 pm. Thus, although the substrate selection has improved the stability of the device once manufactured, there remains a need to manufacture devices such as fiber Bragg gratings or other optically tuned components to a CWL that produces a yield rate for precise CWL devices higher than that previously available with existing manufacturing techniques.
It has been discovered that the variability of the CWL of fiber-optic devices is not a function of the laser power employed in the manufacturing of the devices nor is it a result of the substrate material. Instead, it appears that the variability is inherent in the attachment process and there remains a need, therefore, for a process and system for manufacturing precisely tuned fiber-optic devices.
SUMMARY OF THE INVENTION
The method and apparatus of the present invention achieves the manufacturing of fiber-optic devices to precise CWL specifications by plasticizing one attachment end of a mounted fiber-optic device and finely adjusting the fiber tension while monitoring the CWL.
A method of manufacturing an optical fiber component to a precise CWL
includes the step of affixing the ends of a fiber component under tension to a substrate to approximate a desired CWL. Subsequently, one end of the fiber is gripped with a movable clamp and the adjacent attachment plasticized while the tension on the fiber is adjusted until the CWL is within a desired range. The attachment is rehardened while the tension on the fiber is maintained by the movable clamp.
In one embodiment, one end of a fiber is bonded to a negative coefficient of expansion substrate using a glass frit and the opposite end gripped under tension by a movable clamp while the CWL is monitored. The fiber tension is adjusted by moving the clamp until the CWL is about .35 nm below the target CWL for 70 mm substrates. Next, a second frit bonds the fiber to the substrate at an opposite end adjacent the movable clamp. The CWL is again checked and, if off more than 10 picometers, the fiber is retensioned by moving the clamp to the previous position, repeating and plasticizing the second frit, and adjusting the clamp while monitoring the CWL until the CWL change equals an amount corresponding to the difference between the first measured CWL and the target CWL. Once cooled, the clamp is released and the final CWL is measured and recorded.
The result of this process produces precisely tuned fiber-optic devices, such as a fiber Bragg grating. Although particularly suitable for manufacturing fiber Bragg gratings, other tunable fiber-optic components likewise can be manufactured using such technique, to precisely control the optical path length of the optical fiber device during manufacturing.
Additional features and advantages of the invention will be set forth in the detailed description which follows and will be apparent to those skilled in the art from the description or recognized by practicing the invention as described in the description which follows together with the claims and appended drawings.
It is to be understood that the foregoing description is exemplary of the invention only and is intended to provide an overview for the understanding of the nature and character of the invention as it is defined by the claims. The accompanying drawings are included to provide a further understanding of the invention and are incorporated and constitute part of this specification. The drawings illustrate various features and embodiments of the invention which, together with their description serve to explain the principals and operation of the invention.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a chart illustrating the variations in CWL of fiber Bragg gratings manufactured by conventional techniques;
Fig. 2 is an enlarged schematic, side-elevational view of a fiber Bragg grating, shown partially packaged and manufactured according to the present invention;
Fig. 3 is a schematic, side-elevational view of a fiber Bragg grating and an apparatus for manufacturing the same according to the present invention during a first step in the manufacturing process;
Fig. 4 is a schematic, side-elevational view of the next step in the manufacturing process of the fiber Bragg grating shown in Fig. 2;
Fig. 5 is a schematic, side-elevational view of a successive step in the manufacturing process of the fiber Bragg grating shown in Fig. 2; and Fig. 6 is a chart illustrating the high yield of precise CWL fiber Bragg gratings resulting from the manufacturing process of the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
The chart of Fig. 1 illustrates the CWL shift between predicted CWL and actual CWL for 40 samples made using existing techniques which, as seen, vary between approximately 70 nm below the desired CWL (shown by the dotted line in the chart) to about 75 nm above the desired CWL. The number of samples falling within +/- 40 picometers of the desired CWL is relatively small, representing from 20 % to 30 % of the total number of fiber Bragg gratings made by the conventional empirical process.
In order to improve the yield rate to that shown in Fig. 6, the fiber Bragg grating illustrated in Fig. 2 is manufactured according to the process and apparatus described in connection with Figs. 3-5. As seen in Fig. 6, a sample of approximately 70 fiber Bragg gratings manufactured according to the present invention yields 80 %o of gratings falling within +/- 10 picometers of the desired CWL. This tolerance band of precisely manufactured gratings is shown between the dotted lines in Fig. 6.
