14 results about "Magnetic mirror" patented technology

The application discloses a kind of conic cavity electric charge traction collision centrifugal mirror nuclear fusion device, including pressure-bearing cavity (1), gas inlet system (2), gas outlet system (3), main magnetic mirror confinement system (4) and main pulse driving system (5);The pressure-bearing cavity includes the collision cavity in the middle, and the conic cavity is separately arranged at the axial both ends of the end face of collision cavity;The conic cavity and collision cavity are jointly defined by confinement interface, the shrink end of conic cavity is towards the center of pressure-bearing cavity, and the shrink end is provided with spout, and the spout of both ends of conic cavity is oppositely arranged;Conic cavity and collision cavity are sealed and connected, and they jointly form integrated pressure-bearing cavity, and form the spiral flow working cavity that is interconnected in the inside;The gas inlet system injects fusion working substance into the spiral flow working cavity and forms one-way annular centrifugal spiral flow layer, so that the cavity is formed with near-wall high-pressure area and low-pressure cavity area in radial direction.The device has the characteristics of simplified structure, low cost, good stability and high confinement efficiency.

A nuclear fusion reactor includes a first confinement element having axial ends, which define an inner region configured to have a first plasma population disposed therein and produces an axial magnetic field between the axial ends, the axial magnetic field configured to confine the first plasma population in the radial direction, and generate a magnetic mirror effect to confine the first plasma population in an axial direction at axial ends. Second and third confinement elements are disposed outside the first confinement element proximate to corresponding axial ends, and have a second and third plasma population disposed therein, respectively. The second and third plasma populations generate electrostatic barriers at the corresponding axial ends, to form a tandem mirror further confining the first plasma population in the inner region along the axial direction.

The invention discloses a biphase magnetic mirror offset frequency laser gyroscope system, and belongs to the technical field of precise laser gyroscopes. The two gyroscopes are arranged in parallel, each gyroscope comprises a gyroscope cavity and an alternating-current phototube assembly which is arranged on the gyroscope cavity and used for outputting demodulation, and the alternating-current phototube assemblies output two A / B signals with the phase difference of 90 degrees; two magnetic mirror offset frequency assemblies; the double-phase magnetic field control circuit is used for controlling the two magnetic mirror offset frequency assemblies to generate an orthogonally changing magnetic field so as to generate an offset frequency effect on light; and the signal demodulation systems are respectively used for receiving four paths of A / B signals from the two alternating-current photoelectric tube assemblies, respectively acquiring steering pulse signals of the two gyroscopes according to the A / B signals, and eliminating a lock region by crosswise splicing the steering pulse signals. According to the invention, the problems of test precision and the like of multiple types of laser gyroscopes are solved, the negative influence of the lock region on the laser gyroscope is reduced, and the accuracy and sensitivity of the laser gyroscope are improved.

A magnetic mirror dipole field fusion device comprises an excitation ring and two magnetic compression superconductors; and the magnetic compression superconductors are arranged at north and south poles of a dipole field, and a rotating shaft of the magnetic compression superconductor is coaxial with the excitation ring. A cross section of an excitation ring made of a normal temperature material is a circle or a square, and an excitation ring made of a superconducting material is a cylinder. A gap between the excitation ring and the magnetic compression superconductor is a magnetic mirror region, and a region outside the excitation ring is a fusion region. The magnetic mirror region has a very high magnetic field, and can reflect high-energy helium ions generated by fusion. The dipole field adopting a superconducting magnetic field compressor can cancel a levitated coil, and reduce a development difficulty and construction and operation costs.

