50 results about "Superconducting electric machine" patented technology

The invention discloses a liquid hydrogen high-temperature superconducting motor and magnetofluid dual-power propulsion system, and aims to solve the problems that an existing ship propulsion system is single in power mode and insufficient in power density. The system comprises a liquid hydrogen storage and supply unit, a cooling unit, an energy conversion unit, a superconducting motor propulsion unit and a magnetofluid propulsion unit, the liquid hydrogen storage and supply unit conveys liquid hydrogen to the superconducting part through the cooling loop, the liquid hydrogen is converted into hydrogen through the heat exchanger after being cooled, the energy conversion unit converts the hydrogen into electric energy and outputs the electric energy in a matched mode, and the superconducting motor propulsion unit and the magnetic fluid propulsion unit generate mechanical energy or electromagnetic force through the electric energy to drive a ship. And the superconducting component is cooled by the cooling loop. The liquid hydrogen in the system has the dual functions of a cooling medium and fuel, a coolant and fuel do not need to be additionally configured, the requirements for silence, high thrust and rapid maneuvering are met, the power density is high, the environmental protection property is good, and the system is suitable for high-performance propelling scenes such as ships, especially submarines.

The invention belongs to the technical field of superconducting motor testing, and particularly relates to a background magnetic field simulation and testing device for motor superconducting coil quench detection and electromagnetic characteristic analysis. The device comprises an outer stator iron core, an inner stator iron core, an open type or closed type low-temperature container with a built-in superconducting coil device, and a device bracket, wherein the outer stator iron core and the inner stator iron core are coaxially arranged; the outer stator is composed of an outer stator iron core and a multi-phase armature winding embedded in a tooth groove of the outer stator iron core. The inner stator iron core is composed of an even-number-pole iron core salient pole and a pole shoe, and an air gap is formed between the two; the low-temperature container can be of an open structure or a closed structure, and can be flexibly selected according to different test requirements; symmetrical alternating current is introduced into the multi-phase armature winding of the outer stator to simulate the background magnetic field environment of the superconducting coil in motor operation, effective verification and quantitative analysis of the quench characteristic and the electromagnetic performance of the superconducting coil are realized, related tests can be completed without manufacturing a prototype, the experiment cost is remarkably reduced, and the safety and the reliability are improved.

The application belongs to the technical field of superconducting motor testing, and more particularly relates to a background magnetic field simulation and testing device for superconducting coil quench detection and electromagnetic characteristic analysis of a motor. The device comprises coaxially arranged outer and inner stator cores, an open or closed cryogenic container with a built-in superconducting coil device, and a device support; the outer stator is composed of an outer stator core and multiphase armature windings embedded in the tooth slots of the outer stator core; the inner stator core is composed of an even-pole core salient pole and a pole shoe, and an air gap is formed between the two; the cryogenic container can be of an open structure or a closed structure, and can be flexibly selected according to different testing requirements; by passing a symmetric alternating current into the multiphase armature windings of the outer stator, the background magnetic field environment of the superconducting coil in the motor operation is simulated, effective verification and quantitative analysis of the superconducting coil quench characteristics and electromagnetic performance are realized, the related tests can be completed without manufacturing a prototype, and the experimental cost is significantly reduced, and the safety and reliability are improved.

This application discloses a rotor comprising a rotor housing, a rotor shaft, a rotor core, and rotor windings. The rotor forms three coaxially distributed zones: a normal temperature zone, a first low-temperature zone, and a second low-temperature zone. The first low-temperature zone is located between the normal temperature zone and the second low-temperature zone. The temperature of the first low-temperature zone is lower than that of the normal temperature zone, and the temperature of the second low-temperature zone is lower than that of the first low-temperature zone. The rotor shaft is located in the normal temperature zone, while the rotor core and rotor windings are located in the second low-temperature zone. The rotor windings include coil leads, each coil lead comprising a conductor and a Peltier unit. At least a portion of the Peltier unit is in close contact with the conductor. One end of the conductor is connected to the second low-temperature zone, and the other end of the conductor passes through the rotor housing to the outside of the rotor. This application also provides a superconducting motor. This application reduces heat leakage by employing a normal temperature shaft and a three-temperature zone structure within the rotor, while also incorporating Peltier units on the coil leads of the rotor windings.

