|Publication number||US6868212 B2|
|Application number||US 10/383,909|
|Publication date||15 Mar 2005|
|Filing date||6 Mar 2003|
|Priority date||6 Mar 2003|
|Also published as||US20040175081|
|Publication number||10383909, 383909, US 6868212 B2, US 6868212B2, US-B2-6868212, US6868212 B2, US6868212B2|
|Inventors||Jeannie DeWitte, Yuri Grapov, David Owen, Dennis Elkins, Aaron McAllister, Allen Tanner|
|Original Assignee||Evans & Sutherland Computer Corporation|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (19), Referenced by (6), Classifications (12), Legal Events (4)|
|External Links: USPTO, USPTO Assignment, Espacenet|
1. Field of the Invention
The present invention relates generally to the tuning of fiber lasers. More particularly, the present invention relates to an apparatus and method for initially adjusting the wavelength and dominant mode of a fiber laser during installation into a laser assembly.
2. Related Art
Fiber lasers provide an excellent source of infrared energy for coupling in external conversion cavities. Fiber lasers can provide a simple source of high power, single mode infrared energy. In essence, a fiber laser is an optically pumped resonator with a doped-fiber as the gain medium. Fiber lasers are manufactured by subjecting a doped photosensitive fiber to an interference pattern of ultraviolet laser light to create a periodic variation in the refractive index of the fiber. This variation in the refractive index creates the resonating cavity of the distributed feedback laser.
It is well known that stressing a fiber by compression or elongation alters the wavelength and modes produced by the laser. Stressing the fiber alters both the period of the resonating cavity imprinted on the fiber, and the favored polarization of the emitted light.
There are a number of prior inventions that relate to stressing fiber lasers. Some of these provide a method for tuning a fiber laser's wavelength by imposing stress on the fiber through mechanical or thermal compression or tension. These prior methods use a variety of mechanisms for accomplishing this task, including levers, screw mechanisms, elongating stems, and bimetallic strips. Some prior inventions also allow longitudinal mode selection.
These mechanical stressing methods provide a means of control during normal operation of the laser, but do not provide a means of permanently tuning the laser during fabrication and assembly, or while connecting the fiber to a more sensitive control mechanism.
The present invention advantageously provides a method and apparatus for adjusting a fiber laser's wavelength and dominant mode to be within a certain threshold during installation, to thereby allow its dynamic tuning assembly to more accurately adjust within a dynamic range during use.
In accordance with one aspect thereof, the invention provides a method for adjusting an output wavelength and a dominant mode of a laser fiber prior to installation in a laser assembly. The method includes the steps of a) linearly stretching the laser fiber so as to modify its output characteristics; b) axially twisting the laser fiber so as to modify its output characteristics; and c) affixing the laser fiber to a laser assembly in its linearly stretched and axially twisted condition.
In accordance with another aspect of the present invention, the invention provides an apparatus for tuning the output wavelength and dominant mode of a fiber laser. The apparatus includes a moveable bed, a rotatable gear assembly, and an adjustment mechanism. The moveable bed is configured to receive a fiber laser assembly with a first end of a laser fiber affixed to it. A second end of the laser fiber is clamped to the rotatable gear assembly. The adjustment mechanism is configured to (i) move the bed linearly away from the gear assembly, so as to linearly stretch the laser fiber, and (ii) rotate the gear assembly to axially twist the laser fiber. These actions allow rough adjustment of the output wavelength and dominant mode of the laser fiber prior to permanently affixing the laser fiber to the fiber laser assembly.
In accordance with yet another aspect thereof, the invention provides a fiber laser for emitting a laser beam, the fiber laser comprising a substrate with a length of laser fiber coupled thereto. The substrate includes a dynamic tuning mechanism that is configured to modify an adjusted output wavelength of the laser fiber by adjusting the length of the fiber during use. Advantageously, the laser fiber is coupled to the substrate in a linearly stretched and axially twisted condition, such that an unadjusted wavelength and dominant mode of the fiber are within a selected range before adjustment by the dynamic tuning mechanism.
Additional features and advantages of the invention will be apparent from the detailed description which follows, taken in conjunction with the accompanying drawings, which together illustrate, by way of example, features of the invention.