A transverse magnetic field configuration optical system for a high magnetic field Fourier transform infrared (HFT) spectrometer includes a tubular sample cavity containing a solenoid superconducting magnet for the HFT spectrometer, and a non-magnetic damping sleeve housed within the tubular sample cavity. The upper part of the non-magnetic damping sleeve houses a non-magnetic mirror-plated gold-coated optical waveguide, and the lower part houses a transverse magnetic field configuration optical module. The transverse magnetic field configuration optical module contains an adjustable sample support stage, which is connected to a decelerated stepper motor outside the transverse magnetic field configuration optical system. The non-magnetic mirror-plated gold-coated optical waveguide includes an input waveguide for the probe light and an output waveguide for the signal light. The transverse magnetic field configuration optical module comprises a transverse magnetic field configuration reflection module and a transverse magnetic field configuration transmission module, respectively adapted to different HFT Fourier transform infrared spectroscopy measurement requirements. This invention proposes an optical system capable of realizing transverse magnetic field configuration magnetic spectroscopy measurements.

A nuclear fusion reactor includes a first confinement element having axial ends, which define an inner region configured to have a first plasma population disposed therein and produces an axial magnetic field between the axial ends, the axial magnetic field configured to confine the first plasma population in the radial direction, and generate a magnetic mirror effect to confine the first plasma population in an axial direction at axial ends. Second and third confinement elements are disposed outside the first confinement element proximate to corresponding axial ends, and have a second and third plasma population disposed therein, respectively. The second and third plasma populations generate electrostatic barriers at the corresponding axial ends, to form a tandem mirror further confining the first plasma population in the inner region along the axial direction.

The application relates to the technical field of plasma generating devices, in particular to an atmospheric pressure magnetic mirror constraint type stable plasma generating device and a control method, which comprises a high-voltage pulse power supply and a matched radio frequency power supply, a pair of discharge electrodes, two annular neodymium-iron-boron permanent magnets and a radio frequency coil; the two annular neodymium-iron-boron permanent magnets are parallel, coaxial, same-pole and opposite; and the arrangement is N-N / S-S. The application utilizes the Lorentz force to make the plasma discharge channel through the accurate proportioning of the electric field and the magnetic field, avoids the formation of electric arc due to continuous discharge, can automatically close the plasma ball into a spherical shape through linear regulation and control of the equivalent diameter of the plasma ball by adjusting the pulse width of the high-voltage pulse, solves the problems of open plasma and irregularity of a traditional device, greatly improves the plasma constraint stability, can realize accurate physical phenomenon observation, is composed of only the high-voltage pulse power supply and the matched radio frequency power supply, the discharge electrodes and the two annular permanent magnets, has no complex parts, and the part mounting mode is simple.

The application provides an external discharge Hall thruster with a planar shearing magnetic field design, which comprises a thruster structure body, an outer ring magnet, a thruster ceramic wall, an additional anode, an outer magnet, a magnetic screen, an anode, a ceramic structure body, an inner magnet, a short insulating pad, an M2 flat washer, an M2 elastic washer, an M2 nut, a long insulating pad, an M3 flat washer, an M3 elastic washer and an M3 nut. The application increases permanent magnets outside the additional anode to form a new magnetic mirror field to confine electrons, reduces the current of the additional anode, adjusts the magnetic field near the surface of the anode to make the positive gradient magnetic field on the surface of the anode, weakens the bombardment and heating of the electrons during the operation of the anode, improves the heating of the thruster and the demagnetization of the permanent magnet, increases the insulation between the anode and the additional anode, and improves the service life and reliability of the thruster.

The utility model relates to an adjustable magnetic lens bracket, which comprises a base and a lens mounting frame, the base comprises a supporting part and a mounting part, and the lens mounting frame is mounted on the mounting part of the base; the lens is mounted in the lens mounting frame; an adjustable fine thread bolt is arranged on the mounting part of the base, and the head of the adjustable fine thread bolt abuts against the lens mounting frame; the first surface of the lens mounting frame and the second surface of the mounting part are both provided with magnets, and the first surface and the second surface are attracted through the magnets. Compared with the prior art, the utility model has the advantages of simple structure and small volume, can be embedded into the limited space in a precise optical instrument and the like, does not influence the layout of other modules, and is especially suitable for scientific research imaging equipment or industrial optical path systems with high precision, high integration and compact structure.

