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146 protocols using pyris 1 tga

1

Comprehensive Material Characterization of Stent

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First, we checked the structure and chemical composition of the stent material. We used TGA and TGA-GCMS to determine the chemical composition and SEM analysis to assess the material structure.
During TGA, we heated the samples to 600°C at a rate of 10°C/min. The samples were measured in an open platinum crucible in a synthetic air atmosphere (20 ml/min). The samples were measured in an air atmosphere to determine polydioxanone’s thermal stability in this atmosphere. TGA was performed on a Pyris 1 TGA (PerkinElmer, USA).
During TGA-GCMS, we heated the sample to 300°C at a rate of 10°C/min. The samples were measured in an open platinum crucible in a nitrogen atmosphere (20 ml/min; Linde N2 4.6). In TGA-GCMS, a nitrogen atmosphere must be used to protect the mass spectrometer’s heated wolfram filament from oxygen. The TGA-GCMS was performed on a Pyris 1 TGA, GC Clarus 680, and MS Clarus SQ 8T (all PerkinElmer, USA).
We inspected the filament material’s homogeneity, looking at the internal structure using SEM investigation. The samples were prepared by mechanically rupturing the filaments by simply cracking them with tweezers, mounting them on the SEM stub using carbon adhesive tape, and directly (without an additional coating to prevent charging) visualizing them using field-emission SEM (FE-SEM JEOL JSM 7500F, Japan) and the in-lens secondary electron detector.
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2

Thermogravimetric Analysis of Samples

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All samples were prepared with open aluminum pans. A thermogravimetric analyzer (TGA 1-Pyris, PerkinElmer, Inc., USA) was used to heat the samples from 30 °C to 500 °C at a rate of 20 °C/min. Ultra-purified nitrogen was used as a purge gas with a flow rate of 25 ml/min. Data collection and analysis were performed using the PerkinElmer Pyris™ software, and the per cent mass loss and/or onset temperature were calculated.
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3

Thermal Degradation Analysis of Polymers

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A thermogravimetric analyzer (TGA 1-Pyris, PerkinElmer, Inc., Waltham, MA, USA) was used to determine the thermal degradation of the polymers at the temperature employed in HME and 3D printing techniques. The samples were loaded in aluminum pans and heated from 50 to 500 °C at a rate of 20 °C/min. Ultra-purified nitrogen was used as a purge gas at a flow rate of 25 mL/min. The data were collected and analyzed using the PerkinElmer Pyris™ software (Waltham, MA, USA), and the percent mass loss was calculated.
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4

Freeze-Drying of Pollen Samples for Analysis

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FD was carried out on all treated and untreated pollens following the recent method detailed by Conte et al. [16 (link)]. Briefly, a lyophilizer Heto PowerDry® LL1500 with 4 manifolds connecting to 100 mL flasks filled with 70 g of fresh pollen (earlier stored at −20 °C) was used. Temperature in the condensation chamber was −115 °C, with a full vacuum. Heat exchange in Heto PowerDry® LL1500 was achieved by convection with the temperature of the test room, which was continuously conditioned at 25 °C. The maximum temperature reached by the sample during the process was 25 °C. To carry out pollen FD, full vacuum was created in the flasks. Each pollen sample was inserted into the chamber, its initial weight was recorded and then the sample was treated for 9 h. The exposure period was determined by preliminary tests followed by thermogravimetric analysis (TGA). The final weight was determined and the samples were sealed and stored at −20° C until the analyses [16 (link)]. The liquid inside the condensation chamber was sampled, sealed, and stored at a temperature of −20° C for further analysis. TGA (TGA Pyris 1 Perkin Elmer (Waltham, MA, USA)) conducted at 120 °C showed that the residual water content was 6.0%, 6.3%, and 7.5% for chestnut, willow, and ivy pollen, respectively.
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5