Even gratings falling outside the precisely controlled band for the most part fell well within an acceptable range of +/- 40 picometers for most applications. Thus, while only very few conventionally manufactured fiber Bragg gratings fall within a +/- 10 picometers criteria, more than 80 % of the gratings manufactured according to the process of the present invention fell within such tolerance range. The dramatic results achieved by the process and apparatus of the present invention and the resulting fiber-optic component is now described in the context of a fiber Bragg grating with reference to Figs. 2-5.
A partially packaged fiber Bragg grating assembly 10 is shown in Fig. 2 and includes an optical fiber 12 in which there is imprinted a grating 14 in a central area with a precisely controlled CWL of, for example, 1559.25 nm. The optical fiber is supported on a negative coefficient of expansion substrate 16, such as 13-eucryptite, by a pair of spaced glass frits 18 and 20. between the glass frits 18 and 20, there exists fiber end zones 22 and 24 spanning the grating 14. Fiber 12 is mounted to an upper surface 15 of the substrate 16 according to the manufacturing process of the present invention, with grating 14 being conventionally formed utilizing ultraviolet light to selectively change the index of refraction of the core of the fiber 12 in a pattern selected for a wavelength of approximately 1559.25 nm in the example.
Other frequency fiber Bragg gratings or other tuned optical devices can be manufactured with the method of the present invention.
In Fig. 3, there is shown the apparatus for manufacturing the fiber Bragg grating 10 according to the present invention. The apparatus includes a holder 30 for the substrate, which holder generally comprises an open rectangular frame into which the substrate 16 is positioned for holding it in place without adding any significant lateral forces to the substrate during the manufacturing process. The holder 30 rests upon a reference surface 32 during the manufacturing process. At one end (shown on the left in Fig. 3) is a fixed clamp 34 holding one end 19 of the fiber 12 in position with respect to the substrate 16. At an opposite end 21 of the fiber 12, there is positioned a movable clamp 36 comprising a clamp mounted on a moveable stage with micrometer adjustment capabilities. Coupled to the left end of the fiber 12, as seen in Fig. 3, is a broad band optical source 40 while coupled to the opposite end of the optical fiber 12 is an optical spectral analyzer 42 to allow the CWL of the grating to be monitored during the manufacturing process.
In one example for a .125 mm fiber during the first step of manufacturing, a 5 gram load is placed on the fiber. Next, a frit paste 18 is applied to the area adjacent end zone 22 of fiber 12 and a beam from a COz laser 50 is directed to the undersurface 17 of substrate 16 directly under frit paste 18, heating the undersurface of the substrate to a temperature of between 800°C to 900°C and the upper surface onto which the frit past has been applied to approximately 500 ° C to 600 ° C . , fusing the frit to the left end of fiber 12 and to the substrate. The substrate is then allowed to cool for approximately five minutes and the CWL is measured utilizing the optical spectral analyzer 42.
15 Next, the stage for movable clamp 36 is moved to the right in the direction shown by arrow A in Fig. 4 while watching the CWL from analyzer 42 until the CWL is at a predetermined relationship to the desired final CWL. For a negative temperature coefficient 70 mm substrate, such as 13-eucryptite employed in the present invention, typically the strain placed upon the fiber 12 by movable clamp 36 places the CWL below the desired CWL to account for substrate expansion during the cooling of the substrate. In this example, the selected CWL is .35 nm below the target wavelength.
A second bead 20 of glass frit paste is applied to the right end of the fiber 12, as shown in Fig. 4, and the COz laser 50 is positioned under the frit 20 to again heat the under surface of substrate 16 to from 800°C to 900°C and the top surface to from 500°C to 600°C for fusing the glass frit and anchoring end 24 of fiber 12 to the substrate 16. During the fusing process, the CWL is measured twenty seconds after the top hold segment (the twenty second CWL value) while the clamp 36 is held in position. Substrate 16 is then allowed to cool for approximately five minutes, after which the movable clamp releases the tension on the end 21 of fiber 12, and, again, the CWL is tested. Typically, the CWL will at this stage be higher or lower than the target CWL by an amount greater than 10 picometers. For precise fiber Bragg gratings of the type which can be commercially manufactured utilizing the present invention, 10 picometers above or below the CWL is the tolerance limit desired for such precise gratings.