The application relates to the technical field of superconducting motors, in particular to a superconducting magnet support framework, a superconducting motor and a use method. The superconducting magnet support framework comprises a framework body, the framework body is provided with a first flow channel, the first flow channel is suitable for flowing with a cooling medium, and the outer circumferential surface of the framework body is suitable for winding a superconducting coil; a cold conducting plate is arranged on the outer circumferential surface of the framework body, and the cold conducting plate is fixedly connected with the framework body. The application separates the structure for cooling the superconducting coil and supporting the superconducting coil of the superconducting motor, thereby reducing the compactness of the superconducting coil and the problem that the superconducting coil occupies a larger space in the superconducting motor, and the application provides the superconducting magnet support framework, the superconducting motor and the use method.

The invention belongs to the field of fan design, and particularly relates to a hydrogen combustion lift fan system which comprises a lift fan, a box type spray pipe, an output shaft, a main engine and a superconducting motor. The lift fan is coaxially and fixedly connected with the box type spray pipe, one end of the output shaft is connected with rotor blades of the lift fan, the other end of the output shaft is connected with the superconducting motor and the main engine, and the superconducting motor is coaxially arranged in the main engine. A liquid hydrogen tank is arranged on the outer side of the main engine, a rectifying support plate is arranged in the lift fan, and an ignition electric nozzle is arranged on a cartridge receiver of the lift fan; hydrogen in the liquid hydrogen tank can flow into the ignition electric nozzle after passing through the superconducting motor and the rectifying support plate, and is burnt and heated after ignition to generate thrust. The energy conversion mode of a traditional lift fan is optimized, the temperature of airflow behind the lift fan can be increased from 300 DEG C to 1000 DEG C or above, the lift amplification of the lift fan exceeds 150%, and the requirement of a power system for lift is met. According to the scheme, hydrogen for cooling the superconducting motor can be recycled.

This invention provides a method and apparatus for superconducting motor quench detection based on sliding time filtering, relating to the field of superconducting motor quench detection technology. The method includes: differentially processing the terminal voltage signals of adjacent superconducting rotor magnets in the superconducting motor; conducting three trial runs of the superconducting motor before quench detection to obtain interference frequency data; establishing sliding time windows with both long and short time scales during the actual operation of the superconducting motor, and performing notch filtering on the differential voltage signals of adjacent superconducting rotor magnets; performing linear regression fitting on the filtered signals within the sliding time windows to extract effective quench signal feature values; and establishing a quench protection criterion based on the quench feature values. This invention solves the problem of achieving high reliability and rapid response in quench detection technology under the complex interference environment of superconducting motor rotation operation, a problem that is difficult to address in existing technologies.

The invention relates to the technical field of vehicles, in particular to a liquid hydrogen energy management system and a vehicle. The liquid hydrogen energy management system comprises a liquid hydrogen tank, a superconducting coil system, a superconducting motor, a buffer tank, a fuel cell, a power cell and an integrated controller. A liquid hydrogen outlet of the liquid hydrogen tank is communicated with a first cooling working medium inlet of the superconducting coil system, a first cooling working medium outlet of the superconducting coil system is communicated with an inlet of the buffer tank, and an outlet of the buffer tank is communicated with a hydrogen inlet of the fuel cell. A high-voltage interface of the integrated controller is electrically connected with the superconducting coil system, the motor, the fuel cell and the power cell; and a low-voltage control interface of the integrated controller is in signal connection with the liquid hydrogen tank, the superconducting coil system, the motor, the buffer tank, the fuel cell and the power cell. According to the liquid hydrogen energy management system, the vaporization process of liquid hydrogen can be effectively utilized, the energy utilization rate is increased, and the endurance mileage of a vehicle is increased.

