DEVICE FOR MEASURING TRANSMITTANCE CURVE OF FABRY-PEROT USING FREQUENCY COMB LIGHT SOURCE AND METHOD USING THE SAME
20230152153 · 2023-05-18
Inventors
- Yingjian WANG (Hefei, Anhui, CN)
- Yufei CHU (Hefei, Anhui, CN)
- Dong LIU (Hefei, Anhui, CN)
- Decheng WU (Hefei, Anhui, CN)
- Zhenzhu WANG (Hefei, Anhui, CN)
- Kunming XING (Hefei, Anhui, CN)
- Zhiqiang KUANG (Hefei, Anhui, CN)
- Bangxin WANG (Hefei, Anhui, CN)
- Zhiqing ZHONG (Hefei, Anhui, CN)
- Aiyuan FAN (Hefei, Anhui, CN)
- Chenbo XIE (Hefei, Anhui, CN)
Cpc classification
G01M11/0285
PHYSICS
G01J3/027
PHYSICS
G01J3/0208
PHYSICS
G01J3/10
PHYSICS
G01J3/0297
PHYSICS
International classification
Abstract
This application relates to a device for measuring a transmittance curve of an Fabry-Perot using a frequency comb light source and a method using the same. The device includes the following components sequentially arranged in an optical path: a single frequency pulse laser generating single frequency pulse laser; a frequency comb laser converting received single frequency pulse laser into frequency comb laser; and an Fabry-Perot to be detected receiving laser output from the frequency comb laser; where the device further includes a first receiving unit receiving laser from an output end of the frequency comb laser and performing component and spectrum analysis, and a second receiving unit receiving laser from an output end of the Fabry-Perot to be detected and performing component and spectrum analysis.
Claims
1. A device for measuring a transmittance curve of an Fabry-Perot using a frequency comb light source, comprising the following components sequentially arranged in an optical path: a single frequency pulse laser generating single frequency pulse laser; a frequency comb laser converting received single frequency pulse laser into frequency comb laser; and an Fabry-Perot to be detected receiving laser output from the frequency comb laser; wherein the device further comprises a first receiving unit receiving laser from an output end of the frequency comb laser and performing component and spectrum analysis, and a second receiving unit receiving laser from an output end of the Fabry-Perot to be detected and performing component and spectrum analysis.
2. The device for measuring the transmittance curve of the Fabry-Perot by using the frequency comb light source according to claim 1, further comprising a first beam splitter splitting the frequency comb laser into a first output of laser and a second output of laser, wherein the first output of laser is emitted into the first receiving unit and the second output of laser is emitted into the Fabry-Perot to be detected.
3. The device for measuring the transmittance curve of the Fabry-Perot by using the frequency comb light source according to claim 2, wherein the first receiving unit comprises a second beam splitter receiving laser output from the first beam splitter, and two laser beams split by the second beam splitter are respectively emitted into a first detector of the first receiving unit and a first spectrometer of the first receiving unit.
4. The device for measuring the transmittance curve of the Fabry-Perot by using the frequency comb light source according to claim 3, wherein the second receiving unit comprises a third beam splitter, a second detector, and a second spectrometer, and two laser beams split by the third beam splitter are respectively emitted to the second detector and the second spectrometer.
5. The device for measuring the transmittance curve of the Fabry-Perot by using the frequency comb light source according to claim 1, further comprising a collimator provided with an optical aperture and arranged between the first beam splitter and the Fabry-Perot to be detected.
6. The device for measuring the transmittance curve of the Fabry-Perot by using the frequency comb light source according to claim 1, wherein the Fabry-Perot to be detected is an air gap etalon.
7. The device for measuring the transmittance curve of the Fabry-Perot by using the frequency comb light source according to claim 1, wherein the Fabry-Perot to be detected is a solid etalon.
8. The device for measuring the transmittance curve of the Fabry-Perot by using the frequency comb light source according to claim 7, further comprising a computer, wherein a signal input end of the computer is connected to an output end of the first receiving unit and an output end of the second receiving unit, respectively, and a control end of the single frequency pulse laser is connected to a signal output end of the computer.
9. A method using a device for measuring a transmittance curve of an Fabry-Perot by using a frequency comb light source, the device comprising: a single frequency pulse laser generating single frequency pulse laser; a frequency comb laser converting received single frequency pulse laser into frequency comb laser; and an Fabry-Perot to be detected receiving laser output from the frequency comb laser; wherein the device further comprises a first receiving unit receiving laser from an output end of the frequency comb laser and performing component and spectrum analysis, and a second receiving unit receiving laser from an output end of the Fabry-Perot to be detected and performing component and spectrum analysis; wherein the method comprises the following operations: obtaining the required single frequency pulse laser and the frequency comb laser with a set type, and assembling the device; transforming, by the frequency comb laser, the single frequency pulse laser output from the single frequency pulse laser into lasers with different frequency components, passing, by the lasers with different frequency components, through the Fabry-Perot, and measuring, by the detector and the spectrometer, transmittances corresponding to the different frequency components at one time; and performing, by the computer, polynomial fitting on transmittances corresponding to all frequency components to obtain the transmittance curve.