Reference will now be made to the exemplary embodiments illustrated in the drawings, and specific language will be used herein to describe the same. It will nevertheless be understood that no limitation of the scope of the invention is thereby intended. Alterations and further modifications of the inventive features illustrated herein, and additional applications of the principles of the inventions as illustrated herein, which would occur to one skilled in the relevant art and having possession of this disclosure, are to be considered within the scope of the invention.
Fiber lasers are currently used in a wide variety of applications. They are used for high-power projectors, laser cutting or marking systems, optical communication systems, and any application where one laser is used to pump another laser. In most uses of fiber lasers, it is desirable to maintain the laser signal at a constant output wavelength. However, the output of a fiber laser can change during use in response to temperature variations and mechanical vibrations. As a fiber laser apparatus heats up or is vibrated, the output wavelength of the laser light can change substantially. To compensate for this, typical fiber laser assemblies are configured to dynamically tune the laser by adjusting the length of the laser fiber, thereby changing the length and period of oscillation.
The piezo-electric crystal 116 is configured to very accurately and rapidly extend or contract the distance between the two fiber clamps 112 in response to electrical signals provided thereto. Similarly, the heating element 114 thermally expands or contracts in response to electrical current to adjust the distance between the fiber clamps. With these two components, the dynamic tuning mechanism continuously, dynamically tunes the laser 100 by adjusting the distance between the clamps, based upon feedback that senses the output wavelength of the laser during use, so as to continuously tune the output wavelength in response to temperature variations, mechanical vibrations, or other factors. This allows the laser assembly to maintain a constant output wavelength under a variety of conditions.
It will be apparent that the dynamic tuning mechanism 102 will have mechanical limits to its range of adjustment. Consequently, to effectively maintain the desired output wavelength, the unadjusted output characteristics of the laser fiber 106 must start within a range that the dynamic tuning assembly can effectively adjust to compensate for foreseeable conditions. This requires that the physical dimensions of the laser fiber be very carefully controlled during manufacture. Additionally, variations in the quality and physical characteristics of the laser fiber itself also contribute to variations in the output wavelength. Consequently, in order to produce fiber lasers with desired output characteristics, highly accurate and expensive manufacturing processes are required. Naturally, this increases the cost and limits the range of application of fiber lasers.
Advantageously, the inventors have devised a method and apparatus for tuning a fiber laser during manufacture that provides a more accurate gross adjustment of the laser output wavelength characteristics, such that lower manufacturing tolerances will still produce a fiber laser that has unadjusted output characteristics within an acceptable range for a dynamic tuning device. At the same time, the inventors have also discovered a method for isolating the dominant mode of a fiber laser.
The term “dominant mode” refers to the dominant mode of oscillation of the fiber laser. For a given laser application, it is often desirable to have light energy of a single oscillation mode. However, in part because of impurities or inconsistencies in the material of the laser fiber, additional modes will still be produced. These additional modes take energy away from the desired mode, thus reducing the energy efficiency of the laser. It is thus desirable to isolate the desired mode as the dominant mode, and to suppress other modes.
The inventors have found that axially twisting a laser fiber tunes the laser to the dominant mode, and suppresses other modes. The exact reasons for this are not entirely clear. It is believed that because laser fibers are comprised of birefringent material, torsional stress on this material suppresses all but the dominant mode. However, the exact mechanism is still unclear. Nevertheless, extensive testing has confirmed that twisting of a laser fiber has the effect of suppressing undesired oscillation modes in the fiber.
Based on these discoveries, the inventors have developed a method and apparatus for initially tuning the wavelength and dominant mode of a fiber laser during installation into a laser assembly. The invention provides a means to adjust a fiber laser's wavelength during installation to get the wavelength in the correct range for the tuning system. It also isolates the dominant mode. The invention effectively decreases the required manufacturing tolerances of fiber lasers and increases the effective dynamic range of the dynamic tuning system by eliminating biases.
The apparatus functions to twist and stretch a laser fiber as an initial adjustment before installation into a laser assembly. The apparatus 10 for twisting and stretching the fiber laser is shown in
The gear assembly 16 includes a rotatable axle 28 disposed at the centerline of the gear assembly housing 30. The axle is axially aligned with the long axis of the laser fiber 106 when a laser assembly 100 is disposed in the laser groove 24. The axle includes a fiber mounting platform 32 and a center aperture 34, and the gear assembly housing includes a fiber loading groove 36 to allow a fiber to be slid to the center aperture. Once in place, the fiber is affixed to the fiber mounting platform with a fiber clamp 38, and the long axis of the fiber thereby becomes collinear with the axis of rotation of the gear assembly, so that rotation of the axle has the effect of axially twisting the fiber about its long axis.