This invention relates to the field of superconducting motor technology, and in particular to a low-loss superconducting motor and its design method. The low-loss superconducting motor includes a vacuum chamber, a stator assembly, and a mover assembly. The stator assembly includes a stator support frame with a planar top structure and a superconducting coil disposed on the planar structure. A protective cover is disposed above the superconducting coil, and a radiative heat shield is disposed on the protective cover. The mover assembly is disposed between the protective cover and the radiative heat shield. The mover assembly includes a frame-shaped mover support frame and a constant conductor coil. The temperature of the constant conductor coil is controlled by controlling the emissivity of the radiative heat shield, and the surface emissivity of the protective cover is used to cool the constant conductor coil. The invention also discloses a design method based on a low-loss superconducting motor. The air gap between the stator assembly and the mover assembly is small, which facilitates the achievement of a high magnetic field, reduces the Joule loss of the constant conductor coil, eliminates the need for air or water cooling pipes, and facilitates temperature control.

The invention belongs to the related technical field of superconducting, and discloses an annular superconducting armature winding topological structure and a superconducting motor. The armature winding is a high-temperature superconducting coil, and the high-temperature superconducting coil is embedded into each stator groove in an annular winding structure. Compared with a conventional fractional slot concentrated winding, more winding phase distribution and slot potential distribution can be provided for the superconducting motor, and more design freedom degrees are achieved; the influence of the direction of a magnetic field acting on a winding strip on the performance reduction of the strip can be greatly reduced, and the performance bottleneck caused by high harmonic loss and low slot fullness rate of a traditional concentrated / distributed winding is greatly reduced; the technical problems of alternating current loss accumulation, poor superconducting state stability and insufficient mechanical reliability of the superconducting armature winding in the MW-level aviation motor are effectively solved.

This invention belongs to the technical field of superconducting motor quench detection, and more specifically, relates to a superconducting motor quench detection method based on terminal voltage differential and unsupervised autoencoder. The method includes: acquiring the terminal voltage signal of a superconducting magnet; suppressing induced voltage interference through moving average differential processing; and obtaining a preprocessed signal after filtering; inputting this signal into a pre-trained unsupervised autoencoder model, which consists of an encoder and a decoder. The encoder extracts deep features through a convolutional neural network, a bidirectional long short-term memory network, and an attention mechanism; the decoder performs sequence reconstruction; and by calculating the reconstruction error and comparing it with an adaptive threshold, the quench state is detected and located. This invention solves the problem that the quench judgment threshold often relies on empirical settings and is difficult to adapt to the complex and ever-changing dynamic operating conditions of the motor.

The invention discloses a low-temperature cooling system for a superconducting rotor of a superconducting motor, belongs to the field of superconducting motors, and aims to solve the problems that an existing refrigerant transmission device for the superconducting rotor of the superconducting motor is complex in structure and poor in sealing possibly. Comprising a rotor cooling shell, a cooling inner stator, a refrigerant inlet pipe and a refrigerant outlet pipe device. The rotor cooling shell, the cooling inner stator, the refrigerant inlet and outlet pipe and the refrigerant outlet pipe form a cooling loop, a refrigerant is pumped into the cooling loop through the low-temperature pump, the rotor cooling shell is cooled in a convective heat exchange mode, and then the rotor iron core and the superconducting magnet assembly are cooled in a conduction cooling mode. The refrigerant inlet pipe and the refrigerant outlet pipe are static, so that a low-temperature medium is prevented from flowing through the rotary sealing joint, the low-temperature cooling structure is simplified, and the reliability of the superconducting rotor is improved.