With clamp 34 continuing to maintain the left end of the fiber anchored together with frit 18, movable clamp 36 is moved to the same position as before the load was released to retension the fiber while the second frit 20 is repeated by laser 50. When the heating has reached the top hold segment with the upper surface of the substrate 16 at about 500°C to 600°C, depending upon the direction of the measured CWL, the movable clamp 36 is either moved in a direction indicated by arrow A
to the right in Fig. 5 to increase the tension and thereby increase the CWL or to the left as indicated by arrow B in Fig. 5 to decrease the tension in the fiber 12, thereby decreasing the CWL. If, for example, the CWL is 40 picometers below the target CWL after the first attachment, upon repeating frit 20, the movable clamp is moved in a direction indicated by arrow A while monitoring the CWL through analyzer until the twenty second CWL value is increased by 40 picometers.
Movement of movable clamp 36 during the fine tuning of the grating, while observing the CWL, allows real time control of the manufacturing of the grating 10, and, when at the desired changed twenty second CWL, the clamp 36 holds the fiber 12 stationary for a five minute cooling period of the substrate 16. The final CWL is then recorded and typically falls well within the +/- 10 picometers criteria, with over 80 % of samples tested, as shown by Fig. 6, falling within such range. A
strain relief epoxy is placed over the ends of fiber 12 adjacent the outside edges of frits 18 and 20 on the substrate, and the substrate removed from holder 30. Subsequently, the partially assembled grating is finally packaged in a conventional process to complete the manufacture of the optical fiber device.
Although the preferred embodiment of the invention is employed to manufacture a fiber Bragg grating utilizing glass frits for anchoring the gratings to a negative coefficient substrate, other material for anchoring a glass fiber to other substrates can also be employed. Thus, any anchoring material which can be plasticized after an initial estimated manufacturing CWL has been tested can be WO 01/27691 $ PCT/US00/25364 employed for manufacturing an optical device, such as a fiber Bragg grating, employing the technique of the present invention. Further, the method and apparatus of the present invention can be employed to manufacture any fiber-optic device requiring precise tuning.
It will become apparent to those skilled in the art that various modifications to the preferred embodiment of the invention as described herein can be made without departing from the spirit or scope of the invention as defined by the appended claims.
Foremost of optical fiber components are fiber Bragg gratings (FBG) which are typically made by ultraviolet (UV) wavelength energy exposure. Once an FBG is mounted to a substrate and annealed, it is no longer photosensitive and cannot be further tuned.
Thus, it is necessary to empirically predict the final frequency of such a grating which can lead to a significant error resulting in gratings which are not within specifications.
Due to the uncertainty of the wavelength shift resulting from the attachment process and annealing, the center wavelength (CWL) of a packaged fiber Bragg grating can vary as much as +/- 60 picometers from the desired CWL. Such a wavelength error combined with a wavelength drift of, for example, distributed feedback lasers, which may be from +/- 50 picometers, and the residual temperature dependence of +/-picometers imposes a highly stringent requirement on the design of, for example, 50 GHz fiber Bragg gratings.
A typical attachment process for a fiber Bragg grating is to bond one end of the fiber to a substrate, tension the fiber by an empirically determined amount, and bonding the opposite end of the fiber. Fig. 1 shows the distribution of the CWL for samples manufactured by this process. Since the total available margin is only +/-40 picometers, only a fraction (20 % to 30 % ) of the gratings can be employed.
Precise control of optically tuned fiber-optic devices with a CWL within less than +/- 15 picometers is desired to minimize cross-talk between adjacent communication channels of a system. In order to maintain the CWL of a tuned fiber-optic device, such as a fiber Bragg grating, a 13-eucryptite substrate has been employed having a coefficient of temperature expansion of - 7.5 ppm/°C
to compensate for the refractive index change of the fiber with temperature variations.
With such substrates, the CWL shift due to temperature changes over a range of from 0°C to 70°C has been reduced to +/- 15 pm. Thus, although the substrate selection has improved the stability of the device once manufactured, there remains a need to manufacture devices such as fiber Bragg gratings or other optically tuned components to a CWL that produces a yield rate for precise CWL devices higher than that previously available with existing manufacturing techniques.
It has been discovered that the variability of the CWL of fiber-optic devices is not a function of the laser power employed in the manufacturing of the devices nor is it a result of the substrate material. Instead, it appears that the variability is inherent in the attachment process and there remains a need, therefore, for a process and system for manufacturing precisely tuned fiber-optic devices.
SUMMARY OF THE INVENTION
The method and apparatus of the present invention achieves the manufacturing of fiber-optic devices to precise CWL specifications by plasticizing one attachment end of a mounted fiber-optic device and finely adjusting the fiber tension while monitoring the CWL.
A method of manufacturing an optical fiber component to a precise CWL
includes the step of affixing the ends of a fiber component under tension to a substrate to approximate a desired CWL. Subsequently, one end of the fiber is gripped with a movable clamp and the adjacent attachment plasticized while the tension on the fiber is adjusted until the CWL is within a desired range. The attachment is rehardened while the tension on the fiber is maintained by the movable clamp.
