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A schematic diagram of the experimental setup is shown in Fig. 1a. The glass sample is irradiated using a CO2 laser with a centre wavelength of 10.6 μm and a maximum power of 30 W. In this configuration, the CO2 laser beam was maintained in the horizontal plane at an angle of approximately 15° relative to the vertical axis of the sample. To measure the dynamics during irradiation, the temporally stretched femtosecond laser-chirped pulse was first split into signal and reference paths. In the signal path, the pulse was spatially dispersed and focused on the surface of the glass by the first diffraction grating and objective lens, respectively. Therefore, variations on the glass surface were mapped onto the probe-pulse spectrum. Subsequently, the 1D rainbow pulse was collected and spatially recombined by the second objective lens and diffraction grating with the same parameters as the first. Considering temporal stretching, also known as dispersive Fourier transform, has already linked the temporal and frequency domains of the pulse, the spatial information of the glass was mapped onto the temporal waveform of the pulse. To acquire the intensity and phase of the pulse simultaneously, the pulses of the signal and reference paths were coupled and detected by the photodetector. Finally, the 1D interference signal I(t) is sampled by a digitiser and processed in the digital domain to recover the images of the glass.
Fig. 1 Experimental observation and numerical simulation of surface topography evolution in LP. a Real-time and in situ observation of LP using OTS-QI. Temporally stretched femtosecond pulses are split into two paths, one for signal detection and the other as the reference. The pulses in the signal path are spatially dispersed and focused onto the polishing area. After recording the surface topography evolution during LP, the pulses are spatially recombined and coupled with the reference pulses for photodetection later. Finally, the images of the temporal evolution during LP are recovered by digital signal processing. b Positional relationship between the CO2 laser irradiated on the sample and probe pulse. c. Multi-physics model used to numerically analyse the dynamic process in LP, where heat transfer, phase change, microflow, and evaporation are considered.
To better capture a real-world scenario, as depicted in Fig. 1c, a multi-physics FEM was designed as a reference. A two-dimensional model of a full-size sample was established to accurately calculate the solid heat transfer, thereby overcoming the drawback of inaccurate boundary conditions observed in most micro-area models. Subsequently, a micro-area was selected within the laser irradiation area for mesh refinement and dynamic analysis, which included the phase transformation, flow field, evaporation, and other pertinent factors. Detailed information regarding the specific boundary condition settings and control equations is provided in Fig. S1 and Table S1. The physical parameters of the materials are listed in Table S2. In the calculation time range, large-scale Marangoni flow and material evaporation are also accounted for, as these phenomena can occur readily despite not being the intended outcome of the LP process.
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To demonstrate the performance of the OTS-QI, we measured the images of quartz glass processed with the CO2 laser using an optical microscope, a 3D optical surface profiler, and an OTS-QI. As shown in Fig. 1, in OTS-QI, the probe pulse exhibited a linear shape as it passed through the sample. Therefore, in this experiment, we mounted a glass sample on a one-dimensional (1D) y-axis-moved motorised translation stage. As shown in Fig. 2a, each pulse measured one cross-section of the sample. The pulses covered the entire sample surface as the stage moved from the top to the bottom. By stacking z(x, t0), the 2D surface topography z(x, y) of the sample could be recovered on the y-axis (see Materials and Methods). The inset of Fig. 2a shows the image of the standard USAF-1951 resolution chart, and the spatial resolution of the OTS-QI is 7.81 µm. The lateral spatial resolution of the system can be readily enhanced to the optical diffraction limit corresponding to the detection wavelength. However, this enhancement necessitates a trade-off in the spatial range of measurements. The initial roughness of the glass surface was 0.22 µm, and the power density of the laser beam was 7.0 × 104 W/cm2. We irradiated the glass surface for 10 ms, 20 ms, and 40 ms, with the images of the glass samples acquired using the three different methods shown in Fig. 2b. The intensity and phase images acquired with OTS-QI exhibited high similarity to those obtained using a microscope and 3D optical surface profiler. These images reveal that, with an increase in processing time, the central region of the sample undergoes successive stages of smoothing and ablation.
Fig. 2 Imaging performance of OTS-QI. a Principle of 2D image recovery. b 2D surface topography of glass acquired using a conventional microscope, a 3D profilometer, and the proposed OTS-QI with a processing time of 0 ms, 10 ms, 20 ms, and 40 ms at a power density of 7.0 × 104 W/cm2, respectively. c Cross-sections of the images acquired by the 3D profilometer and proposed OTS-QI.