The invention discloses a low-temperature circulating cooling system for a magnetic suspension superconducting magnet, which relates to the technical field of magnetic suspension and is characterized in that a cooling device is arranged on the superconducting magnet, and a refrigerating machine is arranged on the side surface of the cooling device; a built-in superconducting motor is arranged in the cooling device, a superconducting motor stator and a superconducting motor rotor are borne in the built-in superconducting motor through bearings, and the superconducting motor stator and the superconducting motor rotor are matched with the built-in superconducting motor outer Dewar through a secondary condenser to achieve a concentric state; the rotor sealing cylinder is arranged between the superconducting motor rotor and the superconducting motor stator, and the rotor sealing cylinder is connected with a circulating gas inlet and a circulating gas outlet. Through the built-in superconducting motor, the problems of rotating shaft heat conduction and heat leakage, gas heat transfer, rotating shaft high-pressure sealing and the like due to the fact that a driving motor is externally arranged in a traditional low-temperature circulating system are solved. The mode that the magnetic suspension magnet can only be cooled through liquid helium filling is avoided, and the operation cost is saved.

A superconducting machine system includes a superconducting electrical machine. The superconducting machine system also includes a cryogenic vessel. The cryogenic vessel encompasses the superconducting electrical machine. The superconducting machine system further includes a vacuum vessel wall encompassing the cryogenic vessel. The superconducting machine system even further includes a cryocooler coupled to the vacuum vessel wall, wherein the cryocooler is configured to cool the superconducting electrical machine. The superconducting machine system still further includes a system configured, when the cryocooler is switched to a non-operative state, to remove helium gas from within a cryocooler housing to reduce a helium gas pressure within the cryocooler to minimize a parasitic heat load generated when the cryocooler is switched from an operative state to the non-operative state.

The application discloses a rotor, which comprises a rotor shell, a rotor shaft, a rotor core, a rotor winding and a cold medium transmission mechanism; the cold medium transmission mechanism comprises a rotating transmission assembly, a stationary transmission assembly and a magnetic fluid sealing assembly; the rotating transmission assembly is installed to one end of the rotor shaft; the stationary transmission assembly is rotationally connected to the rotating transmission assembly; the stationary transmission assembly forms a stationary input channel and a stationary output channel located outside the stationary input channel; the rotating transmission assembly forms a rotating input channel and a rotating output channel located outside the rotating input channel; and the magnetic fluid sealing assembly is located outside the stationary output channel or outside the rotating output channel to seal the gap between the stationary output channel and the rotating output channel. The application also discloses a superconducting motor. In the application, the normal-temperature rotor shaft is adopted, a three-temperature-zone structure is arranged in the rotor, and a sealing structure between the stationary transmission assembly and the rotating transmission assembly is arranged, so that the heat leakage is reduced.

The invention discloses an integrated superconducting aviation electric propulsion system, which belongs to the technical field of aviation electric propulsion and comprises a liquid hydrogen storage tank, a hydrogen supply balance module, a superconducting motor controller, a superconducting motor and a hydrogen fuel cell module. A power supply circuit assembly is arranged between the hydrogen fuel cell module and the superconducting motor, a liquid hydrogen flow path assembly is arranged between the liquid hydrogen storage tank and the superconducting motor, a hydrogen flow path assembly is arranged between the superconducting motor and the hydrogen supply balance module, and a fuel supply assembly is arranged between the hydrogen supply balance module and the hydrogen fuel cell module. And the hydrogen fuel cell module is also connected with an air supply assembly. According to the integrated superconductive aviation electric propulsion system, the cooling cost and complexity of the superconductive aviation electric propulsion system are reduced, the structure of a low-temperature system is simplified, and the problem of efficiency loss caused by separation design of an airborne liquid hydrogen energy system and a thermal management system is solved.

The invention discloses a preparation method of a lightweight high-stability MgB2 multi-core superconducting wire. The method comprises the following steps: 1, loading an Al2O3-Al rod into a Cu tube, and processing to obtain a reinforced core; 2, putting the Mg powder / rod and the B powder precursor into an Nb tube, putting the Nb tube into a Cu tube, and processing to obtain a single core wire; 3, inserting the reinforced core and the single-core wire into the composite sheath which is filled into the Al2O3-Al tube from the Monel tube to obtain a secondary composite tube body; 4, processing the secondary composite tube body into a wire rod; and 5, performing phase heat treatment on the wire. According to the invention, the low-density nano Al2O3 reinforced aluminum-based composite material is adopted to partially replace a high-density metal sheath and optimize the Al2O3-Al area proportion, so that the weight of the wire is reduced, and the electrical-thermal-mechanical comprehensive stability of the MgB2 superconducting wire is synergistically improved by utilizing the excellent mechanical, electrical and thermal conductivity of the composite material; and the requirements of light weight and high stability of the aviation-level superconducting motor are met.