Thermal Analysis of Unsaturated Polyester

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TGA (Pyris1, PerkinElmer, Waltham, MA, USA) was used to investigate the mass loss and mass derivative of UP, UP-MEKPO, and UP-TBPO. The mass of pure UP was 3.0–3.5 mg. The heating rates were 10, 15, 20 and 25 °C/min, and the temperature range was 30–800 °C under a nitrogen atmosphere at 20 mL/min. DSC (DSC 821e, Mettler-Toledo, Greifensee, Switzerland) was used to observe the exothermic reaction of UP, UP-MEKPO, and UP-TBPO, which can obtain critical thermodynamic parameters, such as T0, Tp, and ΔHexo. The masses of UP mixed with hardeners for 1:1, 3:1, and 5:1 were 3.5–4.0, 4.0–5.5, and 6.0–6.5 mg, respectively. The heating rates were 2, 4, 8, and 16 °C/min, and the temperature range was 30–300 °C under a nitrogen atmosphere at 20 mL/min. Moreover, oven heating was used to carry out the curing reaction for UP-TBPO or UP-MEKPO at 150 °C and 20 min.
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6

Thermal Stability and Flammability Analysis of Polymers

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The thermal stability of the samples was determined using thermogravimetric analysis (TGA Pyris 1, Perkin-Elmer, Waltham, MA, USA). The sample weights were approximately 5 mg. Experiments were performed between 30 and 750 °C at different heating rates (5, 10, 20, and 40 K/min) under nitrogen (20 mL/min). The decomposition temperature used with Kissinger’s method was determined as the temperature of the peak of mass loss rate on a dTG (derivative thermogravimetric) curve.
The flammability of the polymers listed in Table 1 was analyzed using a PCFC (FTT, Derby, UK) under standard conditions, i.e., anaerobic pyrolysis from 25 to 750 °C at 1 °C/s in nitrogen, and complete combustion in an excess of oxygen at 900 °C [12 ].
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7

Thermogravimetric Analysis of Functionalized Fillers

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Thermogravimetric analysis (TGA Pyris 1, PerkinElmer) was used to analyze the functionalized fillers. Each sample was run in a nitrogen atmosphere (20 ml /min) from 50°C to 850°C at a heating rate of 10°C/ min.
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8

Thermal Analysis of Functionalized Fillers

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Thermogravimetric analysis (TGA Pyris 1, Perkin Elmer) was used to analyze the functionalized fillers. Each sample was run in a nitrogen atmosphere (20 ml min−1) from 50 °C to 850 °C at a heating rate of 10 °C min−1.
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9

Comprehensive Characterization of Carbon-Based Materials

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The morphology of the samples was examined through FE-SEM (Ultra Plus, Zeiss) and FE-TEM (JEM-2100F, JEOL). The phase and crystal structure of the samples were analyzed by XRD (D8 Discover with GADDS, Bruker) using Cu Κα radiation (I = 1.5418 Å). The chemical environment of elements in the samples was determined by XPS (K-Alpha, Thermo Fisher Scientific) using a monochromatic Al Κα radiation at 12 kV and 20 mA. The crystallinity of the carbonaceous materials in the prepared samples was investigated through Raman spectroscopy (Horiba Jobin–Yvon, HR800, LabRam). The surface area of the samples was measured by the BET method, where N2 was used as the adsorbate gas. The carbon content was quantified by TGA (Pyris 1, PerkinElmer) in an air atmosphere from 30 to 600 °C at a ramp rate of 10 °C min−1. The inductively coupled plasma-optical emission spectrometer (ICP-OES) analysis was performed to determine the elemental composition using Perkin Elmer OPTIMA 7300 DV. Elemental analysis (EA) technique based on high temperature (1200 ~ 1400 °C) combustion method was employed for quantitative analysis of C and N elements in the prepared samples (vario MICRO cube, Elementar). The amount of sample used for the analysis was 2.5 mg.
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10

Thermal Characterization of Starch-based Bioplastics

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Thermal behaviors of pure starch-based and chitosan-reinforced starch-based bioplastic films were characterized by thermal gravimetric analysis (TGA). This thermal decomposition analysis was performed by using a thermogravimetric analyzer (Perkin Elmer, model TGA Pyris 1). A bioplastic film of around 5 mg was placed in a platinum pan and heated from ambient temperature to a final temperature of 900 °C at a heating rate of 20 °C/min with nitrogen flow rate of 50 mL/min [19 (link),32 (link)].
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