The small-current grounding fault in distribution network is hard to be located because of its weak fault features.To accurately locate the faults,the transient process is analyzed in this paper.Through the study we t...The small-current grounding fault in distribution network is hard to be located because of its weak fault features.To accurately locate the faults,the transient process is analyzed in this paper.Through the study we take that the main resonant frequency and its corresponding component is related to the fault distance.Based on this,a fault location method based on double-end wavelet energy ratio at the scale corresponding to the main resonant frequency is proposed.And back propagation neural network(BPNN)is selected to fit the non-linear relationship between the wavelet energy ratio and fault distance.The performance of this proposed method has been verified in different scenarios of a simulation model in PSCAD/EMTDC.展开更多
The refraction index of the quantized lossy composite right-left handed transmission line（CRLH-TL） is deduced in the thermal coherence state. The results show that the negative refraction index（herein the left-hand...The refraction index of the quantized lossy composite right-left handed transmission line（CRLH-TL） is deduced in the thermal coherence state. The results show that the negative refraction index（herein the left-handedness） can be implemented by the electric circuit dissipative factors（i.e., the resistances R and conductances G） in a higher frequency band（1.446 GHz≤ ω ≤ 15 GHz）, and flexibly adjusted by the left-handed circuit components（Cl, Ll） and the right-handed circuit components（Cr, Lr） at a lower frequency（ω = 0.995 GHz）. The flexible adjustment for left-handedness in a wider bandwidth will be significant for the microscale circuit design of the CRLH-TL and may make the theoretical preparation for its compact applications.展开更多
The construction of major marine infrastructure projects and the exploration and development of deep-sea mineral resources require fine imaging of seabed strata and structures.The highresolution marine seismic explora...The construction of major marine infrastructure projects and the exploration and development of deep-sea mineral resources require fine imaging of seabed strata and structures.The highresolution marine seismic exploration based on a high broadband sparker source is an important approach to reveal seabed stratum and reservoir structure,and identify geohazard.To optimize the performance of sparker seismic source,we investigated the electro-acoustic characteristics of spark discharge under conditions of different charging voltages and electrode numbers.Results show that the sound source level increased with the increase of the charging voltage,whereas the main frequency decreased when the charging voltage increases.In addition,it was found that the charging capacitance had more obvious influence on the main frequency than the sound source level did.Although the load energy decreased with increasing electrode number,the sound source level still increased but the main frequency decreased.Meanwhile,the primary to bubble(P/B)ratio increased with the increase of the electrode number.To gain a deeper insight into the electro-acoustic characteristics,we investigate the relationship between sound source level and power peak,from which a good correlation was observed.A more practical statistical analysis on the rise rate of current was processed,and a perfect logarithmic function was derived.Furthermore,we found that the main frequency was most possibly subjected to the electrical energy,especially the charging energy per electrode.The results indicate that the charging energy per electrode less than 10 J could increase the main frequency to above 300 Hz.At last,the main frequency could be reduced to 20 Hz when the charging energy of a single-electrode discharge was enhanced to over 4 kJ.This study shall be helpful in developing a sparker seismic source and improving the performance for marine engineering exploration and geohazard assessment.展开更多
To date,no experimental study has been done on eliminating the energy consumption of the flapping wing rotor(FWR;caused by inertial force)based on an energy capture mechanism(such as a spring).Also,the effect of the v...To date,no experimental study has been done on eliminating the energy consumption of the flapping wing rotor(FWR;caused by inertial force)based on an energy capture mechanism(such as a spring).Also,the effect of the variation amplitude of the twist angles on the FWR remains unknown.In this study,a 19.2-g FWR model is designed and manufactured.Three different kinds of springs are then selected and assembled onto the FWR to reduce the energy consumption caused by the inertial forces.Afterward,a motion capture system and a lift measurement system are built to test the aerodynamic and kinematic performance of the FWR.Then,the influence of the variation range of the twist angles and the dimensions of the spring on the motion parameters and lift efficiency of the FWR is analyzed.If the rigid twist angle variation range is set to 10°–70°instead of 10°–50°,the FWR can generate 3 to 10 g of greater average lifts under the same input voltage.In most cases,the introduction of the spring also improves the average lifting rate by 1-4 g.The lift enhancement effect induced by the spring is more pronounced when the main frequency with the maximum amplitude is close to or coincides with the resonant frequency of the FWR structure.If the main frequency is greater than the resonance frequency of the FWR structure,the lift enhancement effect is hardly observed.In conclusion,according to experimental analyses,both the selection of 10°-70°preset twist angles and the application of springs can improve the lift efficiency of FWR and overcome the weight of the FWR system(37.8 g)assembled with a flight control system.Free-flight test results show that the FWR system(including the 19.2-g FWR model and an 18.6-g flight control system)has sufficient lifting margin to successfully perform a take-off mission and achieve a stable hovering action.展开更多
基金supported by National Key R&D Program of China(2017YFB0902800)Science and 333 Technology Project of State Grid Corporation of China(52094017003D).
