1. The device for detecting the interturn electromagnetic pulse vibration wave characteristics of the rotor winding of the turbonator is characterized by comprising an ultra-large capacity internal resistance signal source, wherein the ultra-large capacity internal resistance signal source is connected with an ultra-high speed time sequence control circuit, the ultra-high speed time sequence control circuit is connected with the positive electrode and the negative electrode of the rotor winding through a parasitic inductive power supply and a positive and negative load wave guide line, and the positive electrode and the negative electrode of the rotor winding are connected with an ultra-high speed acquisition circuit through an operational amplifier circuit.

2. The apparatus for detecting the turn-to-turn electromagnetic pulse vibration wave characteristics of the rotor winding of the non-salient pole type steam turbine generator according to claim 1,

the ultra-large capacity internal resistance signal source is matched with the circular polarization characteristic average time constant of each turn of winding and can generate the energy width of the power circular polarization characteristic wave matched with the whole-course response time constant of the rotor winding;

the parasitic inductive power supply performs circular waveguide coupling exchange on the input and output coupled circular polarized waves of the positive and negative poles;

the positive and negative load wave guide lines couple circularly polarized waves to the positive and negative poles of the rotor in parallel;

the operational amplifier circuit combines, couples and amplifies the signals transmitted and received by the concurrent circular polarization;

the ultrahigh-speed acquisition circuit acquires waveforms which are combined by circularly polarized dual-signal emission sources, induced polarization sources at each turn and circularly polarized waveguide loads formed by double-symmetrical combination and time constants for energy maintenance of signal sources.

3. The method for detecting the characteristics of the distributed electromagnetic pulse vibration waves among the turns of the rotor winding of the large-scale non-salient pole type steam turbine generator as claimed in claim 1 or 2, characterized in that a super-large capacity internal resistance signal source and a super-high speed time sequence control circuit generate a high-order mutation electric field of an avalanche polarization edge, symmetrically deflect 180-degree circularly polarized electromagnetic waves generated by a parasitic inductive power supply, and are coupled to a positive electrode and a negative electrode of the rotor clockwise or anticlockwise through positive and negative electrode load wave guide lines, a first positive electrode turn and a first negative electrode turn are mutually inducted to generate a first sine wave in sequence, energy is returned to the inductive parasitic power supply in time delay, and meanwhile, the energy is sequentially conducted to a second turn; the parasitic inductive power supply and the second turn start circularly polarized feedback energy feedback; feeding back and overlapping each turn step by step in sequence; each coupling turn exhibits a sine wave with the same time constant.

4. The method for detecting the inter-turn distributed electromagnetic pulse vibration wave characteristics of the rotor winding of the large-scale non-salient pole type steam turbine generator according to claim 3, wherein when the time for maintaining the positive circular polarization transmission and the negative polarization deflection of 180 degrees for transmitting the one-way energy field is simultaneously longer than the full-length wave guide time of the rotor winding, each turn of symmetrical winding presents double electromagnetic pulse vibration wave characteristic waveforms of signal source and load superposition, and circular polarization wave waveforms formed by the current turn can be synchronously superposed and coupled in time through self-inductance and mutual inductance, and the magnetic flux which is changed from top to bottom in the positive direction is characterized; if the sine wave of the current turn is complete and the change of the wavelength time constant is small, the electromagnetic property of the current symmetrical turn is complete; if the sine wave of the current turn is incomplete, the wavelength of the sine wave superposed with the front and the back is larger than the standard time constant, which indicates that the current turn has defects, and has early hidden troubles such as deformation, oil stain, slot wedge looseness or displacement, early turn-to-turn short circuit and the like.

5. The method for detecting the characteristics of the distributed electromagnetic pulse vibration waves between the turns of the rotor winding of the large-scale non-salient pole type steam turbine generator according to the claim 3, is characterized in that a circular polarized unidirectional energy field with a positive pole and a circular polarized unidirectional energy field with a negative pole deflected by 180 degrees are applied in a counterclockwise direction, symmetric acquisition and comparison are carried out, two circular polarized waves with the same rotating direction are coupled with a counterclockwise circular polarized wave waveform formed by a current turn, and magnetic fluxes which change reversely from bottom to top are characterized; the defect turns can be repeatedly verified, and the positions of the defects on the positive electrode and the negative electrode are judged.