In one embodiment, one end of a fiber is bonded to a negative coefficient of expansion substrate using a glass frit and the opposite end gripped under tension by a movable clamp while the CWL is monitored. The fiber tension is adjusted by moving the clamp until the CWL is about .35 nm below the target CWL for 70 mm substrates. Next, a second frit bonds the fiber to the substrate at an opposite end adjacent the movable clamp. The CWL is again checked and, if off more than 10 picometers, the fiber is retensioned by moving the clamp to the previous position, repeating and plasticizing the second frit, and adjusting the clamp while monitoring the CWL until the CWL change equals an amount corresponding to the difference between the first measured CWL and the target CWL. Once cooled, the clamp is released and the final CWL is measured and recorded.
The result of this process produces precisely tuned fiber-optic devices, such as a fiber Bragg grating. Although particularly suitable for manufacturing fiber Bragg gratings, other tunable fiber-optic components likewise can be manufactured using such technique, to precisely control the optical path length of the optical fiber device during manufacturing.
Additional features and advantages of the invention will be set forth in the detailed description which follows and will be apparent to those skilled in the art from the description or recognized by practicing the invention as described in the description which follows together with the claims and appended drawings.
It is to be understood that the foregoing description is exemplary of the invention only and is intended to provide an overview for the understanding of the nature and character of the invention as it is defined by the claims. The accompanying drawings are included to provide a further understanding of the invention and are incorporated and constitute part of this specification. The drawings illustrate various features and embodiments of the invention which, together with their description serve to explain the principals and operation of the invention.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a chart illustrating the variations in CWL of fiber Bragg gratings manufactured by conventional techniques;
Fig. 2 is an enlarged schematic, side-elevational view of a fiber Bragg grating, shown partially packaged and manufactured according to the present invention;
Fig. 3 is a schematic, side-elevational view of a fiber Bragg grating and an apparatus for manufacturing the same according to the present invention during a first step in the manufacturing process;
Fig. 4 is a schematic, side-elevational view of the next step in the manufacturing process of the fiber Bragg grating shown in Fig. 2;
Fig. 5 is a schematic, side-elevational view of a successive step in the manufacturing process of the fiber Bragg grating shown in Fig. 2; and Fig. 6 is a chart illustrating the high yield of precise CWL fiber Bragg gratings resulting from the manufacturing process of the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
The chart of Fig. 1 illustrates the CWL shift between predicted CWL and actual CWL for 40 samples made using existing techniques which, as seen, vary between approximately 70 nm below the desired CWL (shown by the dotted line in the chart) to about 75 nm above the desired CWL. The number of samples falling within +/- 40 picometers of the desired CWL is relatively small, representing from 20 % to 30 % of the total number of fiber Bragg gratings made by the conventional empirical process.
In order to improve the yield rate to that shown in Fig. 6, the fiber Bragg grating illustrated in Fig. 2 is manufactured according to the process and apparatus described in connection with Figs. 3-5. As seen in Fig. 6, a sample of approximately 70 fiber Bragg gratings manufactured according to the present invention yields 80 %o of gratings falling within +/- 10 picometers of the desired CWL. This tolerance band of precisely manufactured gratings is shown between the dotted lines in Fig. 6.
Even gratings falling outside the precisely controlled band for the most part fell well within an acceptable range of +/- 40 picometers for most applications. Thus, while only very few conventionally manufactured fiber Bragg gratings fall within a +/- 10 picometers criteria, more than 80 % of the gratings manufactured according to the process of the present invention fell within such tolerance range. The dramatic results achieved by the process and apparatus of the present invention and the resulting fiber-optic component is now described in the context of a fiber Bragg grating with reference to Figs. 2-5.
A partially packaged fiber Bragg grating assembly 10 is shown in Fig. 2 and includes an optical fiber 12 in which there is imprinted a grating 14 in a central area with a precisely controlled CWL of, for example, 1559.25 nm. The optical fiber is supported on a negative coefficient of expansion substrate 16, such as 13-eucryptite, by a pair of spaced glass frits 18 and 20. between the glass frits 18 and 20, there exists fiber end zones 22 and 24 spanning the grating 14. Fiber 12 is mounted to an upper surface 15 of the substrate 16 according to the manufacturing process of the present invention, with grating 14 being conventionally formed utilizing ultraviolet light to selectively change the index of refraction of the core of the fiber 12 in a pattern selected for a wavelength of approximately 1559.25 nm in the example.