The application discloses a preparation mold and a preparation method of a superconducting motor rotor magnet support structure, relates to the technical field of superconducting motors, and alternately winds glass fiber reinforced composite materials on an outer layer support boss of an outer layer support ring and on an inner layer support boss of an inner layer support ring, so as to form a support rod in an uncured state; the preparation mold comprises a curing mold and a positioning mold; the curing mold comprises a first support and a second support; the first support is used for being attached to the outer surface of the support rod in the uncured state; the second support is attached to the outer surface of the first support; the thermal expansion coefficient of the first support is greater than that of the second support; and the positioning mold is connected with the outer layer support ring and the inner layer support ring respectively. The support rod prepared by the preparation mold is continuous and complete in the internal fiber, the mechanical properties of the structure are improved, and the structural stability of the superconducting motor rotor is improved.

This invention discloses a harmonic magnetic field simulation device for testing the characteristics of superconducting magnets, relating to electrical and mechanical transmission equipment. It includes a support frame and a superconducting magnet module mounted on the support frame, a ferromagnetic tuning module mounted below the superconducting magnet module, and a magnetomotive force source module mounted below the ferromagnetic tuning module. An upper back iron is disposed above the superconducting magnet module. A first characteristic air gap exists between the superconducting magnet module and the ferromagnetic tuning module, and a second characteristic air gap exists between the ferromagnetic tuning module and the magnetomotive force source module. The ferromagnetic tuning module is mounted on a moving device. This invention can conveniently simulate the magnetic fields within different superconducting motors, making its principle intuitive, its applicability wide, and its simulated magnetic field closer to the actual magnetic field of the superconducting magnet. The experimental results are direct, facilitating research on the current-carrying capacity testing, loss analysis, and electromagnetic shielding analysis of superconducting magnets under specific magnetic field environments.

The application provides a decoupling type stator excited superconducting motor, which comprises a rear end cover, a front end cover and a casing; at least one superconducting excitation winding is arranged in the casing in an axial direction; two stator structures are arranged on the axial two sides of each superconducting excitation winding, and only one stator structure is arranged between any two adjacent superconducting excitation windings; a rotor structure is arranged on the inner side of each stator structure, and the rotor structure is connected with a rotating shaft which extends from the front end cover; the stator structure comprises a stator core and a stator winding, and the top of the stator tooth on the inner side of the stator core is provided with uniformly distributed magnetic adjustment grooves I; the rotor structure comprises a rotor core and a magnetic conducting block arranged between the two rotor structures, and the outer side of the rotor core is provided with uniformly distributed magnetic adjustment grooves II.

A superconducting motor includes a rotor holding permanent magnets and able to rotate about a longitudinal axis, a stator holding windings suitable for being powered in order to generate a magnetic field that rotates the rotor by virtue of the permanent magnets, and a motor housing. The motor housing has a plurality of compartments that are hermetic with respect to each other, each compartment enclosing one or more windings of the stator, each compartment being evacuated in order to form a thermal insulation barrier for the winding or windings enclosed in the compartment in question. As a result, any particles that might detach from a faulty winding do not damage the thermal insulation barrier of any other winding housed in another compartment.

