US20220404543A1 - Devices, systems, and methods for temporal compression or stretching of optical pulses - Google Patents
Devices, systems, and methods for temporal compression or stretching of optical pulses Download PDFInfo
- Publication number
- US20220404543A1 US20220404543A1 US17/896,458 US202217896458A US2022404543A1 US 20220404543 A1 US20220404543 A1 US 20220404543A1 US 202217896458 A US202217896458 A US 202217896458A US 2022404543 A1 US2022404543 A1 US 2022404543A1
- Authority
- US
- United States
- Prior art keywords
- optical
- reflective surface
- optical component
- pulse
- optical system
- 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
- 230000003287 optical effect Effects 0.000 title claims abstract description 293
- 230000006835 compression Effects 0.000 title description 18
- 238000007906 compression Methods 0.000 title description 18
- 238000000034 method Methods 0.000 title description 4
- 230000002123 temporal effect Effects 0.000 title description 3
- 239000011248 coating agent Substances 0.000 claims abstract description 24
- 238000000576 coating method Methods 0.000 claims abstract description 24
- 239000006185 dispersion Substances 0.000 claims abstract description 16
- 239000000835 fiber Substances 0.000 claims description 10
- ORQBXQOJMQIAOY-UHFFFAOYSA-N nobelium Chemical compound [No] ORQBXQOJMQIAOY-UHFFFAOYSA-N 0.000 description 11
- 238000013461 design Methods 0.000 description 4
- 239000013307 optical fiber Substances 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000001228 spectrum Methods 0.000 description 3
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 238000003491 array Methods 0.000 description 1
- 238000000231 atomic layer deposition Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- -1 for example Substances 0.000 description 1
- 239000005350 fused silica glass Substances 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 238000000869 ion-assisted deposition Methods 0.000 description 1
- 238000001659 ion-beam spectroscopy Methods 0.000 description 1
- 238000001755 magnetron sputter deposition Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000386 microscopy Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012634 optical imaging Methods 0.000 description 1
- 238000000399 optical microscopy Methods 0.000 description 1
- 238000002310 reflectometry Methods 0.000 description 1
- 230000003595 spectral effect Effects 0.000 description 1
- 238000004611 spectroscopical analysis Methods 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
Images
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
- G02B6/02195—Refractive index modulation gratings, e.g. Bragg gratings characterised by means for tuning the grating
- G02B6/022—Refractive index modulation gratings, e.g. Bragg gratings characterised by means for tuning the grating using mechanical stress, e.g. tuning by compression or elongation, special geometrical shapes such as "dog-bone" or taper
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/005—Optical devices external to the laser cavity, specially adapted for lasers, e.g. for homogenisation of the beam or for manipulating laser pulses, e.g. pulse shaping
- H01S3/0057—Temporal shaping, e.g. pulse compression, frequency chirping
-
- 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
- G02B6/0001—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings specially adapted for lighting devices or systems
- G02B6/0011—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings specially adapted for lighting devices or systems the light guides being planar or of plate-like form
- G02B6/0013—Means for improving the coupling-in of light from the light source into the light guide
- G02B6/0023—Means for improving the coupling-in of light from the light source into the light guide provided by one optical element, or plurality thereof, placed between the light guide and the light source, or around the light source
-
- 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
- G02B6/02295—Microstructured optical fibre
- G02B6/023—Microstructured optical fibre having different index layers arranged around the core for guiding light by reflection, i.e. 1D crystal, e.g. omniguide
- G02B6/02304—Core having lower refractive index than cladding, e.g. air filled, hollow core
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/0014—Monitoring arrangements not otherwise provided for
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/005—Optical devices external to the laser cavity, specially adapted for lasers, e.g. for homogenisation of the beam or for manipulating laser pulses, e.g. pulse shaping
Definitions
- Stretching or compressing optical pulses can be useful in a variety of applications.
- One method of achieving stretching or compressing of pulses is the use of a long dispersive optical fiber to guide and propagate the light pulse. Because of the chromatic dispersion of the optical fiber, different frequency components experience different refractive indices and travel at different speeds along the fiber. This separates different frequency components in time.
- Optical fibers can also be used to compress pulses. This may be useful in telecommunications and in optical microscopy and imaging. However, the amount of stretching or compressing is limited by the length of the fiber. The acceptable wavelengths may also be restricted based on the material of the fiber. In addition, the pulses may experience linear dispersion that may distort the pulses.
- the present disclosure relates generally to optical systems, and more particularly, optical systems for temporal compression or stretching of optical pulses.
- an optical system includes a first optical component including a reflective surface opposing a second optical component; and the second optical component including a non-flat reflective surface opposing the first optical component, wherein a portion of the first optical component allows an optical pulse to pass through the first optical component and reflect off the non-flat reflective surface, an arrangement of the first optical component and the second optical component defines a self-focusing cavity that refocuses the optical pulse and controls divergence of the optical pulse, and at least one of the reflective surface and the non-flat reflective surface is coated with a group delay dispersion (GDD) coating.
- GDD group delay dispersion
- a distance and a rotation angle between the first optical component and the second optical component are adjustable to change a number of times the optical pulse reflects off the reflective surface and the non-flat reflective surface before exiting the optical system without changing optical alignment.
- the reflective surface includes a flat reflective surface, and the portion of the first optical component allows the optical pulse reflected off the second optical component to exit the optical system.
- the reflective surface includes a non-flat reflective surface to reflect the optical pulse from a portion of the second optical component to another portion of the second optical component, and the other portion of the second optical component allows the optical pulse to exit the optical system.
- the portion of the first optical component comprises a truncated edge, notch, or hole and is coupled to a hollow core fiber.
- the GDD coating comprises a negative GDD coating that temporally compresses the optical pulse passing through the optical system.
- a GDD of at least one of the reflective surface of the first optical component and the non-flat reflective surface of the second optical component is less than ⁇ 20 femtoseconds2 (fs2).
- the GDD coating includes a positive GDD coating that stretches the optical pulse passing through the optical system.
- a GDD of at least one of the reflective surface of the first optical component and the non-flat reflective surface of the second optical component is greater than 20 femtoseconds2 (fs2).
- the optical system compresses or stretches the optical pulse based on a type of wavelength.