Furthermore, in Fig. 2c, we depict the cross-sections of the images acquired with our OTS-QI and the 3D optical surface profiler with different processing times. We employed the relevant factor, defined as
$$ {\rho _{xy}} = \frac{{\mathop \sum \nolimits_{n = 1}^N \left( {{x_n} - \bar x} \right)\left( {{y_n} - \bar y} \right)}}{{\sqrt {\mathop \sum \nolimits_{n = 1}^N {{\left( {{x_n} - \bar x} \right)}^2} \cdot \mathop \sum \nolimits_{n = 1}^N {{\left( {{y_n} - \bar y} \right)}^2}} }} $$ (1) to quantitatively evaluate the differences between the curves. In Eq. 1, xn and yn represent the 1D data of the curves acquired using the OTS-QI and optical profiler, respectively. The results show that the relevance of all the curve pairs in Fig. 2c is greater than 0.9, indicating that the accuracy of our OTS-QI is almost identical to that of the optical profiler.
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Alternatively, as shown in Fig. 3a, we can also fix the position of the 1D rainbow beam on the surface of the glass and then start laser processing and measurement simultaneously. Owing to the high repetition rate of the probe pulse (~100 MHz), each pulse measures z(x, t) at a specific time t. Hence, by stacking the pulses, an image recording the temporal evolution of the material surface during LP can be obtained. In the experiment, the glass sample was illuminated by a CO2 laser with a power density of 7.0 × 104 W/cm2 for 50 ms before turning off the laser. The surface evolution over 100 ms, including 50 ms for processing and 50 ms for cooling, was measured by our OTS-QI, and z(x, t) at different times is plotted as black curves in Fig. 3b. We simulated the same process using the numerical model and show images of the glass sample at the corresponding times in Fig. 3b. Both the experimental and numerical results showed that, as the processing started, the centre part of the glass bulged owing to an increase in the local temperature. When the temperature reaches the glass softening point, the material tends to flow towards a smaller surface area owing to surface tension, decreasing the roughness. The roughness of the glass surface reached its minimum value at approximately 25 ms. As heating continued, the temperature at the centre reached the evaporation point. The Marangoni effect causes the liquid in the molten pool to flow from the centre to the sides while simultaneously ablating the pool centre. Combining these two factors results in the gradual formation of a pit at the laser irradiation centre, with a convex edge commonly known as a ‘crater’ shape. Thus, the formation of the MFW is primarily attributed to the Marangoni effect and ablation, both of which occur over prolonged interaction times. After laser irradiation was terminated, the material was rapidly cooled. The correspondence between the experimental and numerical results indicated that the OTS-QI system accurately and efficiently captured and recorded the evolution of the surface topography during the LP in situ and in real time.
Fig. 3 Temporal evolution of glass surface topography during LP. a Image construction of glass surface topography evolution during LP. b Numerical (colour regions) and experimental (black curves) results of the glass surface topography at different time points during LP. As LP starts, surface thermal expansion occurs first, followed by the smoothing process of shallow melt microflow at 20–25 ms, the Marangoni flow from 27 ms, and ablation from 30 ms to 50 ms. As the laser is turned off at 50 ms, the surface starts to cool down, eventually resulting in a crater shape at 70 ms.
These findings provide a comprehensive picture of the evolution of surface topography during LP. As shown in Fig. 4, the glass surface underwent a sequence of transformations, including thermal expansion, smoothing flow, wavy flow, and ablation, from the beginning of the process. Thermal expansion does not directly affect the final processing outcome. Although Marangoni flow is always present in physics, in the early stages, the smoothing process driven by the surface tension was dominated by the shallow molten pool. As the molten pool expanded, the disadvantages of the Marangoni effect began to emerge, leading to the formation of waviness on a large spatial scale. As the temperature of the molten pool needs to be controlled just below the evaporation point in LP, the fluctuations in laser power (e.g., the typical stability of industrial CO2 lasers is ±5%) and the differences in thermal processes at different locations unavoidably cause slight ablation in random areas, resulting in random MFW. Therefore, the smoothness achieved depends strongly on when laser processing is terminated.
Fig. 4 Schematic diagram of the surface topography evolution of quartz glass during LP. As LP starts, a series of transformations occur successively, including melting, flow, smoothing, and ablation processes. Notably, the process of shallow melting and surface smoothing is transient. Therefore, the achieved surface roughness highly depends on when the heating is terminated. The minimum surface roughness can be acquired when the processing is terminated at a certain point; otherwise, Marangoni flow and ablation will occur on the surface, resulting in MFW.