6. The method for detecting the characteristics of the distributed inter-turn electromagnetic pulse vibration waves of the rotor winding of the large-scale non-salient pole type steam turbine generator according to claim 3,

when the unit length of each turn of the rotor load is integral multiple of the wavelength of transmitting the circularly polarized wave,

the measured rotor load is a dielectric material (ur ═ 1), and the attenuation constant and phase constant of the electromagnetic wave are known as follows:

wherein alpha is_sIs the decay constant; beta is a_sIs a phase constant; c is the vacuum light speed; f is the frequency of the generated electromagnetic wave; epsilon₀Is a free space dielectric constant of 10^-9/36πF/m；ε_rFor each turn of the winding the relative dielectric constant, e_r＝ε′_r-jε″_r，ε′_rIs the real part of the relative dielectric constant of each turn of winding, epsilon ″)_rRelative dielectric constant imaginary part of each turn of winding;

the wavelength of the circularly polarized wave in the rotor winding is:

in the formula, λ₀C/f is the free space wavelength of the circularly polarized wave; lambda [ alpha ]_SThe average wavelength of circular polarized waves in the rotor winding; when the circumference of the single turn rotor winding is an integer multiple of the wavelength 1/2 of the emitted electromagnetic wave, i.e.

Wherein n is a positive integer, the propagation coefficient T can be obtained²：

The propagation coefficient may truly reflect the internal impedance time constant.

Background art:

at present, the detection of the state of a rotor winding of a non-salient pole large-scale turbonator at home and abroad generally adopts lumped parameter detection, such as direct current resistance, insulation resistance, alternating current impedance, high-frequency alternating current impedance and the like; the distribution parameter detection method comprises an open transformer method, a distributed voltage method, an RSO single pulse method, a large coil single alternating current pulse test method and the like. The detection of the winding inter-turn state is rough, only approximate cumulative characteristics of the rotor winding coil can be judged, most of the waveforms can be analyzed integrally, each large coil is analyzed in detail at most, and the electromagnetic wave characteristics of each turn cannot be reflected accurately, comprehensively, completely and visually. At present, a corresponding theory and a targeted detection means for the coupled electromagnetic wave characteristics of each turn of winding are not available. And the targeted and accurate waveform data analysis cannot be realized.

The invention content is as follows:

the invention aims to provide a device and a method for detecting the interturn electromagnetic pulse vibration wave characteristics of a rotor winding of a turbonator, which can fill the detection defects, and can clearly, simply and intuitively present the real electromagnetic characteristics of each forward or reverse symmetrical corresponding turn of a positive winding and a negative winding in a one-to-one correspondence manner.

In order to achieve the purpose, the device for detecting the turn-to-turn electromagnetic pulse vibration wave characteristics of the rotor winding of the turbonator comprises an ultra-large capacity internal resistance signal source, wherein the ultra-large capacity internal resistance signal source is connected with an ultra-high speed time sequence control circuit, the ultra-high speed time sequence control circuit is connected with the positive electrode and the negative electrode of the rotor winding through a parasitic inductive power supply and a positive and negative load wave guide line, and the positive electrode and the negative electrode of the rotor winding are connected with an ultra-high speed acquisition circuit through an operational amplifier circuit.

Preferably, the ultra-large capacity internal resistance signal source is matched with the circular polarization characteristic average time constant of each turn of winding and can generate the energy width of the power circular polarization characteristic wave matched with the whole-course response time constant of the rotor winding;

the parasitic inductive power supply performs circular waveguide coupling exchange on the input and output coupled circular polarized waves of the positive and negative poles;

the positive and negative load wave guide lines couple circularly polarized waves to the positive and negative poles of the rotor in parallel;

the operational amplifier circuit combines, couples and amplifies the signals transmitted and received by the concurrent circular polarization;

the ultrahigh-speed acquisition circuit acquires waveforms which are combined by circularly polarized dual-signal emission sources, induced polarization sources at each turn and circularly polarized waveguide loads formed by double-symmetrical combination and time constants for energy maintenance of signal sources.

The method comprises the steps that a super-large capacity internal resistance signal source and a super-high speed time sequence control circuit generate a high-order mutation electric field of an avalanche polarization edge, circularly polarized electromagnetic waves which are generated by a parasitic inductive power supply and symmetrically deflect 180 degrees are coupled to a positive electrode and a negative electrode of a rotor through a positive load wave guide line and a negative load wave guide line in a clockwise or anticlockwise mode, a first positive turn and a first negative turn are mutually induced to generate a first sine wave in sequence, energy is returned to the inductive parasitic power supply in a time sequential delay mode, and meanwhile, the energy is sequentially conducted to a second turn; the parasitic inductive power supply and the second turn start circularly polarized feedback energy feedback; feeding back and overlapping each turn step by step in sequence; each coupling turn exhibits a sine wave with the same time constant.