- the portion of the first optical component is an uncoated portion of the first optical component.
- either the first optical component or the second optical component allows the optical pulse to exit the optical system.
- the reflective surface comprises a flat reflective surface.
- the reflective surface comprises a non-flat reflective surface.
- the optical system can further include a light emitting device that generates the optical pulse.
- an optical system in another embodiment, includes a first optical component including a reflective surface opposing a second optical component, and the second optical component including a non-flat reflective surface opposing the first optical component, wherein a portion of the first optical component allows an optical pulse to pass through the first optical component and reflect off the non-flat reflective surface, a distance and a rotation angle between the first optical component and the second optical component are adjustable to change a number of times the optical pulse reflects off the reflective surface and the non-flat reflective surface before exiting the optical system without changing optical alignment, the distance between the first optical component and the second optical component is adjustable in discrete increments that are predetermined to correlate with specific numbers of reflections of the optical pulse within the optical system while controlling the divergence of the optical pulse, and the rotation angle between the first optical component and the second optical component is adjustable to change the number of times the optical pulse is reflected off the reflective surface and the non-flat reflective surface while controlling the divergence of the optical pulse.
- the optical system can further include a hollow core fiber coupled to the portion of the first optical component.
- the optical system can further include further include a light emitting device that generates the optical pulse, wherein the light emitting device comprises an ultrafast laser oscillator or amplifier.
- either the first optical component or the second optical component allows the optical pulse to exit the optical system.
- the first optical component or the second optical component is coated with a group delay dispersion (GDD) coating.
- GDD group delay dispersion
- FIG. 1 shows an optical system according to one embodiment described herein.
- FIG. 2 shows an optical system according to another embodiment described herein.
- FIG. 3 shows an optical system according to another embodiment described herein.
- FIG. 4 illustrates a chirped pulse modification system including a compressor system according to embodiments described herein.
- FIG. 5 illustrates a system for dispersion compensation of chirped ultrafast pulses including a compressor according to embodiments described herein.
- FIG. 6 illustrates an example measured group delay dispersion spectrum of an example multi-pass compression cell.
- FIG. 7 illustrates an example laser system used to test performance of the example multi-pass compression cell.
- FIG. 8 illustrates an autocorrelation measurement of a laser pulse duration with and without the example multi-pass compression cell.
- FIG. 9 illustrates an optical system of the example multi-pass compression cell.
- Described herein are systems including two or more optically reflective surfaces. At least one of the optically reflective surfaces includes a negative or positive group delay dispersion (GDD) coating. Temporal compression or elongation of an optical pulse is achieved by reflecting a beam such that it contacts each of the optically reflective surfaces at least one time.
- GDD group delay dispersion
- the system may be arranged in a self-focusing design and may provide efficient alignment and enhanced compression or pulse stretching performance, and controlling beam divergence. Additionally, the refocusing cavity designs disclosed herein allow for long path lengths without requiring large mirrors.
- Optical pulse stretching and compression may be used in many applications.
- optical pulse stretching and compression may be used in imaging and spectroscopy systems.
- Optical pulse stretching and compression may also be used in telecommunications.
- an optical system 100 includes a first optical element 102 and a second optical element 104 .
- first optical element 102 and a second optical element 104 .
- FIG. 1 illustrates a three-mirror optical system.
- the substrate of the optical components could be composed of various materials such as, for example, fused silica, N-BK7, or metal. A dielectric coating with negative group delay dispersion is applied on these substrates.
- the first optical element 102 has a flat reflective surface 106 .
- the second mirror 104 has a non-flat reflecting surface 108 .
- the reflective surface 108 can have any appropriate geometry.
- the reflective surface 108 may be spherical, aspherical (e.g. toroidal mirrors), cylindrical, acylindrical, or freeform (i.e., having no translational or rotational symmetry).
- the reflective surface 108 may be a metasurface to allow for refocusing of the optical beam and mitigating beam divergence as the beam reflects off of the reflective surfaces 106 and 108 .
- the reflective surfaces 106 , 108 may be, for example, mirrors, filters, windows, or metasurfaces.
- At least one of reflective surface 106 and reflective surface 108 is coated with a GDD coating.
- the GDD is positive such that the system is configured to temporally stretch optical pulses.
- the GDD is negative such that the system is configured to temporally compress optical pulses.
- the optical coating may be composed of dielectric layers that are designed to give an overall negative group delay dispersion that can be used for pulse compression applications. This coating may be applied with various deposition or sputtering techniques. Examples of coating application techniques include electron deposition, ion-assisted deposition, magnetron sputtering, ion beam sputtering, and atomic layer deposition.
- TOD third order dispersion
- one of the optical elements may contain an inlet that allows an optical pulse to pass into the optical system.
- the first optical element 102 may include an inlet 112 .
- the inlet 112 can be, for example, an aperture in the optical element.
- the inlet 112 is an uncoated portion of the optical element or a portion of the optical element that has a coating different than the reflective surface.
- the inlet 112 may be a truncated edge or notch in the first optical element 102 .
- one of the optical elements may contain an outlet 114 . In the illustrated embodiment of FIG. 1 , the inlet 112 and the outlet 114 are the same portion of first optical element 102 .
- the outlet 114 is a second aperture in the first optical element 102 . In other embodiments, the outlet 114 is a portion of the second optical element 104 , as illustrated in FIGS. 3 and 9 . As with the inlet 112 , the outlet 114 can be an aperture, an uncoated portion of the optical element, or a portion of the optical element having a different coating than the reflective surface.
- the beam reflects off of each of the optical elements 102 , 104 multiple times. Each time, the beam may contact a different position on the optical elements 102 , 104 . As a result, no portion of the optical elements 102 , 104 is repeatedly exposed to the high energy beam. This may increase the longevity and reliability of the system. Further, as illustrated in FIG. 9 , the beam may reflect off the optical elements 102 and 104 in a curved path around the reflective surface 108 of the second optical element 104
- the inlet 112 is coupled to hollow core fiber.
- the hollow core fiber provides spectral broadening of the input laser pulses prior to entry into the optical system 100 . This allows for additional broadening of the pulse bandwidth, which will in turn allow the system to achieve shorter pulses.
- the optical system 100 includes various alignment features.