The gear assembly 16 includes a gear assembly knob 40, which is interconnected to a highly accurate reduction gear system (not shown) disposed within the gear assembly housing 30. When a user rotates the gear assembly knob, as indicated by arrow 42, this causes the reduction gear assembly to rotate the axle 28 and thereby twist the fiber 106, as indicated by arrow 44. In one embodiment, the system is designed such that one rotation of the gear assembly knob produces one quarter rotation of the axle. This provides very accurate control of the amount of rotation applied to the fiber, allowing a user to accurately apply very small amounts of twist to the fiber. Naturally, other rotational ratios could be used.
The wedge assembly 20 is connected to the base 12 and disposed between the slidable bed 14 and the gear assembly housing 30. The wedge assembly includes a metal wedge 46, interconnected to a micrometer drive 48 oriented perpendicular to the axis of the fiber 106. Rotation of the micrometer drive, as indicated by arrow 50, pushes and rotates the wedge against a spring 52, thereby sliding the bed linearly along the track, as indicated by arrow 54. This has the effect of lengthening the distance between the laser assembly clamp 112 at the first end 108 of the laser assembly 100, and the fiber clamp 38 disposed on the fiber mounting platform 32, thereby linearly stretching the fiber. The micrometer drive allows the user to very accurately stretch the fiber in very small increments, so as to very accurately adjust the output wavelength. When the fiber is stretched and twisted to the desired extent, the fiber assembly clamp 112 at the second end 110 of the laser assembly is then clamped, fixing the laser fiber in place with a proper gross adjustment.
The invention thus roughly tunes the wavelength by stretching the fiber, and tunes the dominant mode by twisting the fiber, before installation onto the laser assembly. To allow this tuning, the fiber laser operates during adjustment. Referring to
It will be apparent that the system could be automated. Force to mechanically twist and pull the fiber 106 could be provided by motors or other mechanical devices (not shown), rather than by a user manually turning knobs. The mechanical twisting and pulling mechanisms in turn could be computer controlled and interconnected to the feedback devices (the wavelength meter 62 and optical spectrum analyzer 64), creating a system that automatically tunes the fiber laser to the desired wavelength and dominant mode, and then fixes it to the laser assembly.
The apparatus 10 thus allows rough adjustment of the wavelength and oscillation modes while clamping a laser fiber 106 to a laser assembly 100, and is configured for mating the laser assembly to the apparatus while attaching the fiber. Once the adjustment of the modes is completed and the wavelength is within the desired tolerance, the second clamp 112 on the second end 110 of the laser assembly is tightened to maintain the level of stress (both axial and torsional) in the fiber, and the laser assembly is then freed from the device to be installed in the final optical system.
It will be apparent that the actual required magnitude of twisting and pulling of the fiber to accomplish the purposes of the invention is actually quite small. In one operative example, using a fiber laser of 5.0 cm in length and having a desired wavelength centered at 1064 nm, the inventors have found that typical linear stretching within a range of from 0 to about 500 μm and axial twisting of about ±360° is usually sufficient to tune the wavelength and dominant mode of the fiber to the desired level, in spite of product irregularities and manufacturing variations inherent in the fibers. To this end, the limit of total linear travel of the bed 14 in the depicted apparatus 10 is about 10 mm, and the mechanical limit of rotation of the gear assembly 16 is about ±3 revolutions. It will be apparent, however, that these limits will not necessarily be suitable for all sizes and types of fibers.