10. The method according to claim 9, wherein specific operations of measuring transmittances corresponding to the different frequency components are: removing the Fabry-Perot in the device, obtaining energy in the first detector of the first receiving unit and the second detector of the second receiving unit, and obtaining an energy ratio N1=energy value of the first detector/energy value of the second detector, wherein N1 is configured as a calibration coefficient; and after calibration, comparing a relative energy change of a frequency component measured by the first spectrometer of the first receiving unit and a frequency component measured by the second spectrometer of the second receiving unit, and multiplying the relative energy change by the calibration coefficient to obtain a transmittance of a corresponding frequency.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0032]
[0033]
[0034]
[0035]
[0036]
[0037] The meanings of the reference numerals in the figures are as follows:
[0038] 1—single frequency pulse laser 2—frequency comb laser 3—FP
[0039] 41—first beam splitter 42—second beam splitter 43—third beam splitter 5—collimator
[0040] 61—first detector 62—first spectrometer 71—second detector 72—second spectrometer
DETAILED DESCRIPTION OF THE EMBODIMENTS
Embodiment 1
[0041] As shown in
[0042] a single frequency pulse laser 1 generating single frequency pulse laser;
[0043] a frequency comb laser 2 converting received single frequency pulse laser into frequency comb laser; and
[0044] an FP 3 to be detected receiving laser output from the frequency comb laser;
[0045] the device further includes a first beam splitter 41, a first receiving unit, and a second receiving unit. The first receiving unit is configured to receive laser from an output end of the frequency comb laser 2 and perform component and spectrum analysis. The second receiving unit is configured to receive laser from an output end of the FP 3 to be detected and perform component and spectrum analysis. The first beam splitter 41 splits the frequency comb laser into a first output of laser and a second output of laser. The first output of laser is emitted into the first receiving unit and the second output of laser is emitted into the FP 3 to be detected. The first receiving unit includes a second beam splitter 42, a first detector 61, and a first spectrometer 62. The second beam splitter 42 splits the light emitted into the first receiving unit into two beams and transmits them to the first detector respectively 61 and the first spectrometer 62, respectively. The second receiving unit includes a third beam splitter 43, a second detector 71, and a second spectrometer 72. The third beam splitter 43 splits the light emitted into the second receiving unit into two beams and transmits them to the second detector 71 and the second spectrometer 72, respectively.
[0046] The single frequency pulse laser 1 outputs multiple frequency components at equal intervals through the frequency comb laser 2, and the multiple frequency components pass through the first beam splitter 41 to be split into a beam A1 and a beam A2. The second beam splitter 42 splits the beam A2 into a beam B1 and a beam B2, and then detects a frequency component of the beam B2 by the first spectrometer 62, and the first detector 61 receives energy of the beam B1. The beam A1 passes through the FP 3 etalon, and the beam is split into a beam C1 and a beam C2 by the third beam splitter 43, and then a frequency component of the beam C2 is detected by the second spectrometer 72, and the beam C1 is received by the second detector 71 to measure its energy. The energy changes of the first detector 61 and the second detector 71 are used for calibration, and then by comparing the relative energy changes of the corresponding frequency components before and after the FP 3, the transmittance of the corresponding frequency may be obtained. The transmission curve may be obtained by fitting each frequency component by a polynomial.
[0047] The device further includes a collimator 5 provided with an optical aperture and arranged between the first beam splitter 41 and the FP 3 to be detected, so as to adjust the light beam emitted to the FP 3 to be detected.
[0048] Specifically, the FP 3 to be detected is an air gap etalon or a solid etalon.
[0049] The device further includes a computer (not shown), where a signal input end of the computer is connected to an output end of the first receiving unit and an output end of the second receiving unit and a control end of the single frequency pulse laser 1 is connected to a signal output end of the computer. The computer controls and processes the data.
Embodiment 2
[0050] A method using the above device for measuring the transmittance curve of the FP by using the frequency comb light source as described in Embodiment 1, including the following operations:
[0051] S1, obtaining the required single frequency pulse laser 1 and the frequency comb laser 2 with a set type, and assembling the device;
[0052] S2. according to the working principle of the frequency comb laser 2 in
[0053] Specific operations of measuring transmittances corresponding to the different frequency components are:
[0054] S21, removing the FP 3 in the device, obtaining energy in the first detector 61 of the first receiving unit and the second detector 71 of the second receiving unit, and obtaining an energy ratio N1=energy value of the first detector 61/energy value of the second detector 71, where N1 is configured as a calibration coefficient; and
[0055] S22, after calibration, comparing a relative energy change of a frequency component measured by the first spectrometer 62 of the first receiving unit and a frequency component measured by the second spectrometer 72 of the second receiving unit, and multiplying the relative energy change by the calibration coefficient to obtain a transmittance of a corresponding frequency.
[0056] S3, performing, by the computer, polynomial fitting on transmittances corresponding to all frequency components to obtain the transmittance curve.
[0057] In this embodiment, taking a solid etalon as an example, the main parameters are shown in the following table.
TABLE-US-00001 Technical Require- Technical Require- parameter ment parameter ment Center wavelength (nm) 532 Surface accuracy λ/100 @633 nm Material refractive index 1.461 Fine number 17.9 Beam divergence full angle 8 Peak transmittance 0.860 (mrad) Thickness of etalon (mm) 0.1311 FWHM(pm) 41.3 Optical aperture (mm) 40 Center wavelength 532.12 (nm) Effective aperture (mm) 30 Resource spectral 739 range (pm) Reflectivity 86%
[0058] Combining the parameters in the table with the calculation methods in the background technology, the numerical simulation results of the etalon transmittance curve may be obtained.
[0059] It can be seen from the above numerical simulation results that when the thickness of the etalon is 131 μm and the two optical surfaces are coated with 86% reflective film, the center wavelength of the etalon is 532.37 nm and the peak transmittance is 86%.
[0060] According to this solution, that is, according to the principle shown in
[0061] In
[0062] The above are only preferred embodiments of this application and are not intended to limit this application. Any modification, equivalent replacement and improvement made within the spirit and principle of this application should be included in the scope of protection of this application.