- the alignment features may lead to efficient alignment and enhanced compression or stretching performance due to the increased number of reflections through the reflective surface(s) 106 , 108 .
- Examples of these alignment features include pinholes or slits added for the entrance and exit beam, mirror mounts with mounts that allow for alignment of the optical elements to the beam, and translation or rotational stages that allow for control of the distance between the mirrors.
- the optical system 100 may be used to compress laser pulses with any appropriate pulse duration, including, but not limited to, pulse durations on the femtosecond (fs), picosecond (ps), and nanosecond (ns) scale. Further, the optical system 100 may be used to stretch laser pulses of any appropriate pulse duration, including, but not limited to, pulse durations on the femtosecond and picosecond scale.
- the distance between the optical elements 102 , 104 may be any appropriate distance. In typical applications, the distance between two mirrors can range from 2 inches to greater than 100 inches.
- the distance between the first optical element 102 and the second 104 is adjustable. Adjustment of this distance may lead to a change in the number of times the optical pulse is reflected off of the reflective surfaces 106 , 108 before exiting through the outlet 114 .
- the distance may be adjustable in discrete increments that are predetermined to correlate with specific numbers of reflections of the optical pulse within the optical system 100 .
- the distance may be adjustable manually or automatically.
- the rotation angle between the first optical element 102 and the second optical element 104 is adjustable to a change in the number of times the optical pulse is reflected off of the reflective surfaces 106 , 108 before exiting through the outlet 114 .
- the optical system 100 can be used to compress or stretch pulses of various wavelengths, such as, for example, from ultraviolet to infrared.
- the mirror design may be optimized for a particular wavelength range depending on the wavelength of the incident laser beam.
- the optical system 100 is actively cooled, or thermally-isolated, or inert gas-purged to limit temperature fluctuations of the system and ensure highest beam quality for demanding applications. Additionally, or alternatively, the optical system 100 may be under complete or partial vacuum conditions which may be advantageous for extremely short ultrafast lasers that require vacuum conditions.
- both optical elements 102 , 104 are non-flat.
- both optical elements 102 , 104 can have a concave reflective surface.
- the first optical component 102 can include the inlet 112 and the second optical component 104 can include the outlet 114 . After entering through the inlet 112 , the beam can be reflected between the reflective surfaces 106 , 108 multiple times to compress or expand the beam before exiting through the outlet 114 .
- an optical system may include the optical element 102 having a flat-reflective surface and optical element 104 having a non-flat reflective surface, as illustrated in FIGS. 1 and 9 .
- the optical system may be configured such that the beam reflects off of the optical element 104 and exits the optical element 102 .
- the optical system such as optical system 708 , may be configured such that the beam reflects off of the optical element 102 and exits the optical element 104 .
- the optical system 100 includes a third optical element 116 having a reflective surface 118 .
- the third optical element 116 may be arranged adjacent to the second optical element 104 such that the beam can reflect between the first, second, and third optical elements 102 , 104 , 116 .
- the second 104 and third 116 optical components have different reflective characteristics such that the compression or stretching of the pulse can be tailored as desired.
- the optical systems described herein may be incorporated into, or used with, various other systems.
- the optical systems described herein can be incorporated into a multifocal plane microscopy system.
- the optical systems described herein can replace multi-mirror arrays and, thereby, greatly simplify the alignment.
- the optical systems described herein may also include one or more optical mediums such as, for example, an objective, an acousto-optic modulator, a window, or a lens, positioned between the optical elements 102 and 104 to direct the beam.
- the optical medium may be coated with a GDD coating.
- FIG. 4 illustrates a system 200 including a compressor 201 according to the embodiments described herein (e.g., as shown in FIGS. 1 - 3 and 9 , and as described above).
- the system 200 includes an oscillator 202 (e.g., an ultrafast laser oscillator) to generate an optical pulse.
- the system 200 further includes a stretcher 204 to stretch the pulse duration of the optical pulse.
- the stretcher 204 can include, for example, optical fibers, dispersive prism pairs, diffraction gratings, grisms, or Bragg gratings.
- the system 200 can further include an amplifier 206 to amplify the optical pulse.
- the amplifier 206 can include, for example, laser amplifiers, amplifiers based on optical nonlinearities, or ultrafast amplifiers.
- the system 200 includes a chain of multiple amplifiers of the same or different types.
- the system 200 can further include one or more mirrors 208 for directing the pulse as desired for alignment with the compressor 201 .
- the oscillator 202 generates the pulse and directs it toward the stretcher 204 .
- the pulse After exiting the stretcher 204 , the pulse enters the amplifier 206 for amplifying the magnitude of the pulse.
- the pulse is then directed by the one or more mirrors 208 before entering the compressor 201 .
- the system As shown in FIG. 4 , the system generates a high energy pulse.
- FIG. 5 illustrates a system 300 for dispersion compensation of chirped ultrafast pulses including a compressor 301 according to embodiments described herein.
- the system 300 includes a laser 302 for generating chirped ultrafast pulses.
- the system 300 may further include an optical medium 304 such as, for example, an objective, an acousto-optic modulator, a window, or a lens.
- the system 300 may further include one or more mirrors 306 for directing the pulse as desired for alignment with the compressor 301 .
- the laser 302 is configured to generate a pulse and direct it toward the optical medium 304 . After exiting the optical medium 304 , the pulse is directed by the one or mirrors 306 toward the compressor 301 .
- the compressor 301 may correct all or some of the dispersion caused by the optical medium 304 .
- the optical system 708 of FIG. 9 was used to determine a GDD spectrum of an example dispersive mirror coating applied to the reflective surface 106 and reflective surface 108 .
- incident ultrafast pulses 704 e.g., the example beam illustrated in FIG. 9
- the first optical component 102 has a flat reflective surface
- the second optical component 104 has a concave reflective surface.
- each reflective surface 106 and 108 is coated with a GDD coating of ⁇ 1,000 fs 2 and reflectivity of >99.9% between 1010 nanometers (nm) and 1070 nm.
- a white-light interferometer at 7° angle of incidence (AOI) was used to measure the GDD of the multi-pass compression cell, and produced the measured GDD spectrum illustrated in FIG. 6 .