Preferably, when the time of maintaining the positive circular polarization sending and the negative polarization deflection 180 degrees and circularly polarization sending one-way energy field clockwise is simultaneously longer than the full-length wave guide time of the rotor winding, each turn of symmetrical winding presents dual electromagnetic pulse vibration wave characteristic waveforms superposed by a signal source and a load, and circular polarization wave waveforms formed by the current turn can be synchronously superposed and coupled in time through self-inductance and mutual inductance, and the characteristic is magnetic flux changing from top to bottom in a forward direction; if the sine wave of the current turn is complete and the change of the wavelength time constant is small, the electromagnetic property of the current symmetrical turn is complete; if the sine wave of the current turn is incomplete, the wavelength of the sine wave superposed with the front and the back is larger than a standard time constant, which shows that the current turn has defects, and has health hidden troubles such as deformation, oil stain, slot wedge looseness or displacement, early turn-to-turn short circuit and the like;

preferably, a positive circularly polarized unidirectional energy field and a negative circularly polarized unidirectional energy field which is deflected by 180 degrees are applied in the counterclockwise direction, symmetric acquisition and comparison are carried out, two circularly polarized waves with the same rotation direction are coupled with a counterclockwise circularly polarized wave waveform formed by the current turn, and magnetic flux which is reversely changed from bottom to top is represented; the defective turns can be repeatedly verified, and the positions of the defects on the positive and negative windings are judged.

Preferably, when the unit length of each turn of the rotor load is integral multiple of the wavelength of transmitting circularly polarized wave,

the measured rotor load is a dielectric material (ur ═ 1), and the attenuation constant and phase constant of the electromagnetic wave are known as follows:

wherein alpha is_sIs the decay constant; beta is a_sIs a phase constant; c is the vacuum light speed; f is the frequency of the generated electromagnetic wave; epsilon₀Is a free space dielectric constant of 10^-9/36πF/m；ε_rFor each turn of the winding the relative dielectric constant, e_r＝ε′_r-jε″_r，ε′_rIs the real part of the relative dielectric constant of each turn of winding, epsilon ″)_rRelative dielectric constant imaginary part of each turn of winding;

the wavelength of the circularly polarized wave in the rotor winding is:

wherein λ 0 ═ c/f is the free space wavelength of a circularly polarized wave; lambda [ alpha ]_sThe average wavelength of circular polarized waves in the rotor winding; when the circumference of the single turn rotor winding is an integer multiple of the wavelength 1/2 of the emitted electromagnetic wave, i.e.

Wherein n is a positive integer, the propagation coefficient T can be obtained²：

The propagation coefficient may truly reflect the internal impedance time constant.

Has the advantages that:

the invention can accurately measure the health condition of each turn of the rotor winding of the generator, judge whether the rotor winding of the generator has faults or not and judge whether the rotor winding of the generator has the fault trend or not, can accurately position the fault form and the fault position of the rotor on each turn of the rotor winding, is an important means for the nondestructive state detection of the whole life cycle of the rotor of the large-scale non-salient-pole turbonator, and can provide accurate and clear data and key evidences for each overhaul after the rotor is manufactured, shipped out of a factory and put into operation.

Description of the drawings:

FIG. 1 is a diagram of a circular polarized wave formed by a current turn that can be concurrently coupled out clockwise in time;

FIG. 2 is a circular polarized wave diagram of the cumulative feedback of a circular polarized wave waveform formed clockwise on each turn of a current coil;

FIG. 3 is a schematic diagram of a signal source structure;

FIG. 4 is a schematic diagram of operational amplifier, filter, acquisition, and control circuitry;

FIG. 5 is a schematic diagram of a clockwise circularly polarized wave;

FIG. 6 is a schematic diagram of a circularly polarized wave deflected 180 ° clockwise;

FIG. 7 is a schematic diagram of a counterclockwise circularly polarized wave;

FIG. 8 is a diagram illustrating an equivalent internal resistance inductive reactance time constant;

FIG. 9 is a schematic view of example 2;

FIG. 10 is a schematic view of example 2;

FIG. 11 is a schematic view of example 3;

FIG. 12 is a schematic view of example 4;

FIG. 13 is a schematic view of example 5;

FIG. 14 is a schematic view of example 6;

fig. 15 is a schematic diagram of the full speed 650MW rotor 1# coils and 2, 3, 4, 5, 6, 7, 8# coils of examples 2-4.