Other frequency fiber Bragg gratings or other tuned optical devices can be manufactured with the method of the present invention.
In Fig. 3, there is shown the apparatus for manufacturing the fiber Bragg grating 10 according to the present invention. The apparatus includes a holder 30 for the substrate, which holder generally comprises an open rectangular frame into which the substrate 16 is positioned for holding it in place without adding any significant lateral forces to the substrate during the manufacturing process. The holder 30 rests upon a reference surface 32 during the manufacturing process. At one end (shown on the left in Fig. 3) is a fixed clamp 34 holding one end 19 of the fiber 12 in position with respect to the substrate 16. At an opposite end 21 of the fiber 12, there is positioned a movable clamp 36 comprising a clamp mounted on a moveable stage with micrometer adjustment capabilities. Coupled to the left end of the fiber 12, as seen in Fig. 3, is a broad band optical source 40 while coupled to the opposite end of the optical fiber 12 is an optical spectral analyzer 42 to allow the CWL of the grating to be monitored during the manufacturing process.
In one example for a .125 mm fiber during the first step of manufacturing, a 5 gram load is placed on the fiber. Next, a frit paste 18 is applied to the area adjacent end zone 22 of fiber 12 and a beam from a COz laser 50 is directed to the undersurface 17 of substrate 16 directly under frit paste 18, heating the undersurface of the substrate to a temperature of between 800°C to 900°C and the upper surface onto which the frit past has been applied to approximately 500 ° C to 600 ° C . , fusing the frit to the left end of fiber 12 and to the substrate. The substrate is then allowed to cool for approximately five minutes and the CWL is measured utilizing the optical spectral analyzer 42.
15 Next, the stage for movable clamp 36 is moved to the right in the direction shown by arrow A in Fig. 4 while watching the CWL from analyzer 42 until the CWL is at a predetermined relationship to the desired final CWL. For a negative temperature coefficient 70 mm substrate, such as 13-eucryptite employed in the present invention, typically the strain placed upon the fiber 12 by movable clamp 36 places the CWL below the desired CWL to account for substrate expansion during the cooling of the substrate. In this example, the selected CWL is .35 nm below the target wavelength.
A second bead 20 of glass frit paste is applied to the right end of the fiber 12, as shown in Fig. 4, and the COz laser 50 is positioned under the frit 20 to again heat the under surface of substrate 16 to from 800°C to 900°C and the top surface to from 500°C to 600°C for fusing the glass frit and anchoring end 24 of fiber 12 to the substrate 16. During the fusing process, the CWL is measured twenty seconds after the top hold segment (the twenty second CWL value) while the clamp 36 is held in position. Substrate 16 is then allowed to cool for approximately five minutes, after which the movable clamp releases the tension on the end 21 of fiber 12, and, again, the CWL is tested. Typically, the CWL will at this stage be higher or lower than the target CWL by an amount greater than 10 picometers. For precise fiber Bragg gratings of the type which can be commercially manufactured utilizing the present invention, 10 picometers above or below the CWL is the tolerance limit desired for such precise gratings.
With clamp 34 continuing to maintain the left end of the fiber anchored together with frit 18, movable clamp 36 is moved to the same position as before the load was released to retension the fiber while the second frit 20 is repeated by laser 50. When the heating has reached the top hold segment with the upper surface of the substrate 16 at about 500°C to 600°C, depending upon the direction of the measured CWL, the movable clamp 36 is either moved in a direction indicated by arrow A
to the right in Fig. 5 to increase the tension and thereby increase the CWL or to the left as indicated by arrow B in Fig. 5 to decrease the tension in the fiber 12, thereby decreasing the CWL. If, for example, the CWL is 40 picometers below the target CWL after the first attachment, upon repeating frit 20, the movable clamp is moved in a direction indicated by arrow A while monitoring the CWL through analyzer until the twenty second CWL value is increased by 40 picometers.
Movement of movable clamp 36 during the fine tuning of the grating, while observing the CWL, allows real time control of the manufacturing of the grating 10, and, when at the desired changed twenty second CWL, the clamp 36 holds the fiber 12 stationary for a five minute cooling period of the substrate 16. The final CWL is then recorded and typically falls well within the +/- 10 picometers criteria, with over 80 % of samples tested, as shown by Fig. 6, falling within such range. A
strain relief epoxy is placed over the ends of fiber 12 adjacent the outside edges of frits 18 and 20 on the substrate, and the substrate removed from holder 30. Subsequently, the partially assembled grating is finally packaged in a conventional process to complete the manufacture of the optical fiber device.