It is to be understood that the above-referenced arrangements are illustrative of the application for the principles of the present invention. Numerous modifications and alternative arrangements can be devised without departing from the spirit and scope of the present invention while the present invention has been shown in the drawings and described above in connection with the exemplary embodiments(s) of the invention. It will be apparent to those of ordinary skill in the art that numerous modifications can be made without departing from the principles and concepts of the invention as set forth in the claims.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US4636031||28 Oct 1983||13 Jan 1987||Chevron Research Company||Process of tuning a grated optical fiber and the tuned optical fiber|
|US4725110||27 Oct 1986||16 Feb 1988||United Technologies Corporation||Method for impressing gratings within fiber optics|
|US5007705||26 Dec 1989||16 Apr 1991||United Technologies Corporation||Variable optical fiber Bragg filter arrangement|
|US5053698 *||19 Oct 1989||1 Oct 1991||Fujitsu Limited||Test device and method for testing electronic device and semiconductor device having the test device|
|US5159601||17 Jul 1991||27 Oct 1992||General Instrument Corporation||Method for producing a tunable erbium fiber laser|
|US5691999||30 Sep 1994||25 Nov 1997||United Technologies Corporation||Compression-tuned fiber laser|
|US6188712 *||9 Aug 1999||13 Feb 2001||Optigain, Inc.||Asymmetrical distributed feedback fiber laser|
|US6229827||6 Dec 1999||8 May 2001||Cidra Corporation||Compression-tuned bragg grating and laser|
|US6240220||29 Jul 1998||29 May 2001||E-Tek Dynamics, Inc.||Tunable optical fiber package|
|US6356683||3 Dec 1999||12 Mar 2002||Industrial Technology Research Institute||Optical fiber grating package|
|US6360042||31 Jan 2001||19 Mar 2002||Pin Long||Tunable optical fiber gratings device|
|US6363089||19 Oct 2000||26 Mar 2002||Cidra Corporation||Compression-tuned Bragg grating and laser|
|US6366721||21 Jan 2000||2 Apr 2002||Industrial Technology Research Institute||Tunable optical fiber grating|
|US6374015||1 Aug 2000||16 Apr 2002||Rich Key Technologies Limited||Temperature-compensating device with tunable mechanism for optical fiber gratings|
|US6393181||18 Jun 1998||21 May 2002||Jds Uniphase Pty. Ltd.||Temperature stable Bragg grating package with post tuning for accurate setting of centre frequency|
|US6396994||10 Mar 2000||28 May 2002||Jds Uniphase Inc.||Apparatus for varying the optical characteristics of an optical fiber by stretching the fiber|
|US6643299 *||31 Dec 2001||4 Nov 2003||Calmar Optcom, Inc.||Bi-metal and other passive thermal compensators for fiber-based devices|
|US6671293 *||19 Nov 2002||30 Dec 2003||Chiral Photonics, Inc.||Chiral fiber laser apparatus and method|
|US20020071453 *||17 Jul 2001||13 Jun 2002||Hong Lin||Active and low-power laser stabilization|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US7891818||12 Dec 2007||22 Feb 2011||Evans & Sutherland Computer Corporation||System and method for aligning RGB light in a single modulator projector|
|US8077378||12 Nov 2009||13 Dec 2011||Evans & Sutherland Computer Corporation||Calibration system and method for light modulation device|
|US8358317||22 Jan 2013||Evans & Sutherland Computer Corporation||System and method for displaying a planar image on a curved surface|
|US8644651 *||21 Apr 2011||4 Feb 2014||Ge Healthcare Bio-Sciences Corp.||Uniform light source for an imaging instrument|
|US8702248||11 Jun 2009||22 Apr 2014||Evans & Sutherland Computer Corporation||Projection method for reducing interpixel gaps on a viewing surface|
|US20110286232 *||24 Nov 2011||William Dougherty||Uniform light source for an imaging instrument|
|U.S. Classification||385/123, 385/14, 372/6, 385/13|
|International Classification||H01S3/102, G02B6/02, H01S3/067|
|Cooperative Classification||H01S3/102, G02B6/022, H01S3/06704|
|European Classification||H01S3/067B, H01S3/102|
|11 Jul 2003||AS||Assignment|
Owner name: EVANS & SUTHERLAND COMPUTER CORPORATION, UTAH
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:DEWITTE, JEANNIE;GRAPOV, YURI;OWEN, DAVID;AND OTHERS;REEL/FRAME:014264/0171;SIGNING DATES FROM 20030322 TO 20030407
|15 Sep 2008||FPAY||Fee payment|
Year of fee payment: 4
|25 Apr 2012||FPAY||Fee payment|
Year of fee payment: 8
|22 Jul 2015||AS||Assignment|
Owner name: PENSION BENEFIT GUARANTY CORPORATION, DISTRICT OF
Free format text: SECURITY INTEREST;ASSIGNORS:EVANS & SUTHERLAND COMPUTER CORPORATION;SPITZ, INC.;REEL/FRAME:036149/0501
Effective date: 20150721