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The aforementioned phenomenon indicates the existence of a ‘polishing window’, which facilitates controlling the interaction time between the laser and the material, thus allowing the processing area to begin cooling just as the roughness decreases to its minimum value, thereby avoiding uneven flow and material removal. This window constitutes an essential foundation for the theoretical feasibility of LP processes. We refer to this window as the ‘perfect polishing point’, denoting a specific action time for a given laser power density at which roughness can be reduced to its lowest value. As illustrated in Fig. 5a, we measured the temporal evolution of the laser-polished glass surfaces at different power densities ranging from 3.5 × 104 W/cm2 to 1.4 × 105 W/cm2. The four critical time points—T1, T2, T3, and T4—represent the moments when the measurement starts, heating starts, heating stops, and the measurement ends, respectively. Except for the power density of 3.5 × 104 W/cm2, insufficient to melt the surface within the given processing time, the other three figures exhibit a similar trend as that in Fig. 3. Additionally, owing to the quantitative measurement capability of OTS-QI, the specific values of surface roughness directly correspond to z(x, t), allowing us to detect changes in roughness with nanosecond accuracy, as shown by the solid line in Fig. 5b. To facilitate the comparison, we included the results generated by the numerical model (shown as dashed lines). Both the experimental and numerical results demonstrate the existence of a perfect polishing point, which represents the processing window we strive to achieve in practice.
Fig. 5 Temporal evolution of the quartz glass topography during LP under different power densities. a Images of temporal evolution of the quartz glass topography under laser power densities of 3.5 × 104 W/cm2, 7.0 × 104 W/cm2, 1.05 × 105 W/cm2, and 1.4 × 105 W/cm2, respectively. T1, T2, T3 and T4 represent the moments of the start of the measurement, heating started, heating stopped, and the end of the measurement, respectively. b Temporal evolution of the surface roughness of the quartz glass during LP under different laser power densities acquired by OTS-QI and the simulation. The perfect consistency between the experimental and numerical results indicates that OTS-QI can achieve high-speed and accurate quantitative measurement of surface roughness during LP.
In practice, the beam scanning of a material surface is necessary to polish a specific surface area, with the interaction time determined by the size of the light spot and the scanning speed; therefore, a ‘perfect polishing point’ can be considered an optimal combination of power density and scanning speed. Fig. 6 presents the experimental results of the scanning polishing process conducted at a peak power density of 800 W/cm2 and scanning speeds ranging from 0.03 mm/s to 0.25 mm/s. To analyse the data, we converted the X-axis in Fig. 5b from time to scanning speed, with the calculated surface RMS variation curve shown in Fig. 6a. We selected four typical scanning speeds and measured their corresponding surface topographies. The measured topographies before and after applying the roughness filter are shown in Fig. 6b, with the calculated RMS values indicated for comparison in Fig. 6a. The results indicate that excessively high scanning speeds result in insufficient re-melting flow (Fig. 6bI), whereas excessively low scanning speeds lead to Marangoni flow (Fig. 6bIII) and significant material removal (Fig. 6bIV). The optimal scanning speed corresponded to the proposed ‘perfect polishing point’ (Fig. 6bII). In Figs. 6bIII, IV, despite a pronounced MFW caused by Marangoni flow and non-uniform removal, the micro-roughness does not exhibit a significant increase. This finding aligns with our theoretical predictions using FEM and the observations using OTS-QI.
Fig. 6 Surface roughness evolution of CO2 laser polished quartz glass under different scanning speeds. a Surface roughness under different scanning speeds with a CO2 laser power density of 800 W/cm2. b Surface topography measured by a white light interferometer (WLI) under different scanning speeds. The upper images show the original results, while the lower images are the results after roughness filtering. The results demonstrate that optimal polishing is achieved at the scanning speed of 0.2 mm/s, where the RMS reduced from >300 nm to 3.5 nm, and the corresponding microroughness is 0.1 nm, aligning with our perfect polishing point theory acquired using OTS-QI.
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The source was a femtosecond laser (PriTel FFL-FR-PMFA) with a central wavelength of 1555 nm, bandwidth of 15–30 nm, pulse repetition frequency of 101.7 MHz, and average output power greater than 100 mW, with an adjustable pulse width and spectral width in the range of 100–400 fs and a 3 dB spectral width in the range of 15–30 nm, respectively. Each pulse of the laser was used for time-domain stretching by a 15 km single-mode fibre (SMF) (YofcA5H02621WB1) with a group velocity dispersion (GVD) of approximately 255 ns/nm and amplified by an erbium-doped fibre amplifier (EDFA) (GT-EDFA-C-T-200-FA-FA) with an optical gain of approximately 20 dB. The dispersed amplified pulses were split into two optical paths using a non-polarised beam splitter (Thorlabs BS006) with a power ratio of 50:50, forming a signal path and a reference path. In the signal path, the optical signal pulse was spatially dispersed through a diffraction grating (Thorlabs GR25-0616) with an inscribed line density of 600 lines/mm, resulting in a one-dimensional (1D) rainbow pulse focused on the laser processing area by a lens (Thorlabs LA1509-C, f = 100 mm) acting as an objective lens.