The application provides an open magnetic plasma thermoelectric conversion and kinetic energy conversion regulation device, which is composed of a magnetic plasma channel, a front-stage regulation coil, a plasma probe group, a magnet array, a thermoelectric conversion channel, a magnetic shield plate, an acceleration coil and a rear-stage regulation coil. The device generates a dynamic magnetic field to transport high-temperature magnetic plasma through an excitation coil array, carries out plasma distribution regulation based on the measurement results of the plasma probe, obtains a magnetic plasma induced electromotive force by using a horizontal magnetic field and a tilted electrode, and realizes thermoelectric conversion with the magnetic plasma as a working medium. Meanwhile, the high-temperature magnetic plasma is accelerated by using a magnetic mirror structure to realize secondary conversion of the magnetic plasma heat energy, and a high-speed plasma jet flow is generated to produce a reaction thrust, thereby providing space power for a spacecraft. The application has the advantages of simple thermoelectric conversion process, no mechanical pump conveying structure and integration of the thermoelectric conversion and the space propulsion device.

The utility model relates to the technical field of ion source auxiliary coating, in particular to a novel durable anode ion source which comprises a base, an anode is arranged on the base, a cooling structure matched with the anode is arranged on the base, an electricity leading part is arranged on the cooling structure, and the cooling structure is externally connected with a power supply device through the electricity leading part. An inner cathode and an outer cathode are arranged on the base, a gas distribution structure is further arranged on the base, the gas distribution structure is externally connected with a gas supply device, magnetic steel is arranged on the outer wall of the supporting part, and the magnetic mirror ratio of a discharge cavity magnetic field formed by the inner cathode, the outer cathode and the anode is high. According to the technical scheme, electrons can be effectively gathered at the open end of a discharge cavity formed by the inner cathode, the outer cathode and the anode, namely in an ion emitting channel, so that collision of ions on the side walls of the inner cathode and the outer cathode is effectively reduced, sputtering pollution is reduced, and powder and cut pollutants generated in the using process cannot be accumulated on the outer cathode and the anode.

The magnetic mirror device (200) comprises a first inner coil (104) arranged to conduct current in a first direction, and a second inner coil (105) axially offset from the first inner coil (104) and arranged to conduct current in a second direction opposite the first direction. The mirror device (200) further comprises a first outer coil (210) positioned radially outward of the first inner coil (104) and arranged to conduct current in the second direction, and a second outer coil (212) positioned radially outward of the second inner coil (105) and arranged to conduct current in the first direction.

A magnetic confinement system includes a magnetic mirror device that includes a chamber to hold a target plasma and a coil arrangement to generate a magnetic field configuration in the chamber to confine the target plasma in cylindrically-symmetric form in the chamber, the magnetic field configuration having open ends. The magnetic confinement system further includes plasma guns to generate plasma pistons and project the plasma pistons at the open ends of the magnetic field configuration. In operation, the plasma pistons converge towards each other to close the open ends of the magnetic field configuration and to compress and heat the target plasma.

This invention provides an active electron microscope demagnetization method, apparatus, and system based on FFT harmonic suppression feedback. The method includes the following steps: acquiring real-time time-domain signals of interfering magnetic fields along the X, Y, and Z axes to obtain three-axis discrete-time sequences; performing Fast Fourier Transform (FFT) on each of the three-axis discrete-time sequences to convert the signals from the time domain to the frequency domain, obtaining three-axis frequency-domain signals; decomposing the corresponding time-domain signals into at least six harmonic components based on the three-axis frequency-domain signals, and extracting the amplitude and phase parameters of each harmonic component; generating a compensation signal with the same amplitude but opposite direction to the interfering magnetic field based on the amplitude and phase parameters of each harmonic component; and determining the driving current required to drive the three-axis coils through a constant current source based on the compensation signal, so as to generate a dynamic compensation magnetic field with the same amplitude but opposite direction to the spatial magnetic field in real time. This invention enables real-time acquisition, frequency-domain analysis, and precise cancellation of environmental magnetic fields.