- an ultrafast laser system 700 as illustrated in FIG. 7 was employed consisting of an ultrafast laser 702 having a Yb:doped fiber laser with 1040 nm center wavelength, 140 fs pulse duration, and 18 W average power at 80 MHz repetition rate to output beam 704 .
- the beam 704 passes through pulse stretcher 706 , in which the 140 fs pulse is stretched to 600 fs.
- the pulse stretcher 706 may be a grating-based stretcher.
- the beam 704 passes through is the pulse compressor 708 , which includes the multi-pass optical system 100 .
- the pulse compressor 708 By changing the distance between the first and second optical components 102 and 104 in the pulse compressor 708 , the number of reflections can be tuned. After multiple bounces, the pulse compressor 708 , via the system 100 , compresses the pulse of the beam 704 back to 140 fs. Having passed through the pulse compressor 708 , the beam 704 may enter and be measured by an autocorrelator 710 .
- FIG. 8 illustrates the autocorrelation measurement of the pulse of the beam 704 without passing through the pulse compressor 708 and with passing through the pulse compressor 708 . The signal of the autocorrelation measurement was fit using a sech 2 function.
- Adding the dispersive mirrors, such as the first and second optical components 102 and 104 , to a multi-pass cell configuration advantageously creates a compact, tunable, and alignment-free ultrafast compressor. Further, by refocusing the beam with one or more reflections off the second optical component, the divergence of the beam may be mitigated or reduced.
- the careful optical design of the systems described herein obtain high-quality beams. As such, these systems can be used in CPA laser systems or for dispersion compensation in any ultrafast laser system that requires careful control and fine-tuning of the pulse duration.
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Lasers (AREA)
Abstract
An optical system includes a first optical component including a reflective surface opposing a second optical component; and the second optical component including a non-flat reflective surface opposing the first optical component, wherein a portion of the first optical component allows an optical pulse to pass through the first optical component and reflect off the non-flat reflective surface, an arrangement of the first optical component and the second optical component defines a self-focusing cavity that refocuses the optical pulse and controls divergence of the optical pulse, and at least one of the reflective surface and the non-flat reflective surface is coated with a group delay dispersion (GDD) coating.
Description
- This application claims the benefit of U.S. Provisional Patent Application No. 62/914,049 filed Oct. 11, 2019; and U.S. patent application Ser. No. 17/068,117 filed Oct. 12, 2020, which are all hereby incorporated by reference for all purposes as if fully set forth herein.
- Stretching or compressing optical pulses can be useful in a variety of applications. One method of achieving stretching or compressing of pulses is the use of a long dispersive optical fiber to guide and propagate the light pulse. Because of the chromatic dispersion of the optical fiber, different frequency components experience different refractive indices and travel at different speeds along the fiber. This separates different frequency components in time. Optical fibers can also be used to compress pulses. This may be useful in telecommunications and in optical microscopy and imaging. However, the amount of stretching or compressing is limited by the length of the fiber. The acceptable wavelengths may also be restricted based on the material of the fiber. In addition, the pulses may experience linear dispersion that may distort the pulses.
- The present disclosure relates generally to optical systems, and more particularly, optical systems for temporal compression or stretching of optical pulses.
- In an embodiment, an optical system includes a first optical component including a reflective surface opposing a second optical component; and the second optical component including a non-flat reflective surface opposing the first optical component, wherein a portion of the first optical component allows an optical pulse to pass through the first optical component and reflect off the non-flat reflective surface, an arrangement of the first optical component and the second optical component defines a self-focusing cavity that refocuses the optical pulse and controls divergence of the optical pulse, and at least one of the reflective surface and the non-flat reflective surface is coated with a group delay dispersion (GDD) coating.
- In as aspect, a distance and a rotation angle between the first optical component and the second optical component are adjustable to change a number of times the optical pulse reflects off the reflective surface and the non-flat reflective surface before exiting the optical system without changing optical alignment.
- In an aspect, the reflective surface includes a flat reflective surface, and the portion of the first optical component allows the optical pulse reflected off the second optical component to exit the optical system.
- In an aspect, the reflective surface includes a non-flat reflective surface to reflect the optical pulse from a portion of the second optical component to another portion of the second optical component, and the other portion of the second optical component allows the optical pulse to exit the optical system.
- In an aspect, the portion of the first optical component comprises a truncated edge, notch, or hole and is coupled to a hollow core fiber.
- In an aspect, the GDD coating comprises a negative GDD coating that temporally compresses the optical pulse passing through the optical system.
- In an aspect, a GDD of at least one of the reflective surface of the first optical component and the non-flat reflective surface of the second optical component is less than −20 femtoseconds2 (fs2).
- In an aspect, the GDD coating includes a positive GDD coating that stretches the optical pulse passing through the optical system.
- In an aspect, a GDD of at least one of the reflective surface of the first optical component and the non-flat reflective surface of the second optical component is greater than 20 femtoseconds2 (fs2).
- In an aspect, the optical system compresses or stretches the optical pulse based on a type of wavelength.
- In an aspect, the portion of the first optical component is an uncoated portion of the first optical component.
- In an aspect, wherein either the first optical component or the second optical component allows the optical pulse to exit the optical system.
- In an aspect, the reflective surface comprises a flat reflective surface.
- In an aspect, the reflective surface comprises a non-flat reflective surface.
- The optical system can further include a light emitting device that generates the optical pulse.
- In another embodiment, an optical system includes a first optical component including a reflective surface opposing a second optical component, and the second optical component including a non-flat reflective surface opposing the first optical component, wherein a portion of the first optical component allows an optical pulse to pass through the first optical component and reflect off the non-flat reflective surface, a distance and a rotation angle between the first optical component and the second optical component are adjustable to change a number of times the optical pulse reflects off the reflective surface and the non-flat reflective surface before exiting the optical system without changing optical alignment, the distance between the first optical component and the second optical component is adjustable in discrete increments that are predetermined to correlate with specific numbers of reflections of the optical pulse within the optical system while controlling the divergence of the optical pulse, and the rotation angle between the first optical component and the second optical component is adjustable to change the number of times the optical pulse is reflected off the reflective surface and the non-flat reflective surface while controlling the divergence of the optical pulse.
- The optical system can further include a hollow core fiber coupled to the portion of the first optical component.
- The optical system can further include further include a light emitting device that generates the optical pulse, wherein the light emitting device comprises an ultrafast laser oscillator or amplifier.