Although the preferred embodiment of the invention is employed to manufacture a fiber Bragg grating utilizing glass frits for anchoring the gratings to a negative coefficient substrate, other material for anchoring a glass fiber to other substrates can also be employed. Thus, any anchoring material which can be plasticized after an initial estimated manufacturing CWL has been tested can be WO 01/27691 $ PCT/US00/25364 employed for manufacturing an optical device, such as a fiber Bragg grating, employing the technique of the present invention. Further, the method and apparatus of the present invention can be employed to manufacture any fiber-optic device requiring precise tuning.
It will become apparent to those skilled in the art that various modifications to the preferred embodiment of the invention as described herein can be made without departing from the spirit or scope of the invention as defined by the appended claims.
Claims (20)
1. A method of manufacturing an optical fiber component comprising the steps of:
providing an optical fiber having a tunable element;
providing a substrate for the optical fiber;
anchoring one end of the fiber to the substrate;
tensioning the fiber while monitoring the center wavelength of the tunable element formed in the fiber to a predetermined center wavelength;
anchoring an opposite end of the fiber to the substrate;
measuring the center wavelength of the resulting tunable element;
plasticizing one of the anchored ends while adjusting the tension on the fiber to change the monitored center wavelength an amount selected to reach a target center wavelength; and hardening the one anchor point.
providing an optical fiber having a tunable element;
providing a substrate for the optical fiber;
anchoring one end of the fiber to the substrate;
tensioning the fiber while monitoring the center wavelength of the tunable element formed in the fiber to a predetermined center wavelength;
anchoring an opposite end of the fiber to the substrate;
measuring the center wavelength of the resulting tunable element;
plasticizing one of the anchored ends while adjusting the tension on the fiber to change the monitored center wavelength an amount selected to reach a target center wavelength; and hardening the one anchor point.
2. The method of claim 1 wherein the monitoring step comprises applying a broadband optical signal at one end of the fiber and coupling an optical spectral analyzer to the opposite end of the fiber.
3. The method of claim 1 wherein the anchoring steps comprise applying a glass frit paste to the fiber and heating and subsequently cooling the substrate to fuse the frit paste to the fiber and substrate.
4. The method of claim 3 wherein the plasticizing step comprises repeating one of the anchor points to a temperature to allow the fiber tension to be adjusted.
5. The method of claim 4 wherein the plasticizing step comprises heating the frit to a temperature of from about 500°C to about 600°C.
6. The method of claim 1 wherein said tensioning steps comprise clamping the opposite end of the optical fiber in a clamp movable in a direction toward and away from the one end of the optical fiber.
7. The method of claim 1 wherein the tunable element of the optical fiber is a grating.
8. The method of claim 1 wherein the fiber optic component is a fiber Bragg grating.
9. An apparatus for manufacturing a precise fiber Bragg grating comprising:
a holder for a substrate;
a first clamp for clamping one end of a fiber during its attachment to the substrate held by the holder;
a movable clamp positioned adjacent an end of the holder opposite the first clamp, the movable clamp adjustable to adjust the tension in a fiber mounted to the substrate;
a broad band source of radiation for coupling to an input end of the fiber;
a structure for selectively anchoring opposite ends of the fiber onto said substrate during first and second adjustments of the movable clamp to achieve a target center wavelength for a fiber Bragg grating mounted to a substrate; and an optical analyzer for coupling to an opposite end of said fiber to monitor the center wavelength of the grating during the first and second adjustments of the movable clamp.
a holder for a substrate;
a first clamp for clamping one end of a fiber during its attachment to the substrate held by the holder;
a movable clamp positioned adjacent an end of the holder opposite the first clamp, the movable clamp adjustable to adjust the tension in a fiber mounted to the substrate;
a broad band source of radiation for coupling to an input end of the fiber;
a structure for selectively anchoring opposite ends of the fiber onto said substrate during first and second adjustments of the movable clamp to achieve a target center wavelength for a fiber Bragg grating mounted to a substrate; and an optical analyzer for coupling to an opposite end of said fiber to monitor the center wavelength of the grating during the first and second adjustments of the movable clamp.
10. The apparatus of claim 9 wherein the structure for anchoring opposite ends of the fiber includes a laser for heating and reheating a glass frit employed to anchor the optical fiber to the substrate.
11. The apparatus of claim 10 wherein the laser is a CO2 laser.
12. The apparatus of claim 9 wherein the movable clamp comprises a second clamp and a micrometer adjustment stage for moving the second clamp in precise amounts for changing the center wavelength of the grating.
