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Morphology Effects on Space Charge Characteristics of Low Density Polyethylene
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Low density polyethylene (LDPE) film samples with different morphology were prepared by three kinds of annealing methods which were different in cooling rates in this study. A pulsed electro-acoustic (PEA) space charge measurement system was improved to solve the surface discharge problems for small samples applied with a high voltage. Negative direct current (DC) fields from 50 to above 220 kV/mm were applied to the samples. The influences of morphologies on space charge and space charge packet characteristics were measured by the improved high voltage withstand (HVW) PEA system. Mobility and trap depth of released charges were calculated by space charge decay. It was found that there is a different probability of space charge packet initiation under applied field from -60 to -100 kV/mm. Average velocity and mobility of the space charge packets were calculated by space charge packet dynamics. It was found that the lower cooling rate samples have higher crystallinity, more homo-charge accumulation, lower mobility and deeper trap depth. The mechanism of morphological effects on space charge phenomena have been presumed to give a plausible explanation for their inherent relationships. The morphology in the metal–dielectric interface and in the bulk is convincingly suggested to be responsible for the injection and propagation processes of space charge. A model of positive space charge initiation in LDPE samples was also suggested and analyzed. The mechanism of morphological effects and the charge injection model are well fit with the injection and propagation processes of space charge. The different effects of morphology in the metal–dielectric interface and in the bulk of polymers are stressed.
Title: Morphology Effects on Space Charge Characteristics of Low Density Polyethylene
Description:
Low density polyethylene (LDPE) film samples with different morphology were prepared by three kinds of annealing methods which were different in cooling rates in this study.
A pulsed electro-acoustic (PEA) space charge measurement system was improved to solve the surface discharge problems for small samples applied with a high voltage.
Negative direct current (DC) fields from 50 to above 220 kV/mm were applied to the samples.
The influences of morphologies on space charge and space charge packet characteristics were measured by the improved high voltage withstand (HVW) PEA system.
Mobility and trap depth of released charges were calculated by space charge decay.
It was found that there is a different probability of space charge packet initiation under applied field from -60 to -100 kV/mm.
Average velocity and mobility of the space charge packets were calculated by space charge packet dynamics.
It was found that the lower cooling rate samples have higher crystallinity, more homo-charge accumulation, lower mobility and deeper trap depth.
The mechanism of morphological effects on space charge phenomena have been presumed to give a plausible explanation for their inherent relationships.
The morphology in the metal–dielectric interface and in the bulk is convincingly suggested to be responsible for the injection and propagation processes of space charge.
A model of positive space charge initiation in LDPE samples was also suggested and analyzed.
The mechanism of morphological effects and the charge injection model are well fit with the injection and propagation processes of space charge.
The different effects of morphology in the metal–dielectric interface and in the bulk of polymers are stressed.
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