文摘The small-current grounding fault in distribution network is hard to be located because of its weak fault features.To accurately locate the faults,the transient process is analyzed in this paper.Through the study we take that the main resonant frequency and its corresponding component is related to the fault distance.Based on this,a fault location method based on double-end wavelet energy ratio at the scale corresponding to the main resonant frequency is proposed.And back propagation neural network(BPNN)is selected to fit the non-linear relationship between the wavelet energy ratio and fault distance.The performance of this proposed method has been verified in different scenarios of a simulation model in PSCAD/EMTDC.
基金supported by the National Natural Science Foundation of China(Grant Nos.61205205 and 6156508508)the General Program of Yunnan Provincial Applied Basic Research Project,China(Grant No.2016FB009)the Foundation for Personnel Training Projects of Yunnan Province,China(Grant No.KKSY201207068)
文摘The refraction index of the quantized lossy composite right-left handed transmission line（CRLH-TL） is deduced in the thermal coherence state. The results show that the negative refraction index（herein the left-handedness） can be implemented by the electric circuit dissipative factors（i.e., the resistances R and conductances G） in a higher frequency band（1.446 GHz≤ ω ≤ 15 GHz）, and flexibly adjusted by the left-handed circuit components（Cl, Ll） and the right-handed circuit components（Cr, Lr） at a lower frequency（ω = 0.995 GHz）. The flexible adjustment for left-handedness in a wider bandwidth will be significant for the microscale circuit design of the CRLH-TL and may make the theoretical preparation for its compact applications.
基金Supported by the National Natural Science Foundation of China(No.42276195)the Natural Science Foundation of Zhejiang Province(No.LQ22D060006)the Science Foundation of Zhejiang Sci-Tech University(No.21022092-Y)。
文摘The construction of major marine infrastructure projects and the exploration and development of deep-sea mineral resources require fine imaging of seabed strata and structures.The highresolution marine seismic exploration based on a high broadband sparker source is an important approach to reveal seabed stratum and reservoir structure,and identify geohazard.To optimize the performance of sparker seismic source,we investigated the electro-acoustic characteristics of spark discharge under conditions of different charging voltages and electrode numbers.Results show that the sound source level increased with the increase of the charging voltage,whereas the main frequency decreased when the charging voltage increases.In addition,it was found that the charging capacitance had more obvious influence on the main frequency than the sound source level did.Although the load energy decreased with increasing electrode number,the sound source level still increased but the main frequency decreased.Meanwhile,the primary to bubble(P/B)ratio increased with the increase of the electrode number.To gain a deeper insight into the electro-acoustic characteristics,we investigate the relationship between sound source level and power peak,from which a good correlation was observed.A more practical statistical analysis on the rise rate of current was processed,and a perfect logarithmic function was derived.Furthermore,we found that the main frequency was most possibly subjected to the electrical energy,especially the charging energy per electrode.The results indicate that the charging energy per electrode less than 10 J could increase the main frequency to above 300 Hz.At last,the main frequency could be reduced to 20 Hz when the charging energy of a single-electrode discharge was enhanced to over 4 kJ.This study shall be helpful in developing a sparker seismic source and improving the performance for marine engineering exploration and geohazard assessment.
基金supported by the Natural Science Foundation of Zhejiang Province(Grant No.LQ22A020006)the National Natural Science Foundation of China(Grant No.52105285)+3 种基金the Aeronautical Science Foundation Program(Grant No.ASFC-20230023052001)China Postdoctoral Science Foundation(Grant No.2024M754237)Science and Technology Project of Jiangxi Education Department(Grant No.GJJ200452)Basic Public Welfare Research Program of Wenzhou(Grant No.G2023046)。
文摘To date,no experimental study has been done on eliminating the energy consumption of the flapping wing rotor(FWR;caused by inertial force)based on an energy capture mechanism(such as a spring).Also,the effect of the variation amplitude of the twist angles on the FWR remains unknown.In this study,a 19.2-g FWR model is designed and manufactured.Three different kinds of springs are then selected and assembled onto the FWR to reduce the energy consumption caused by the inertial forces.Afterward,a motion capture system and a lift measurement system are built to test the aerodynamic and kinematic performance of the FWR.Then,the influence of the variation range of the twist angles and the dimensions of the spring on the motion parameters and lift efficiency of the FWR is analyzed.If the rigid twist angle variation range is set to 10°–70°instead of 10°–50°,the FWR can generate 3 to 10 g of greater average lifts under the same input voltage.In most cases,the introduction of the spring also improves the average lifting rate by 1-4 g.The lift enhancement effect induced by the spring is more pronounced when the main frequency with the maximum amplitude is close to or coincides with the resonant frequency of the FWR structure.If the main frequency is greater than the resonance frequency of the FWR structure,the lift enhancement effect is hardly observed.In conclusion,according to experimental analyses,both the selection of 10°-70°preset twist angles and the application of springs can improve the lift efficiency of FWR and overcome the weight of the FWR system(37.8 g)assembled with a flight control system.Free-flight test results show that the FWR system(including the 19.2-g FWR model and an 18.6-g flight control system)has sufficient lifting margin to successfully perform a take-off mission and achieve a stable hovering action.
