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Recently, polyethylene (PE)-based single polymer composites (SPCs) have been found to be potential candidates for high-voltage applications (HVAs) due to their ability to form supramolecular structures and their recyclabilities. However, a deeper understanding of the controls and evolutions of such a structure is still needed. Herein, by introducing elongational flow into the melt compounding, we could successfully control the structure of polymeric materials and prepared PE-SPCs with additive-level ultrahigh-molecular-weight polyethylene (UHMWPE) for HVAs. The elongational flow-induced multiscale multilevel structure was confirmed and analyzed through X-ray diffraction. Specifically, under elongational flow, we fabricated PE-SPCs with the shish-kebab structure and 2D variated crystal units. The melting behaviors of each sample were studied, and the results indicated an elongational flow-induced cocrystallization phenomenon of low-density polyethylene and UHMWPE during melt processing. Benefiting from the as-formed structure, we obtained PE-SPCs with enhanced mechanical properties and more HVA-adaptable dielectric properties. Particularly, the yield strength, tensile strength, and Young’s modulus of PE-SPC (sample R80) show 42, 23, and 29% enhancement than the virgin PE, respectively. The dielectric constant and dielectric loss of our PE-SPC are determined to be around 2.94 and 2 × 10–4 at 1000 Hz, respectively. Moreover, 10-fold decreases in conductivites in both AC and DC of our PE-SPC are achieved after melt compounding under elongational flow. In conclusion, this work gives a comprehensive understanding of the PE-SPCs’ structure evolution under elongational flow, and the structure–property relationship was also determined. It is believed that this work can promote the development of SPCs for HVAs.
Recently, polyethylene (PE)-based single polymer composites (SPCs) have been found to be potential candidates for high-voltage applications (HVAs) due to their ability to form supramolecular structures and their recyclabilities. However, a deeper understanding of the controls and evolutions of such a structure is still needed. Herein, by introducing elongational flow into the melt compounding, we could successfully control the structure of polymeric materials and prepared PE-SPCs with additive-level ultrahigh-molecular-weight polyethylene (UHMWPE) for HVAs. The elongational flow-induced multiscale multilevel structure was confirmed and analyzed through X-ray diffraction. Specifically, under elongational flow, we fabricated PE-SPCs with the shish-kebab structure and 2D variated crystal units. The melting behaviors of each sample were studied, and the results indicated an elongational flow-induced cocrystallization phenomenon of low-density polyethylene and UHMWPE during melt processing. Benefiting from the as-formed structure, we obtained PE-SPCs with enhanced mechanical properties and more HVA-adaptable dielectric properties. Particularly, the yield strength, tensile strength, and Young’s modulus of PE-SPC (sample R80) show 42, 23, and 29% enhancement than the virgin PE, respectively. The dielectric constant and dielectric loss of our PE-SPC are determined to be around 2.94 and 2 × 10–4 at 1000 Hz, respectively. Moreover, 10-fold decreases in conductivites in both AC and DC of our PE-SPC are achieved after melt compounding under elongational flow. In conclusion, this work gives a comprehensive understanding of the PE-SPCs’ structure evolution under elongational flow, and the structure–property relationship was also determined. It is believed that this work can promote the development of SPCs for HVAs.
Insulation material is a key component of electrical equipment in satellites; its electrical properties determine the reliability and lifetime of the whole satellite. High-energy radioactive rays in space affect the molecular structure of the polymeric insulating materials. Under the action of plasma, high energy particles, along with the magnetic fields experienced in orbits, electric charges get injected into and trapped by the insulating material creating distortions in the electric field and even electrostatic discharges. Polyimides have been widely used for insulation in spacecraft. Choosing Co-60 gamma ray with irradiation doses of 1 MGy and 5 MGy to simulate the radiation environment of space, we investigated the effect of radiation on charging behaviour. The thermal stimulated current (TSC) from a high electric field over a wide range of temperatures was measured from which the activation energy was calculated. These results for the two sources show that the percentage increase in total charge was 133.3% and 119.4%. The γ, β 3 , and α charge peaks of specimens after an irradiation dose of 1 MGy rose. In comparison, the β 2 peak of the 5 MGy-dosed specimens was enhanced. Also, there is almost no change in the γ, β 3 , and α peaks. To understand the mechanism behind the TSC changes, the resulting physicochemical characteristics of an irradiated specimen were observed employing various analyses of chemical characteristics (x-ray photoelectron spectroscopy, differential scanning calorimetry and x-ray diffraction). Compared with the non-dosed specimen, the relative content of C-N and the glass transition temperature of the 1 MGy sample decreased, and the crystallinity increased, thus increasing the γ and α peak intensities. Compared with the 1 MGy sample, only the glass transition temperature had risen, thereby enhancing the β peak intensity. With the foregoing, a theoretical base for the selection and modification of insulation materials for spacecraft is provided.
Due to their excellent electrical insulation properties and processability, polymer materials are used in many electrical products. It is widely believed that space charge plays an important role for the electric field distribution, conduction, ageing, and electric breakdown of polymeric insulation. This paper reviews measurements and characteristics of space charge behavior which mainly determined by the pulsed electro-acoustic (PEA) measurement technique. Particular interests are the effects of the applied voltage, the electrodes, temperature, humidity, microstructure, additives, and filler materials on accumulation, distribution, transport, and the decay of space charge in polymeric materials. This review paper is to provide an overview on various space charge effects under different conditions, and also to summarize the information for polymeric materials with suppressed space charge and improved electrical behavior.
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