The specific implementation mode is as follows:

example 1

As shown in fig. 1-8, the apparatus for detecting turn-to-turn electromagnetic pulse vibration wave characteristics of a rotor winding of a turbo generator according to the present invention includes an ultra-large capacity internal resistance signal source, the ultra-large capacity internal resistance signal source is connected to an ultra-high speed time sequence control circuit, the ultra-high speed time sequence control circuit is connected to the positive and negative electrodes of the rotor winding through a parasitic inductive power supply via positive and negative load wave guide lines, and the positive and negative electrodes of the rotor winding are connected to an ultra-high speed acquisition circuit via an operational amplifier circuit.

The ultra-large capacity internal resistance signal source is matched with the circular polarization characteristic average time constant of each turn of winding and can generate the energy width of the power circular polarization characteristic wave matched with the whole-course response time constant of the rotor winding;

the parasitic inductive power supply performs circular waveguide coupling exchange on the input and output coupled circular polarized waves of the positive and negative poles;

the positive and negative load wave guide lines couple circularly polarized waves to the positive and negative poles of the rotor in parallel;

the operational amplifier circuit combines, couples and amplifies the signals transmitted and received by the concurrent circular polarization;

the ultrahigh-speed acquisition circuit acquires waveforms which are combined by circularly polarized dual-signal emission sources, induced polarization sources at each turn and circularly polarized waveguide loads formed by double-symmetrical combination and time constants for energy maintenance of signal sources.

The method comprises the steps that a super-large capacity internal resistance signal source and a super-high speed time sequence control circuit generate a high-order mutation electric field of an avalanche polarization edge, circularly polarized electromagnetic waves of 180 degrees are symmetrically deflected by a parasitic inductive power supply and are coupled to a positive electrode and a negative electrode of a rotor through positive and negative load wave guide lines in a clockwise or anticlockwise mode, a first positive electrode turn and a first negative electrode turn are mutually induced to generate a first sine wave, energy returns to the inductive parasitic power supply, and meanwhile, the energy is sequentially transmitted to a second turn; the parasitic inductive power supply and the second turn start circularly polarized feedback energy feedback; feeding back and overlapping each turn step by step in sequence; each coupling turn exhibits a sine wave with the same time constant.

When the time of positive circular polarization sending and negative electrode deflection 180 degrees for circular polarization sending one-way energy field is maintained clockwise and is simultaneously longer than the full-length wave guide time of the rotor winding, each turn of symmetrical winding presents a signal source and load superposed dual electromagnetic pulse vibration wave characteristic waveform, the circular polarization wave waveform formed by the current turn can be synchronously superposed and coupled in time through self-inductance and mutual inductance, and the characteristic is magnetic flux which is changed from top to bottom in a positive direction; if the sine wave of the current turn is complete and the change of the wavelength time constant is small, the electromagnetic property of the current symmetrical turn is complete; if the sine wave of the current turn is incomplete, the wavelength of the sine wave superposed with the front and the back is larger than a standard time constant, which shows that the current turn has defects, and has health hidden troubles such as deformation, oil stain, slot wedge looseness or displacement, early turn-to-turn short circuit and the like;

applying a positive circularly polarized unidirectional energy field and a negative circularly polarized unidirectional energy field which are deflected by 180 degrees in the counterclockwise direction, symmetrically acquiring and comparing, and coupling a counterclockwise circularly polarized wave waveform formed by the current turn by using two circularly polarized waves with the same rotation direction, wherein the waveform is characterized by magnetic flux which reversely changes from bottom to top; the defective turns can be repeatedly verified, and the positions of the defects on the positive and negative windings are judged.