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Interferometric fringes can be extracted by applying a digital high-pass filter to remove the low-frequency components. The interferogram was then Fourier transformed to obtain the real and imaginary parts of the transform, which are used to calculate the intensity and phase signals. A phase unwrapping algorithm is employed to obtain a continuous phase image44.
In an optical time-domain stretching quantitative phase microscopy system, the spatial information (x) of the laser processing region in intensity and phase is converted into the spectral information (ω) of the pulse via a conversion factor (B).
$$ {{\Delta }}x = B{{\Delta }}\omega $$ (2) The conversion factor (B), typically determined by the inscribed density of the diffraction grating (600 lines/mm), focal length (f) of the lens acting as the objective, and magnification of the 4f lens system in the system, is generally calibrated for confirmation by imaging a known resolution chart, such as the USAF-1951 resolution plate. This method is typically used to determine B in optical systems.
The temporal information of the detected signal (t) is obtained from the spectral information of the pulse (ω) via a conversion factor (C), also known as a temporal interferogram. This method is commonly used to convert spectral information into temporal information in pulse measurement systems.
$$ {{\Delta }}\omega = C{{\Delta }}t $$ (3) The conversion factor (C) was determined using the total group velocity dispersion (GVD) of the system. In this study, the GVD of a single-mode fibre (SMF) used for the time-domain stretching of the entire system was approximately equal to the total GVD of the system.
Eqs. 2 and 3 can be combined to obtain the following result:
$$ {{\Delta }}x = BC{{\Delta }}t $$ (4) According to Eq. 4, the spatial information (x) of the laser-processing region can be obtained by detecting the temporal information (t), which allows us to decode the temporal interferogram using the conventional QPI algorithm to construct an intensity and phase image of the laser-processing region. To create a frequency difference between the signal and reference path pulses, we partially aligned the reference path pulse in the time domain with the signal path pulse and adjusted the optical range difference between the reference and signal paths to s. Each temporal interferogram can be expressed as
$$ I(t) = {I_R}(t) + {I_S}(t) + 2\sqrt {{I_R}(t){I_S}(t)} \cos \left[ {K(t){{\Delta s}} + {\phi _S}(t)} \right] $$ (5) In Eq. 5, $ {I_R}(x) $ and $ {I_S}(x) $ represent the intensity values of the reference and signal pulses, respectively. The chirp rate of the temporal dispersion pulse is represented by $ K(t) $, while $ {\phi _S}(t) $ represents the phase information of the detected laser-processing region. By utilising the conversions of x and t in Eq. 4, Eq. 5 can be rewritten as follows:
$$ I(x) = {I_R}(x) + {I_S}(x) + 2\sqrt {{I_R}(x){I_S}(x)} \cos \left[ {\frac{{K(x){{\Delta s}}}}{{BC}} + {\phi _S}(x)} \right] $$ (6) Extract the intensity graph information $ {I_S}(x) $ and phase graph information $ {I_R}(x) $ from Eq. 6, respectively representing $ {I_S}(x) $ and $ {I_R}(x) $ in Eq. 6 as low-frequency components and high-frequency components, we can remove $ {I_S}(x) $ and $ {I_R}(x) $ by high-pass filtering and only retain the last term in Eq. 6, a high-frequency component (HFC). By applying the Hilbert transform in Eq. 6, the real and imaginary parts of the final term in Eq. 6.
$$ {\rm Re} [HFC] = \sqrt {{I_R}(x){I_S}(x)} \cos \left[ {\frac{{K(x){{\Delta }}s}}{{BC}} + {\phi _S}(x)} \right] $$ (7) $$ {\rm Im} [HFC] = \sqrt {{I_R}(x){I_S}(x)} \sin \left[ {\frac{{K(x){{\Delta }}s}}{{BC}} + {\phi _S}(x)} \right] $$ (8) Eq. 7 and Eq. 8 lead to:
$$ {I_S}(x) = \frac{{{\rm Re} {{[HFC]}^2} + {\rm Im} {{[HFC]}^2}}}{{{I_R}(x)}} $$ (9) $$ {\phi _S}(x) = \frac{1}{2}{\tan ^{ - 1}}\frac{{{\rm Im} [HFC]}}{{{\rm Re} [HFC]}} - \frac{{K(x)\Delta s}}{{BC}} $$ (10) Once the phase map information $ {\phi _S}(x) $ is obtained, the phase image of the detected laser processing area can be obtained using the phase demodulation method.