- In an aspect, either the first optical component or the second optical component allows the optical pulse to exit the optical system.
- In an aspect, the first optical component or the second optical component is coated with a group delay dispersion (GDD) coating.
- The foregoing and other objects, features, and advantages of the disclosure will be apparent from the following more particular descriptions of the embodiments as illustrated in the accompanying drawings.
- The features of the embodiments described herein will be more fully disclosed in the following detailed description, which is to be considered together with the accompanying drawings wherein like numbers refer to like parts and further wherein:
-
FIG. 1 shows an optical system according to one embodiment described herein. -
FIG. 2 shows an optical system according to another embodiment described herein. -
FIG. 3 shows an optical system according to another embodiment described herein. -
FIG. 4 illustrates a chirped pulse modification system including a compressor system according to embodiments described herein. -
FIG. 5 illustrates a system for dispersion compensation of chirped ultrafast pulses including a compressor according to embodiments described herein. -
FIG. 6 illustrates an example measured group delay dispersion spectrum of an example multi-pass compression cell. -
FIG. 7 illustrates an example laser system used to test performance of the example multi-pass compression cell. -
FIG. 8 illustrates an autocorrelation measurement of a laser pulse duration with and without the example multi-pass compression cell. -
FIG. 9 illustrates an optical system of the example multi-pass compression cell. - The following description is provided as an enabling teaching of a representative set of examples. Many changes can be made to the embodiments described herein while still obtaining beneficial results. Some of the desired benefits discussed below can be obtained by selecting some of the features or steps discussed herein without utilizing other features or steps. Accordingly, many modifications and adaptations, as well as subsets of the features and steps described herein are possible and can even be desirable in certain circumstances. Thus, the following description is provided as illustrative and is not limiting.
- This description of the embodiments is intended to be read in connection with the accompanying drawings, which are to be considered part of the entire written description. The drawing figures are not necessarily to scale and certain features may be shown exaggerated in scale or in somewhat schematic form in the interest of clarity and conciseness. In the description, relative terms such as “horizontal,” “vertical,” “up,” “down,” “top” and “bottom” as well as derivatives thereof (e.g., “horizontally,” “downwardly,” “upwardly,” etc.) should be construed to refer to the orientation as then described or as shown in the drawing figure under discussion. These relative terms are for convenience of description and normally are not intended to require a particular orientation. Terms including “inwardly” versus “outwardly,” “longitudinal” versus “lateral” and the like are to be interpreted relative to one another or relative to an axis of elongation, or an axis or center of rotation, as appropriate. Terms concerning attachments, coupling and the like, such as “connected” and “interconnected,” refer to a relationship wherein structures are secured or attached to one another either directly or indirectly through intervening structures, as well as both movable or rigid attachments or relationships, unless expressly described otherwise. The term “operatively connected” or “operably connected” is such an attachment, coupling or connection that allows the pertinent structures to operate as intended by virtue of that relationship. Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by anyone of ordinary skill level in the field to which this invention belongs.
- As used herein, use of a singular article such as “a,” “an” and “the” is not intended to exclude pluralities of the article's object unless the context clearly and unambiguously dictates otherwise.
- Described herein are systems including two or more optically reflective surfaces. At least one of the optically reflective surfaces includes a negative or positive group delay dispersion (GDD) coating. Temporal compression or elongation of an optical pulse is achieved by reflecting a beam such that it contacts each of the optically reflective surfaces at least one time. The system may be arranged in a self-focusing design and may provide efficient alignment and enhanced compression or pulse stretching performance, and controlling beam divergence. Additionally, the refocusing cavity designs disclosed herein allow for long path lengths without requiring large mirrors.
- Optical pulse stretching and compression may be used in many applications. For example, optical pulse stretching and compression may be used in imaging and spectroscopy systems. Optical pulse stretching and compression may also be used in telecommunications.
- As shown in
FIG. 1 , in one embodiment, anoptical system 100 includes a firstoptical element 102 and a secondoptical element 104. Although only two optical elements are illustrated inFIG. 1 , any number of optical elements can be used. For example,FIG. 2 illustrates a three-mirror optical system. The substrate of the optical components could be composed of various materials such as, for example, fused silica, N-BK7, or metal. A dielectric coating with negative group delay dispersion is applied on these substrates. - In the illustrated embodiment, the first
optical element 102 has a flatreflective surface 106. Thesecond mirror 104 has anon-flat reflecting surface 108. Thereflective surface 108 can have any appropriate geometry. For example, thereflective surface 108 may be spherical, aspherical (e.g. toroidal mirrors), cylindrical, acylindrical, or freeform (i.e., having no translational or rotational symmetry). In addition, thereflective surface 108 may be a metasurface to allow for refocusing of the optical beam and mitigating beam divergence as the beam reflects off of thereflective surfaces FIG. 3 . Thereflective surfaces - At least one of
reflective surface 106 andreflective surface 108 is coated with a GDD coating. In various embodiments, the GDD is positive such that the system is configured to temporally stretch optical pulses. In various other embodiments, the GDD is negative such that the system is configured to temporally compress optical pulses. The optical coating may be composed of dielectric layers that are designed to give an overall negative group delay dispersion that can be used for pulse compression applications. This coating may be applied with various deposition or sputtering techniques. Examples of coating application techniques include electron deposition, ion-assisted deposition, magnetron sputtering, ion beam sputtering, and atomic layer deposition. - In one embodiment configured for stretching of optical pulses, the GDD of at least one of the
reflective surfaces reflective surfaces - As shown in