13. A fiber Bragg grating made by the steps of:
anchoring one end of a fiber Bragg grating to a substrate;
tensioning the fiber while monitoring the center wavelength of the grating to a predetermined center wavelength;
anchoring an opposite end of the fiber to the substrate;
measuring the center wavelength of the grating; and plasticizing one of the anchored ends of the grating while adjusting the tension on the fiber to change the monitored center wavelength an amount selected to reach a target center wavelength; and hardening the one anchor point.
anchoring one end of a fiber Bragg grating to a substrate;
tensioning the fiber while monitoring the center wavelength of the grating to a predetermined center wavelength;
anchoring an opposite end of the fiber to the substrate;
measuring the center wavelength of the grating; and plasticizing one of the anchored ends of the grating while adjusting the tension on the fiber to change the monitored center wavelength an amount selected to reach a target center wavelength; and hardening the one anchor point.
14. A method of manufacturing a fiber Bragg grating comprising the steps of:
mounting an optical fiber having a grating onto a substrate;
measuring the center wavelength of the resulting grating;
plasticizing one of the mounted ends of the grating while adjusting the tension on the fiber while monitoring the center wavelength until a target center wavelength is detected; and hardening the one end.
mounting an optical fiber having a grating onto a substrate;
measuring the center wavelength of the resulting grating;
plasticizing one of the mounted ends of the grating while adjusting the tension on the fiber while monitoring the center wavelength until a target center wavelength is detected; and hardening the one end.
15. The method of claim 14 wherein the mounting step comprises applying a glass frit paste to the fiber and heating and subsequently cooling the substrate to fuse the frit paste to the fiber and substrate.
16. The method of claim 14 wherein the plasticizing step comprises repeating one of the frits to a temperature to allow the fiber tension to be adjusted.
17. The method of claim 16 wherein the plasticizing step comprises heating the frit to a temperature of from about 500°C to about 600°C.
18. The method of claim 14 wherein said adjusting step comprises clamping an end of the optical fiber in a clamp movable in a direction toward and away from the opposite end of the optical fiber.
19. The method of claim 18 wherein the plasticizing step comprises reheating one of the frits to a temperature to allow the fiber tension to be adjusted.
20. The method of claim 14 wherein the monitoring step comprises applying a broadband optical signal at one end of the fiber and coupling an optical spectral analyzer to the opposite end of the fiber.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/417,261 US6278819B1 (en) | 1999-10-12 | 1999-10-12 | Method and apparatus for manufacturing optical fiber components |
| US09/417,261 | 1999-10-12 | ||
| PCT/US2000/025364 WO2001027691A1 (en) | 1999-10-12 | 2000-09-15 | Method and apparatus for manufacturing optical fiber components |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2385604A1 true CA2385604A1 (en) | 2001-04-19 |
Family
ID=23653230
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002385604A Abandoned CA2385604A1 (en) | 1999-10-12 | 2000-09-15 | Method and apparatus for manufacturing optical fiber components |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US6278819B1 (en) |
| EP (1) | EP1221067A4 (en) |
| JP (1) | JP2003511741A (en) |
| CN (1) | CN1378658A (en) |
| AU (1) | AU7583800A (en) |
| CA (1) | CA2385604A1 (en) |
| TW (1) | TW542925B (en) |
| WO (1) | WO2001027691A1 (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999047955A1 (en) * | 1998-03-17 | 1999-09-23 | Minnesota Mining And Manufacturing Company | Passively compensated optical fibers |
| US6360042B1 (en) * | 2001-01-31 | 2002-03-19 | Pin Long | Tunable optical fiber gratings device |
| US6925263B2 (en) * | 2001-09-28 | 2005-08-02 | Intel Corporation | Method and apparatus for transmission of upstream data in an optical network |
| US20030108286A1 (en) * | 2001-12-06 | 2003-06-12 | Jacques Albert | Adjustable temperature compensating package for optical fiber devices |
| EP1345059A1 (en) * | 2002-03-16 | 2003-09-17 | Agilent Technologies, Inc. (a Delaware corporation) | Integrated micro-optical elements |