The optical path difference (OPD) of the pulse after passing through the sample as a function of the phase change is given by Eq. 11
$$ OPD(x) = \frac{{\lambda (x)}}{{2\pi }}{\phi _S}(x) $$ (11) The optical path difference of the pulse can also be expressed as
$$ OPD(x) = n(x) \cdot z(x) $$ (12) where n(x) is the refractive index of the sample at different locations and s(x) is the thickness of the sample at different locations
Therefore, height fluctuations on the sample surface can be expressed as
$$ \Delta z(x) = \frac{{\lambda (x)}}{{2\pi n(x)}}\Delta {\phi _S}(x) $$ (13) A two-dimensional static height fluctuation image $ \Delta z(x,y) $ of the melt pool can be reconstructed by stacking the one-dimensional height fluctuations $ \Delta z(x) $ in the above equation in space, while a one-dimensional dynamic height fluctuation image $ \Delta z(x,t) $ of the melt pool can be reconstructed by stacking the one-dimensional height fluctuations $ \Delta z(x) $ in the above equation in time. Similarly, the 2D static-intensity image $ {I_S}(x,y) $ of the melt pool can be obtained by spatially stacking the 1D intensity $ {I_S}(x) $ in Eq. 9.
Considering the transmissive time-domain stretching imaging system used in this study, the detection light with a wavelength of 1555 nm must penetrate the sample to record the surface information, as shown in Eq. 13, with the magnitude of the refractive index of the sample in the imaging system related to the height fluctuation obtained from the measurements. During in situ observations, the refractive index of the glass changes with temperature at different locations, i.e., different times and locations have different refractive indices, affecting the measurement of height fluctuations on the sample surface and becoming part of the cause of the experimental error.
To avoid the effect of refractive-index changes on the measurement results, reflective time-stretch quantitative interferometry will be used in the future.
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The simulation principles and parameters are detailed in Supplementary Sections S1 and S2, respectively. The simulation results for quartz glass and a comparison with laser metal polishing are presented in Supplementary Section S3.
Dynamics of molten pool evolution and high-speed real-time optical measurement in laser polishing
- Light: Advanced Manufacturing , Article number: (2024)
- Received: 09 May 2024
- Revised: 26 August 2024
- Accepted: 28 August 2024 Published online: 14 October 2024
doi: https://doi.org/10.37188/lam.2024.050
Abstract: Laser polishing (LP) is considered an effective method for generating ultrasmooth surfaces owing to its precision, flexibility, and material compatibility. However, a lack of understanding of the evolution of surface topography during LP significantly limits the achievable surface roughness in practice. In this work, for the first time, by employing optical time-stretch quantitative interferometry (OTS-QI), we recorded the entire evolution of surface topography during LP with nanosecond-level temporal resolution, providing insight into the mechanisms involved in the surface roughness evolution, such as the Marangoni effect and the formation mechanism of mid-frequency waviness (MFW). Assisted by numerical calculations, we reveal that a ‘perfect polishing point’ exists, i.e., the optimal interaction time for LP at a specific laser power density, at which the surface roughness can be minimised without the formation of an MFW owing to the Marangoni effect and non-uniform removal. This OTS-QI system harnesses the rapid repetition rate of femtosecond lasers, achieving a remarkable measurement speed exceeding 100,000,000 times per second while preserving a measurement accuracy comparable to that of existing white light interferometers (WLIs), setting a new benchmark as the fastest recorded roughness measurement. In addition to LP, the proposed method can be applied for real-time and in situ monitoring of many machining scenarios involving highly dynamic phenomena.
Research Summary
In-situ monitoring: Real-time optical quantitative measurement of melt pool
A device capable of quantitatively measuring surface topography with ns time resolution holds promise for real-time observation and regulation of laser processing. Optical time stretch is a data acquisition method that enables continuous imaging, reflectometry, terahertz and other measurements at refresh rates reaching billions of frames per second with non-stop recording spanning trillions of consecutive frames. The teams of Du Wang and Cheng Lei from Wuhan University and Zong-qing Zhao from China Academy of Engineering Physics report on the development of an optical time stretch quantitative measurement system that has been applied to the monitoring of surface morphology during laser polishing. The team used this method to confirm the time scale of each mechanism in the laser polishing, demonstrating that optimal polishing can be achieved by tightly controlling the flow field in the molten pool.
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