FIG. 1 , one of the optical elements may contain an inlet that allows an optical pulse to pass into the optical system. For example, as shown, the firstoptical element 102 may include aninlet 112. Theinlet 112 can be, for example, an aperture in the optical element. In other embodiments, theinlet 112 is an uncoated portion of the optical element or a portion of the optical element that has a coating different than the reflective surface. In other embodiments, theinlet 112 may be a truncated edge or notch in the firstoptical element 102. In addition, one of the optical elements may contain anoutlet 114. In the illustrated embodiment ofFIG. 1 , theinlet 112 and theoutlet 114 are the same portion of firstoptical element 102. In other embodiments, theoutlet 114 is a second aperture in the firstoptical element 102. In other embodiments, theoutlet 114 is a portion of the secondoptical element 104, as illustrated inFIGS. 3 and 9 . As with theinlet 112, theoutlet 114 can be an aperture, an uncoated portion of the optical element, or a portion of the optical element having a different coating than the reflective surface. - In various embodiments, the beam reflects off of each of the
optical elements optical elements optical elements FIG. 9 , the beam may reflect off theoptical elements reflective surface 108 of the secondoptical element 104 - In one embodiment, the
inlet 112 is coupled to hollow core fiber. The hollow core fiber provides spectral broadening of the input laser pulses prior to entry into theoptical system 100. This allows for additional broadening of the pulse bandwidth, which will in turn allow the system to achieve shorter pulses. - In various embodiments, the
optical system 100 includes various alignment features. The alignment features may lead to efficient alignment and enhanced compression or stretching performance due to the increased number of reflections through the reflective surface(s) 106, 108. Examples of these alignment features include pinholes or slits added for the entrance and exit beam, mirror mounts with mounts that allow for alignment of the optical elements to the beam, and translation or rotational stages that allow for control of the distance between the mirrors. - The
optical system 100 may be used to compress laser pulses with any appropriate pulse duration, including, but not limited to, pulse durations on the femtosecond (fs), picosecond (ps), and nanosecond (ns) scale. Further, theoptical system 100 may be used to stretch laser pulses of any appropriate pulse duration, including, but not limited to, pulse durations on the femtosecond and picosecond scale. - The distance between the
optical elements - In one embodiment, the distance between the first
optical element 102 and the second 104 is adjustable. Adjustment of this distance may lead to a change in the number of times the optical pulse is reflected off of thereflective surfaces outlet 114. The distance may be adjustable in discrete increments that are predetermined to correlate with specific numbers of reflections of the optical pulse within theoptical system 100. The distance may be adjustable manually or automatically. Moreover, the rotation angle between the firstoptical element 102 and the secondoptical element 104 is adjustable to a change in the number of times the optical pulse is reflected off of thereflective surfaces outlet 114. - The
optical system 100 can be used to compress or stretch pulses of various wavelengths, such as, for example, from ultraviolet to infrared. The mirror design may be optimized for a particular wavelength range depending on the wavelength of the incident laser beam. - In one embodiment, the
optical system 100 is actively cooled, or thermally-isolated, or inert gas-purged to limit temperature fluctuations of the system and ensure highest beam quality for demanding applications. Additionally, or alternatively, theoptical system 100 may be under complete or partial vacuum conditions which may be advantageous for extremely short ultrafast lasers that require vacuum conditions. - In another embodiment, as shown in
FIG. 3 , bothoptical elements optical elements FIG. 3 , the firstoptical component 102 can include theinlet 112 and the secondoptical component 104 can include theoutlet 114. After entering through theinlet 112, the beam can be reflected between thereflective surfaces outlet 114. In other embodiments, an optical system may include theoptical element 102 having a flat-reflective surface andoptical element 104 having a non-flat reflective surface, as illustrated inFIGS. 1 and 9 . In some cases, the optical system may be configured such that the beam reflects off of theoptical element 104 and exits theoptical element 102. In some other cases, the optical system, such asoptical system 708, may be configured such that the beam reflects off of theoptical element 102 and exits theoptical element 104. - In the embodiment shown in
FIG. 2 , theoptical system 100 includes a thirdoptical element 116 having areflective surface 118. The thirdoptical element 116 may be arranged adjacent to the secondoptical element 104 such that the beam can reflect between the first, second, and thirdoptical elements - The optical systems described herein may be incorporated into, or used with, various other systems. For example, the optical systems described herein can be incorporated into a multifocal plane microscopy system. The optical systems described herein can replace multi-mirror arrays and, thereby, greatly simplify the alignment. The optical systems described herein may also include one or more optical mediums such as, for example, an objective, an acousto-optic modulator, a window, or a lens, positioned between the
optical elements -
FIG. 4 illustrates asystem 200 including acompressor 201 according to the embodiments described herein (e.g., as shown inFIGS. 1-3 and 9 , and as described above). Thesystem 200 includes an oscillator 202 (e.g., an ultrafast laser oscillator) to generate an optical pulse. Thesystem 200 further includes astretcher 204 to stretch the pulse duration of the optical pulse. Thestretcher 204 can include, for example, optical fibers, dispersive prism pairs, diffraction gratings, grisms, or Bragg gratings. Thesystem 200 can further include anamplifier 206 to amplify the optical pulse. Theamplifier 206 can include, for example, laser amplifiers, amplifiers based on optical nonlinearities, or ultrafast amplifiers. In some embodiments, thesystem 200 includes a chain of multiple amplifiers of the same or different types. Thesystem 200 can further include one ormore mirrors 208 for directing the pulse as desired for alignment with thecompressor 201. - As shown, the
oscillator 202 generates the pulse and directs it toward thestretcher 204. After exiting thestretcher 204, the pulse enters theamplifier 206 for amplifying the magnitude of the pulse. The pulse is then directed by the one ormore mirrors 208 before entering thecompressor 201. As shown inFIG. 4 , the system generates a high energy pulse. -
FIG. 5 illustrates asystem 300 for dispersion compensation of chirped ultrafast pulses including acompressor 301 according to embodiments described herein. Thesystem 300 includes alaser 302 for generating chirped ultrafast pulses. Thesystem 300 may further include anoptical medium 304 such as, for example, an objective, an acousto-optic modulator, a window, or a lens. Thesystem 300 may further include one ormore mirrors 306 for directing the pulse as desired for alignment with thecompressor 301. - The
laser 302 is configured to generate a pulse and direct it toward theoptical medium 304. After exiting theoptical medium 304, the pulse is directed by the one or mirrors 306 toward thecompressor 301. Thecompressor 301 may correct all or some of the dispersion caused by theoptical medium 304. - In an example, the