| CN1295531C (en) * | 2004-12-21 | 2007-01-17 | 中国科学院上海光学精密机械研究所 | Soft packaging optical fiber grating sensor with vernier wavelength |
| US9988295B2 (en) * | 2016-02-15 | 2018-06-05 | FOMS Inc. | Fiber optic manufacturing in space |
| CN110233415B (en) * | 2019-05-29 | 2020-05-01 | 山东省科学院激光研究所 | Distributed feedback fiber laser with multiple tunable wavelengths |
| CN110941044B (en) * | 2019-12-27 | 2021-04-09 | 天津工业大学 | Convex cone cascade-based ultra-compact ultra-long period fiber grating manufacturing method |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5218655A (en) * | 1992-05-29 | 1993-06-08 | At&T Bell Laboratories | Article comprising an optical waveguide with in-line refractive index grating |
| US5949934A (en) * | 1996-04-05 | 1999-09-07 | Fujikura, Ltd. | Optical waveguide grating and production method therefor |
| US5841920A (en) * | 1997-03-18 | 1998-11-24 | Lucent Technologies Inc. | Fiber grating package |
| KR100283866B1 (en) * | 1998-10-02 | 2001-03-02 | 박호군 | Gain Control Device and Method of Fiber Optic Amplifier |
-
1999
- 1999-10-12 US US09/417,261 patent/US6278819B1/en not_active Expired - Lifetime
-
2000
- 2000-09-15 CA CA002385604A patent/CA2385604A1/en not_active Abandoned
- 2000-09-15 EP EP00965052A patent/EP1221067A4/en not_active Withdrawn
- 2000-09-15 JP JP2001530642A patent/JP2003511741A/en active Pending
- 2000-09-15 CN CN00814036A patent/CN1378658A/en active Pending
- 2000-09-15 AU AU75838/00A patent/AU7583800A/en not_active Abandoned
- 2000-09-15 WO PCT/US2000/025364 patent/WO2001027691A1/en not_active Application Discontinuation
- 2000-10-13 TW TW089121536A patent/TW542925B/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| AU7583800A (en) | 2001-04-23 |
| TW542925B (en) | 2003-07-21 |
| EP1221067A4 (en) | 2005-04-27 |
| CN1378658A (en) | 2002-11-06 |
| US6278819B1 (en) | 2001-08-21 |
| JP2003511741A (en) | 2003-03-25 |
| WO2001027691A1 (en) | 2001-04-19 |
| EP1221067A1 (en) | 2002-07-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6356681B1 (en) | Method and apparatus for trimming the optical path length of optical fiber components | |
| JP3316218B2 (en) | Post-tuning method for accurate setting of center frequency of temperature stable Bragg grating package | |
| JP3805366B2 (en) | Chirped optical fiber grating | |
| US5931983A (en) | Method of forming a fiber optic coupler by dynamically adjusting pulling speed | |
| US6278819B1 (en) | Method and apparatus for manufacturing optical fiber components | |
| CA2209710C (en) | Compact tunable wavelength independent all-fiber optical attenuator and method of making same | |
| US6568220B1 (en) | Method of fabricating optical fiber gratings maximizing residual mechanical stress in the optical fibers | |
| JP2001042148A (en) | Optical device and method for correcting its prescribed light-transmissive characteristic | |
| JP2000098316A (en) | Fiber element having variable refractive index region in proximity to core | |
| US6229941B1 (en) | Apparatus and method of fabricating long-period fiber grating | |
| US20030039448A1 (en) | Method and apparatus for tuning an optical device | |
| EP1332389B1 (en) | Method to stabilize and adjust the optical path length difference in an interferometer | |
| US20040161197A1 (en) | Adjustable chromatic dispersion compensator | |
| US6782152B2 (en) | Method and apparatus for frequency tuning of an unbalanced Mach-Zehnder interferometer | |
| US20040071380A1 (en) | Pretrimming of tunable finite response (FIR) filter | |
| JP2001074950A (en) | Method for adjusting characteristic for optical multiplexer/demultiplexer | |
| Starodubov et al. | Ultrastrong fiber gratings and their applications | |
| CA2389199A1 (en) | Container for optical fibre components | |
| JPH06308546A (en) | Method for adjusting characteristic of optical circuit | |
| JP3587679B2 (en) | Gain flattener and optical transmission system using gain flattener | |
| JP2002072034A (en) | Tunable dispersion compensator | |
| US6498879B1 (en) | Polarization-independent, environmentally stable optical fiber narrow band multi-window wavelength division multiplexer based on biconical tapered fusion coupler technology | |
| JP2002214456A (en) | Method for manufacturing optical fiber grating | |
| US6990274B2 (en) | Apparatus and method for adjusting the spectral response of an optical waveguide grating | |
| Kashyap et al. | Four wavelength dispersion compensation over 125 km of single mode optical fibre at 10 Gbs/sup-1/using multiple in-line step-chirped gratings |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Discontinued |