When the unit length of each turn of the rotor load is integral multiple of the wavelength of transmitting the circularly polarized wave,

the measured rotor load is a dielectric material (ur ═ 1), and the attenuation constant and phase constant of the electromagnetic wave are known as follows:

wherein alpha is_sIs the decay constant; beta is a_sIs a phase constant; c is the vacuum light speed; f is the frequency of the generated electromagnetic wave; epsilon₀Is a free space dielectric constant of 10^-9/36πF/m；ε_rFor each turn of the winding the relative dielectric constant, e_r＝ε′_r-jε″_r，ε′_rIs the real part of the relative dielectric constant of each turn of winding, epsilon ″)_rRelative dielectric constant imaginary part of each turn of winding;

the wavelength of the circularly polarized wave in the rotor winding is:

wherein λ 0 ═ c/f is the free space wavelength of a circularly polarized wave; lambda [ alpha ]_sThe average wavelength of circular polarized waves in the rotor winding; when the circumference of the single turn rotor winding is an integer multiple of the wavelength 1/2 of the emitted electromagnetic wave, i.e.

Wherein n is a positive integer, the propagation coefficient T can be obtained²：

The propagation coefficient may truly reflect the internal impedance time constant.

The invention utilizes the principle that each circle of load coil matched with the circular waveguide is coupled with circularly polarized electromagnetic waves with the same time constant and has the signal source characteristic of transient pulse vibration waves for detection, since the time of the action of the unidirectionally varying magnetic flux formed in each turn has a high correlation with the time of the circularly polarized wave passing through the physical perimeter of each turn, it is formed that, when the circularly polarized wave reaches the second turn, part of the energy will return to the first turn, and similarly, part of the energy will return to the second turn and then to the first turn, namely, the total flux of the first turn is always kept unchanged, the total flux of the second turn is also kept unchanged, the signal emission source keeps the polarization direction of the circularly polarized wave unchanged, clockwise or counterclockwise, so that the first turn, the second turn and the third turn of the anode and the cathode can simultaneously keep the total flux which embodies the characteristics of the turn, and in turn, a forward inter-turn characteristic waveform of 62 turns (such as a 650MW full-speed rotor) in total can be obtained. As shown in fig. 1, the counter-clockwise circularly polarized waves are coupled to obtain an inverse inter-turn signature.

Example 2:

the positions of the gap bridge lines of the 1# coil and the 2# coil of the full-speed 650MW rotor are shown as A and a in FIG. 15;

as shown in FIG. 9, all 62 turns of a 1# full speed 650MW healthy rotor 1-8# coil are clearly visible. The gap bridge line characteristics of the coil No. 1 and the coil No. 2 are obvious, and the transient wave characteristics of each turn of the rotor are healthy.

As shown in FIG. 10, all 62 turns of a 2# full speed 650MW healthy rotor 1-8# coil are clearly visible. The gap bridge line characteristics of the coil No. 1 and the coil No. 2 are obvious, and the transient wave characteristics of each turn of the rotor are healthy.

Example 3:

the positions of the gap bridge lines of the 1# coil and the 2# coil of the full-speed 650MW rotor are shown as A and a in FIG. 15;

as shown in FIG. 11, all 62 turns of a 2# full speed 650MW sub-healthy rotor 1-8# coil are clearly visible except that the 1# coils 5, 6 are combined into 1 sine wave. The characteristics of the gap bridge lines of the 1# coil and the 2# coil are not obvious, the amplitude of the 1 and 2 turn sine waves of the 2# coil is too large relative to the amplitude of the last period, oil stains are judged to exist, and necessary cleaning work needs to be carried out.

Example 4:

the positions of the gap bridge lines of the 1# coil and the 2# coil of the full-speed 650MW rotor are shown as A and a in FIG. 15;

as shown in fig. 12, the transient wave characteristics of a certain 2# full speed 650MW rotor were compared for two major repairs. The light color is the waveform of each turn of the normal rotor, and the dark color is the waveform of each turn after oil stain is fed.

Description of the drawings: 1 st to 3 circles of the 1# coil are completely overlapped, 4 th to 5 th circles of the 1# coil are separated, 6 th circle of the 1# coil is completely disappeared, 1 st circle of the 2# coil has phase difference, and the 2 nd circle of the 2# coil starts until 8 th circle of the 8# coil and is normal. The oil stains can be analyzed to exist in the 5 and 6 turns of the 1# coil and the 1 turn of the 2# coil, the oil stains are located at the gap bridge line of the 1# coil and the 2# coil, and the post-overhaul processing result is verified and tested to be completely correct.

Example 5:

as shown in fig. 13, the results of the annual modified transient characteristics of a certain 2# full speed 390H rotor. The 1-5# coil is normal, and the 6# coil has winding deformation.

Example 6:

as shown in fig. 14, the results of the annual modified transient characteristics of a certain 2# full speed 390H rotor. 1-5#, 7-9# coil normal, 6# coil had winding distortion.