optical system 708 ofFIG. 9 was used to determine a GDD spectrum of an example dispersive mirror coating applied to thereflective surface 106 andreflective surface 108. In this example, incident ultrafast pulses 704 (e.g., the example beam illustrated inFIG. 9 ) enter through theinlet 112 of the firstoptical component 102, reflect of thereflective surfaces outlet 114 of the secondoptical component 104. In this example, the firstoptical component 102 has a flat reflective surface, and the secondoptical component 104 has a concave reflective surface. To create the multi-pass compression cell, eachreflective surface FIG. 6 . - In order to test the compression performance of example optical system 708 (i.e., the pulse compressor), an
ultrafast laser system 700 as illustrated inFIG. 7 was employed consisting of anultrafast laser 702 having a Yb:doped fiber laser with 1040 nm center wavelength, 140 fs pulse duration, and 18 W average power at 80 MHz repetition rate tooutput beam 704. Thebeam 704 passes throughpulse stretcher 706, in which the 140 fs pulse is stretched to 600 fs. In an example, thepulse stretcher 706 may be a grating-based stretcher. Thebeam 704 passes through is thepulse compressor 708, which includes the multi-passoptical system 100. By changing the distance between the first and secondoptical components pulse compressor 708, the number of reflections can be tuned. After multiple bounces, thepulse compressor 708, via thesystem 100, compresses the pulse of thebeam 704 back to 140 fs. Having passed through thepulse compressor 708, thebeam 704 may enter and be measured by anautocorrelator 710.FIG. 8 illustrates the autocorrelation measurement of the pulse of thebeam 704 without passing through thepulse compressor 708 and with passing through thepulse compressor 708. The signal of the autocorrelation measurement was fit using a sech2 function. - Adding the dispersive mirrors, such as the first and second
optical components - While the foregoing description and drawings represent preferred or exemplary embodiments of the present disclosure, it will be understood that various additions, modifications and substitutions may be made therein without departing from the spirit and scope and range of equivalents of the embodiments described herein. In particular, it will be clear to those skilled in the art that the embodiments disclosed herein may be embodied in other forms, structures, arrangements, proportions, sizes, and with other elements, materials, and components, without departing from the spirit or essential characteristics thereof.
Claims (20)
1. An optical system comprising:
a first optical component including a reflective surface opposing a second optical component; and
the second optical component including a non-flat reflective surface opposing the first optical component, wherein
a portion of the first optical component allows an optical pulse to pass through the first optical component and reflect off the non-flat reflective surface,
an arrangement of the first optical component and the second optical component defines a self-focusing cavity that refocuses the optical pulse and controls divergence of the optical pulse, and
at least one of the reflective surface and the non-flat reflective surface is coated with a group delay dispersion (GDD) coating.
2. The optical system of claim 1 , wherein a distance and a rotation angle between the first optical component and the second optical component are adjustable to change a number of times the optical pulse reflects off the reflective surface and the non-flat reflective surface before exiting the optical system without changing optical alignment.
3. The optical system of claim 1 , wherein:
the reflective surface includes a flat reflective surface, and
the portion of the first optical component allows the optical pulse reflected off the second optical component to exit the optical system.
4. The optical system of claim 1 , wherein:
the reflective surface includes a non-flat reflective surface to reflect the optical pulse from a portion of the second optical component to another portion of the second optical component, and
the other portion of the second optical component allows the optical pulse to exit the optical system.
5. The optical system of claim 1 , wherein the portion of the first optical component comprises a truncated edge, notch, or hole and is coupled to a hollow core fiber.
6. The optical system of claim 1 , wherein the GDD coating comprises a negative GDD coating that temporally compresses the optical pulse passing through the optical system.
7. The optical system of claim 6 , wherein a GDD of at least one of the reflective surface of the first optical component and the non-flat reflective surface of the second optical component is less than −20 femtoseconds2 (fs2).
8. The optical system of claim 1 , wherein the GDD coating includes a positive GDD coating that stretches the optical pulse passing through the optical system.
9. The optical system of claim 8 , wherein a GDD of at least one of the reflective surface of the first optical component and the non-flat reflective surface of the second optical component is greater than 20 femtoseconds2 (fs2).
10. The optical system of claim 1 , wherein the optical system compresses or stretches the optical pulse based on a type of wavelength.
11. The optical system of claim 1 , wherein the portion of the first optical component is an uncoated portion of the first optical component.
12. The optical system of claim 1 , wherein either the first optical component or the second optical component allows the optical pulse to exit the optical system.
13. The optical system of claim 1 , wherein the reflective surface comprises a flat reflective surface.
14. The optical system of claim 1 , wherein the reflective surface comprises a non-flat reflective surface.
15. The optical system of claim 1 , further comprising a light emitting device that generates the optical pulse.
16. An optical system comprising:
a first optical component including a reflective surface opposing a second optical component, and
the second optical component including a non-flat reflective surface opposing the first optical component, wherein
a portion of the first optical component allows an optical pulse to pass through the first optical component and reflect off the non-flat reflective surface,
a distance and a rotation angle between the first optical component and the second optical component are adjustable to change a number of times the optical pulse reflects off the reflective surface and the non-flat reflective surface before exiting the optical system without changing optical alignment,
the distance between the first optical component and the second optical component is adjustable in discrete increments that are predetermined to correlate with specific numbers of reflections of the optical pulse within the optical system while controlling the divergence of the optical pulse, and
the rotation angle between the first optical component and the second optical component is adjustable to change the number of times the optical pulse is reflected off the reflective surface and the non-flat reflective surface while controlling the divergence of the optical pulse.
17. The optical system of claim 16 , further comprising a hollow core fiber coupled to the portion of the first optical component.
18. The optical system of claim 16 , further comprising a light emitting device that generates the optical pulse, wherein the light emitting device comprises an ultrafast laser oscillator or amplifier.
19. The optical system of claim 16 , wherein either the first optical component or the second optical component allows the optical pulse to exit the optical system.
