Device, system and method for measuring space charges by using electro-acoustic (PEA) method
An electroacoustic pulse method and space charge technology, which is applied in the direction of measuring devices, electrostatic field measurement, and electric variable measurement, can solve problems that affect the reliability of DC EHV/UHV equipment, the difference in measurement results, and the complexity of electric field calculations.
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Embodiment 1
[0024] like figure 2 As shown, it is a structural block diagram of an electroacoustic pulse method space charge measurement device according to an embodiment of the present invention. The electroacoustic pulse method space charge measurement device 200 includes: an upper electrode unit 201 (which can be regarded as a first electrode), and the upper electrode unit 201 includes: aluminum electrode 202, epoxy resin 203, capacitor C, resistor R 1 and metal case. High voltage DC power supply 205, through resistor R 2 It is connected with the aluminum electrode 202. The pulse generator 206 is connected with the aluminum electrode 202 . The lower electrode 207 (which can be regarded as the second electrode), the piezoelectric sensor 208 connected to the lower electrode 207; the high temperature constant temperature circulating bath 214 (which can be regarded as the first constant temperature source), is connected to the upper electrode unit 201 through double conduits; the low te...
Embodiment 2
[0033] Such as image 3 As shown, the embodiment of the present invention is an electroacoustic pulse method space charge measurement system 300, and the electroacoustic pulse method space charge measurement system 300 includes: a high temperature constant temperature source 306, a low temperature constant temperature source 307, a PEA electrode device 301, a high voltage direct current power supply 302, a pulse Generator 303, oscilloscope 304 and computer 305; Wherein, PEA electrode device 301 comprises (as Figure 4 shown): the upper electrode unit 401 (which includes the first electrode), is in contact with one side of the insulating material sample to be tested, and is connected to the high-temperature constant temperature source 306 through a bidirectional conduit; the lower electrode unit 402 (which can be regarded as the second electrode), which is in contact with the other side of the insulating material sample to be tested, and is connected to the low-temperature cons...
Embodiment 3
[0038] Such as Figure 7 As shown, the embodiment of the present invention is an electroacoustic pulse method space charge measurement system 700, and the electroacoustic pulse method space charge measurement system 700 includes: a high temperature constant temperature source 706, a low temperature constant temperature source 707, a PEA electrode device 701, a high voltage DC power supply 702, a pulse Generator 703, oscilloscope 704, and computer 705; wherein, the PEA electrode device 701 includes an upper electrode unit (including the first electrode), which is in contact with one side of the insulating material sample to be tested, and is in contact with a high-temperature constant temperature source 706 through a bidirectional conduit. Connection; the lower electrode unit (which can be regarded as the second electrode) is in contact with the other side of the insulating material sample to be tested, and is connected to the low-temperature constant temperature source 707 thro...
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