The invention provides a semi-superconducting electric propulsion system model construction method, and belongs to the technical field of aviation electric propulsion, and the method specifically comprises the steps: building a semi-superconducting electric propulsion system dynamic mathematical sub-model comprising a shared rotor kinetic equation of a semi-superconducting motor and a ducted fan, quantifying the key coupling effect parameters and evaluating the influence of each key coupling effect parameter on the overall performance of the semi-superconducting electric propulsion system by a shared rotor kinetic equation of the semi-superconducting motor and the ducted fan; and a cold source flow controller sub-model is constructed, the cold source flow controller sub-model associates the heat dissipation amount in the dynamic mathematical sub-model with the heat exchange capacity of the heat exchanger in real time, and the cold source flow is dynamically predicted based on the current temperature field distribution and the real-time rotating speed instruction signal of the semi-superconducting motor. And dynamically adjusting the cold source flow according to the predicted cold source flow. According to the processing scheme, accurate modeling support is provided for optimization of the actual temperature control strategy of the semi-superconducting electric propulsion system.

The invention discloses a superconducting motor air gap winding inductance calculation method. The method comprises the steps that a plane polar coordinate system is established; determining a first radial coordinate and a first angular coordinate of the actual position of the first coil on the plane polar coordinate system; determining a first equivalent radial coordinate and a first equivalent angular coordinate of a first equivalent coil of the stator core corresponding to the first coil on the plane polar coordinate system; calculating the first self-excitation inductance of the first coil; calculating a second self-excitation inductance of the first equivalent coil based on the polar distance of the winding, the radius of the inner ring, the first radial coordinate, the first angular coordinate, and a second preset radial coordinate and a second preset angular coordinate of a second preset point on the planar polar coordinate system, and determining a separate excitation inductance of the stator core corresponding to the first coil based on the second self-excitation inductance; and determining the total self-inductance of the first coil based on the first self-excitation inductance and the separate-excitation inductance. Through the method, the calculation difficulty and the test cost of the winding self-inductance are reduced, and the calculation efficiency and the test efficiency are improved.

The application discloses a superconducting motor fault-tolerant control method and system considering quench faults, and belongs to the field of motor control. The method obtains a rotor flux estimation value by using a rotor flux estimation model according to a voltage control vector and a response current vector; if it is determined that a superconducting motor has occurred a quench fault, the method obtains a state current observation value of the superconducting motor under the quench fault by using a state current observation model according to the rotor flux estimation value and the response current vector; the method determines a voltage control vector of the superconducting motor under the quench fault by using a fault-tolerant control model according to a given current vector, the state current observation value of the superconducting motor under the quench fault and the response current vector; and the method applies the voltage control vector to the superconducting motor, so that the response current vector of the superconducting motor under the quench fault is equal to the given current vector. The application can effectively solve the robustness control problem of the superconducting motor when the quench fault occurs, and realizes stable operation of the superconducting motor.

A superconducting motor system includes a stator and one or more rotors inside the stator. The rotors may form a plurality of poles, and may rotate when a current is applied thereto. The one or more rotors include: a superconductor winding portion for each pole and in which superconductor coils are wound to form at least two layers; a power supply portion configured to supply a current to the superconductor winding portion; and a resistor portion connecting the superconductor winding portion at least partly in parallel to the power supply portion. the resistor portion enables different currents to be able to flow through the at least two layers of the superconductor winding portion.

The present invention discloses a superconducting motor quench detection method and apparatus based on rotational symmetry of a motor, belonging to the technical field of superconducting motor quench detection. The method includes: acquiring terminal voltages of each group of superconducting magnets in a superconducting motor, where the superconducting motor is pre-divided into at least two unit motors by using the rotational symmetry of the motor, and superconducting magnets located at corresponding positions are selected from the at least two unit motors as a group of superconducting magnets; calculating an absolute value of a terminal voltage difference of each group of superconducting magnets; and judging whether the absolute value exceeds a preset threshold, and if the absolute value exceeds the preset threshold, determining that the superconducting magnets are in a quench state. According to the present invention, induced voltages coupled by the terminal voltages of superconducting magnets are eliminated.

A lightweight, multilayer cryogenic insulator is formed by successive layers of low-emissivity sheeting and a separating truss-structure operating to resist circumferential deflection of the low-emissivity sheeting.