Device, system and method for measuring space charges by using electro-acoustic (PEA) method
An electro-acoustic pulse method, space charge technology, applied in measurement devices, electrostatic field measurement, measurement of electrical variables, etc., can solve problems affecting the reliability of DC ultra/ultra-high voltage equipment, differences in measurement results, and complex electric field calculations.
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Embodiment 1
[0025] like figure 2 As shown, it is a structural block diagram of an electroacoustic pulse method space charge measuring device according to an embodiment of the present invention. The electroacoustic pulse method space charge measuring device 200 includes: an upper electrode unit 201 (which can be regarded as a first electrode), the upper electrode unit 201 includes: aluminum electrode 202, epoxy resin 203, capacitor C, resistor R1 and metal shell. The high-voltage DC power supply 205 is connected to the aluminum electrode 202 through a resistor R2. The pulse generator 206 is connected with the aluminum electrode 202 . Lower electrode 207 (can be regarded as the second electrode), the piezoelectric sensor 208 that links to each other with lower electrode 207; The constant temperature circulating bath 215 (which can be regarded as the second constant temperature source) is connected with the lower electrode unit 207 through double conduits.
[0026] The structure of the f...
Embodiment 2
[0034] like 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 with the high-temperature constant temperature source 306 through a bidirectional conduit; the lower electrode unit 402 (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 tem...
Embodiment 3
[0039] like 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 through...
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