20. The optical system of claim 16 , wherein the first optical component or the second optical component is coated with a group delay dispersion (GDD) coating.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US17/896,458 US20220404543A1 (en) | 2019-10-11 | 2022-08-26 | Devices, systems, and methods for temporal compression or stretching of optical pulses |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201962914049P | 2019-10-11 | 2019-10-11 | |
US17/068,117 US11428863B2 (en) | 2019-10-11 | 2020-10-12 | Devices, systems, and methods for temporal compression or stretching of optical pulses |
US17/896,458 US20220404543A1 (en) | 2019-10-11 | 2022-08-26 | Devices, systems, and methods for temporal compression or stretching of optical pulses |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US17/068,117 Continuation US11428863B2 (en) | 2019-10-11 | 2020-10-12 | Devices, systems, and methods for temporal compression or stretching of optical pulses |
Publications (1)
Publication Number | Publication Date |
---|---|
US20220404543A1 true US20220404543A1 (en) | 2022-12-22 |
Family
ID=75383965
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US17/068,117 Active 2040-10-24 US11428863B2 (en) | 2019-10-11 | 2020-10-12 | Devices, systems, and methods for temporal compression or stretching of optical pulses |
US17/896,458 Abandoned US20220404543A1 (en) | 2019-10-11 | 2022-08-26 | Devices, systems, and methods for temporal compression or stretching of optical pulses |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US17/068,117 Active 2040-10-24 US11428863B2 (en) | 2019-10-11 | 2020-10-12 | Devices, systems, and methods for temporal compression or stretching of optical pulses |
Country Status (1)
Country | Link |
---|---|
US (2) | US11428863B2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11428863B2 (en) * | 2019-10-11 | 2022-08-30 | Edmund Optics, Inc. | Devices, systems, and methods for temporal compression or stretching of optical pulses |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20160070041A1 (en) * | 2014-09-10 | 2016-03-10 | Schott Ag | Dielectric mirror for high-power laser pulses |
US20160149368A1 (en) * | 2014-11-26 | 2016-05-26 | Electronics And Telecommunications Research Institute | Pulse width stretcher and chirped pulse amplifier including the same |
US20170125964A1 (en) * | 2014-05-15 | 2017-05-04 | Fraunhofer-Gesellschaft Zur Foerderung Der Angewandten Forschung E.V. | Method and arrangement for spectral broadening of laser pulses for non-linear pulse compression |
US11428863B2 (en) * | 2019-10-11 | 2022-08-30 | Edmund Optics, Inc. | Devices, systems, and methods for temporal compression or stretching of optical pulses |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5960016A (en) * | 1997-06-05 | 1999-09-28 | The Regents Of The University Of California | Aberration-free, all-reflective laser pulse stretcher |
US8953651B2 (en) * | 2010-02-24 | 2015-02-10 | Alcon Lensx, Inc. | High power femtosecond laser with repetition rate adjustable according to scanning speed |
US10211587B2 (en) * | 2015-03-31 | 2019-02-19 | Versitech Limited | Spatial chirped cavity for temporally stretching/compressing optical pulses |
-
2020
- 2020-10-12 US US17/068,117 patent/US11428863B2/en active Active
-
2022
- 2022-08-26 US US17/896,458 patent/US20220404543A1/en not_active Abandoned
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170125964A1 (en) * | 2014-05-15 | 2017-05-04 | Fraunhofer-Gesellschaft Zur Foerderung Der Angewandten Forschung E.V. | Method and arrangement for spectral broadening of laser pulses for non-linear pulse compression |
US20160070041A1 (en) * | 2014-09-10 | 2016-03-10 | Schott Ag | Dielectric mirror for high-power laser pulses |
US20160149368A1 (en) * | 2014-11-26 | 2016-05-26 | Electronics And Telecommunications Research Institute | Pulse width stretcher and chirped pulse amplifier including the same |
US11428863B2 (en) * | 2019-10-11 | 2022-08-30 | Edmund Optics, Inc. | Devices, systems, and methods for temporal compression or stretching of optical pulses |
Also Published As
Publication number | Publication date |
---|---|
US20210109280A1 (en) | 2021-04-15 |
US11428863B2 (en) | 2022-08-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8619357B2 (en) | Static phase mask for high-order spectral phase control in a hybrid chirped pulse amplifier system | |
US7199924B1 (en) | Apparatus and method for spectral-beam combining of high-power fiber lasers | |
US7233442B1 (en) | Method and apparatus for spectral-beam combining of high-power fiber lasers | |
JPH1068889A (en) | Device for coupling short pulse laser beam in optical path of microscope and method therefor | |
US9472922B2 (en) | Wavelength-tunable light source | |
US8369017B2 (en) | Optical pulse shaping method and apparatus | |
US9158117B2 (en) | Spectra shaping device for chirped pulse amplification | |
CN101101427A (en) | Double cladding large mode field area Yb-doped photon crystal optical fiber femtosecond laser | |
US5960016A (en) | Aberration-free, all-reflective laser pulse stretcher | |
US10857031B2 (en) | Dispersion control using chirped mirrors in femtosecond laser system for ophthalmic application | |
GB2473144A (en) | Spectra shaping scheme for chirped pluse amplication | |
US20220404543A1 (en) | Devices, systems, and methods for temporal compression or stretching of optical pulses | |
US11846866B2 (en) | Apparatus for the spectral broadening of laser pulses and optical system | |
US20090034077A1 (en) | Grating with angled output prism face for providing wavelength-dependent group delay | |
CN101859974A (en) | Narrow linewidth thulium-doped fiber laser | |
Holgado et al. | Tunable high-harmonic generation by chromatic focusing of few-cycle laser pulses | |
Nenchev et al. | Two-wavelength dye-laser operation using a reflecting Fizeau interferometer | |
CN115084978A (en) | Multi-pass laser spectrum broadening optical system and method | |
CN213184959U (en) | Multi-pass laser pulse widening device | |
CN115769139A (en) | Device for spectral broadening of laser pulses and laser system | |
TWI728999B (en) | Spatial chirped cavity for temporally stretching/compressing optical pulses | |
US20230170660A1 (en) | Laser system for nonlinear pulse compression and grating compressor | |
US20200388977A1 (en) | Device and method to adjust tunable laser pulses | |
Cross | Steps towards a tunable vacuum ultraviolet light source for TR-ARPES | |
US20230335964A1 (en) | Short pulse laser system, and method for generating laser pulses |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: EDMUND OPTICS, INC., NEW JERSEY Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:KARAM, TONY;SANDSTROEM, LARS;CARLIE, NATHAN;SIGNING DATES FROM 20200117 TO 20200120;REEL/FRAME:060912/0773 |
|
STPP | Information on status: patent application and granting procedure in general |
Free format text: DOCKETED NEW CASE - READY FOR EXAMINATION |
|
STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |