19 results about "Annular field" patented technology

The present invention provides a multi-degree-of-freedom conductor depositing system for tokamak toroidal field coil winding packs, belongs to the field of development of toroidal field superconducting coils for nuclear fusion. The multi-degree-of-freedom conductor depositing system is mounted on a winding table and distributed along the contour of the toroidal field coil. The optical proximity switches detect the position signals between the winding table and the bending unit and transmit them to an automatic control system. The multi-degree-of-freedom conductor depositing system is distributed in a spiral shape from the top to the bottom from the position of the bending unit along the direction of coil winding. The conductor is deposited onto the track drive mechanism of the multi-degree-of-freedom conductor depositing device, which has a bidirectional moving and rotating function. This avoids the risk of insulation rupture due to friction between the conductor and the depositing tooling during the coil winding process. It also has the advantages of simple structure, convenient operation and high reliability.

The invention relates to the technical field of tokamak device parts, in particular to a supporting system for a polar field coil in a tokamak device. Comprising a toroidal field coil, two first polar field coils, two second polar field coils, two third polar field coils, two first supporting assemblies, two second supporting assemblies and a third supporting assembly, one first supporting assembly is used for fixedly connecting the top end of the toroidal field coil with one first polar field coil, and the other first supporting assembly is used for fixedly connecting the top end of the third polar field coil. And the other first supporting assembly is used for fixedly connecting the bottom end of the annular field coil and the other first polar field coil. Wherein one second supporting assembly is used for fixedly connecting the upper part of the toroidal field coil and one second polar field coil, and the other second supporting assembly is used for fixedly connecting the lower part of the toroidal field coil and the other second polar field coil. And the third supporting assembly is used for fixedly connecting the middle part of the annular field coil and the two third polar field coils.

The invention relates to the technical field of Tokamak nuclear fusion, and discloses an assembling method of a pre-assembled assembly of a nuclear fusion device and an installing method of the nuclear fusion device. The pre-assembled assembly comprises a vacuum chamber, a window neck tube in the vacuum chamber, a vacuum chamber cold shield and a TF magnet; the assembling method of the nuclear fusion device preassembled assembly comprises the following steps: supporting between a cold shield inner sector and a vacuum chamber through a first tool; a first tool is supported between the cold shield outer sector and the vacuum chamber; the TF magnet is connected with the middle window position of the vacuum chamber through a second tool, the upper arc-shaped section of the outer fan section of the cold shield is connected with the hoisting tool of the TF magnet through a third tool, and the lower window section of the outer fan section of the cold shield is connected with the second tool; and the middle window section and the annular field magnet supporting seat are connected through a fourth tool. According to the assembling method of the nuclear fusion device pre-assembled assembly, interference among installation of the vacuum chamber, the window neck tube in the vacuum chamber, the vacuum chamber cold shield and the TF magnet can be avoided, and the stability and functionality of the pre-assembled assembly structure are guaranteed.

The invention discloses a tool for a toroidal field magnet set for a nuclear fusion device, belonging to a toroidal field magnet set tool, wherein the fixed tool comprises an annular guide rail coaxially mounted on the inner wall of a host hall, the annular guide rail is coaxially arranged with a central column erected in the host hall, a plurality of vacuum chamber hangers with one end mounted on the inner wall of the host hall are arranged in an inner annular array of the annular guide rail, the bottom end of the vacuum chamber hanger is used to hang the vacuum chamber sector to the corresponding welding assembly position; a radial beam arranged radially along the annular guide rail is also provided above the vacuum chamber hanger, one end of the radial beam is rotatably mounted in the top bearing of the central column, and the other end is mounted on the annular guide rail through a tail drive system, and can move in a circle along the top surface of the annular guide rail with the center of the central column, so that the toroidal field magnet hoisted below the radial beam is sleeved on the outside of the corresponding vacuum chamber sector. The invention can greatly improve the assembly efficiency and positioning accuracy of the toroidal field magnet of the nuclear fusion device.

The application discloses a spaceborne near-space horizontal two-dimensional wind field interferometer based on a ring-shaped field of view and a full-link simulation method, the imaging instrument comprises an optical system, a detector and a data processing unit, the optical system comprises, in sequence along an optical path, a front cone mirror, a field of view diaphragm, a collimating lens group, a Fabry-Perot interferometer, a narrow-band filter assembly and an imaging lens; and the application improves the time-space resolution of instrument detection.

A gasket arrangement (G) for sealing between two corrugated heat transfer plates (5) is provided. The gasket arrangement (G) includes an annular field gasket portion (41) surrounding a field gasket region (A1) and a plurality of annular ring gasket portions (47c, 47d, 47e, 47f) arranged outside the field gasket region (A1). Each of the plurality of annular ring gasket portions (47c, 47d, 47e, 47f) surrounds an annular gasket region (A2), the annular gasket region (A2) being smaller than the field gasket region (A1) and extending in a central extending plane (p2) of the annular gasket portions (47c, 47d, 47e, 47f). The third annular gasket portion (47c) and the fourth annular gasket portion (47d) of the plurality of annular ring gasket portions (47c, 47d, 47e, 47f) are arranged on opposite sides of the transverse central axis (T1) of the field gasket region (A1). The gasket arrangement (G) is characterized in that the fifth annular gasket portion (47e) of the plurality of annular gasket portions (47c, 47d, 47e, 47f) is arranged on the same side of the transverse central axis (T1) as the third annular gasket portion (47c). Furthermore, the third annular gasket portion (47c) and the fifth annular gasket portion (47e) are arranged on opposite sides of the longitudinal central axis (L1) of the field gasket region (A1). Moreover, the longitudinal central axis (L1) of the field gasket region (A1) extends through one of the plurality of annular gasket portions (47c, 47d, 47e, 47f).

Adjustable aperture (100) for a projection exposure system (1), comprising a support element (102), and several aperture elements (104) movably attached to the carrier element (102) and fixable in an end position (Pe1), wherein the adjustable aperture (100) is configured to move several or all of the aperture elements (104) from an initial position (Pa) to the final position (Pe1) such that the aperture elements (104) together form an inner contour (K1) which corresponds to a predetermined beam cross-sectional shape (Q3) of a working light (16) of the projection exposure system (1), and wherein the predetermined cross-sectional beam shape (Q3, Q6) has a superellipse shape (Q3) and / or an annular field shape (Q6).

A lidar, a mobile system and a laser detection method. The lidar comprises: a rotating platform (10), at least two transceiver modules (11) fixed on the rotating platform (10), and a driving module configured to drive the rotating platform (10) to rotate about an axis of rotation (L) as a center, wherein each transceiver module (11) comprises a transmitting assembly configured to emit at least two laser beams having different exit angles, and a receiving assembly configured to receive echo signals of the emitted laser beams that are reflected by an object; the at least two transceiver modules (11) are arranged around the axis of rotation (L); the field-of-view ranges of at least two detection modules in a direction perpendicular to the axis of rotation (L) are staggered; and at least two annular field-of-view ranges respectively formed by the at least two transceiver modules (11) during rotation are stitched to form a larger annular field-of-view range. The lidar is low in terms of costs and can flexibly form different field-of-view ranges.

The problem addressed by the present invention is to provide a power generation device having a structure capable of suppressing a burden of winding work and a cost burden, and also suitable for enlargement. The power generation device according to the present invention is characterized by comprising a force-receiving rotor that rotates when receiving a fluid force, a shaft base part that rotates in conjunction with the rotation of the force-receiving rotor, and a generator that generates power by means of the rotational force of the shaft base part, and is characterized in that: the power generator is provided with a rotor disposed so as to rotate together with the shaft base part on the outer side of the shaft base part around a shaft, a stator disposed on the outer side of the shaft base part around the shaft so as not to rotate together with the shaft base part, and an excitation body disposed on the outer side of the shaft base part around the shaft so as not to rotate together with the shaft base part; the rotor is provided with a rotor base that is fixed to the shaft base part and rotates together with the shaft base part, and a plurality of magnetic pole cores that are arranged annularly on the rotor base; and the excitation body is provided with an annular field coil that excites the magnetic pole core.

A gasket arrangement (G) for sealing between two corrugated heat transfer plates (5) is provided. The gasket arrangement (G) comprises an annular field gasket portion (41) surrounding a field gasket region (A1) and a plurality of annular ring gasket portions (47c, 47d, 47e, 47f) arranged outside the field gasket region (A1). Each of the plurality of annular ring shim portions (47c, 47d, 47e, 47f) surrounds a ring shim region (A2) that is smaller than the field shim region (A1) and extends in a central extension plane (p2) of the ring shim portions (47c, 47d, 47e, 47f). A third ring gasket portion (47c) and a fourth ring gasket portion (47d) of the plurality of annular ring gasket portions (47c, 47d, 47e, 47f) are arranged on opposite sides of the transverse central axis (T1) of the field gasket region (A1). The gasket arrangement (G) is characterized in that a fifth ring gasket portion (47e) of the plurality of annular ring gasket portions (47c, 47d, 47e, 47f) is arranged on the same side of the transverse central axis (T1) as the third ring gasket portion (47c). Furthermore, the third ring gasket portion (47c) and the fifth ring gasket portion (47e) are arranged on opposite sides of the longitudinal central axis (L1) of the field gasket region (A1). Furthermore, a longitudinal central axis (L1) of the field gasket region (A1) extends through one of the plurality of annular ring gasket portions (47c, 47d, 47e, 47f).

This invention discloses a spaceborne near-space horizontal two-dimensional wind field interferometric imager based on a ring field of view and a full-link simulation method. The imager includes an optical system, a detector, and a data processing unit. The optical system includes a front conical mirror, a field stop, a collimating lens group, a Fabry-Perot interferometer, a narrowband filter assembly, and an imaging lens arranged sequentially along the optical path. This invention improves the spatiotemporal resolution of the instrument's detection.

The application discloses a kind of tunnel lining defect ring view detection methods, belong to tunnel detection technical field, can solve the problems of serious annular field distortion, large difference in multiple types of defect characteristics, insufficient use of spatial position information in existing tunnel lining detection.The method comprises the following steps: S1, collecting the annular field image of the inner wall of the tunnel, and converting the annular field image into a cylindrical expansion image;S2, scale feature extraction is carried out on the cylindrical expansion image to obtain a spatial scale feature map;S3, the spatial scale feature map is segmented and depth estimated respectively, and the corresponding defect feature map and depth feature map are obtained;S4, the defect feature map and the depth feature map are fused by gating, and the fusion feature map is obtained.The defect detection result is obtained by defect segmentation decoding of the fusion feature map.The application is used for tunnel lining defect detection.

The present invention relates to a method for producing a cartridge case by connecting the components thereof. The method comprises: providing a breech ring and a case made of the same or different materials; aligning the breech ring and the case in a device using positioning aids; providing a gap between the breech ring and the case; enclosing the region to be connected using an annular field former; conducting a current through the field former in order to induce currents in at least a first electrically conductive component, whereby a Lorentz force is generated; accelerating the first component away from the field former towards the second component to form an integral bond between the components.

The present application relates to a kind of star simulator annular field coil electromagnetic force analysis structure optimization method and system, it is related to star simulator annular field coil electromagnetic force structure optimization technical field, including according to the spatial constraint of vacuum chamber geometric characteristics and external modular coil, determine the arrangement scheme parameter of star simulator annular field coil;Utilize arrangement scheme parameter to construct coil three-dimensional geometric model, solve electromagnetic volume force distribution;Identify peak load area and extract single-turn coil equivalent load;Through cable deflection experiment, the equivalent Young's modulus of composite cable is determined, the equivalent elastic modulus parameter of cable is obtained;Equivalent load and equivalent elastic modulus parameter are combined with single-turn coil, establish fixture-cable coupling finite element model, determine the key structure size of fixture and verify strength criterion.The present application has beneficial effect for significantly improving the installation reliability and anti-electromagnetic force ability of annular field coil, ensure the accuracy of magnetic field configuration and the stability of device operation.

A system for applying a force or pre-stress to a portion of a toroidal field coil may including a structure having a first arm including a first arm gap wall and a second arm including a second arm gap wall. The structure may include an arcuate space separating the first arm and the second arm. The structure may include a bean-shaped opening configured to surround the toroidal field coil. An expandable container may be positioned between the first arm gap wall and the second arm gap wall. A liquid within the expandable container may expand upon freezing.

The invention discloses a position adjusting tool for a nuclear fusion toroidal field magnet, the position adjusting tool comprises a first support adjusting module and a second support adjusting module, a leveling module is arranged at the bottom of the second support adjusting module, and radial adjusting modules are slidably arranged on the first support adjusting module and the second support adjusting module; each radial adjusting module is provided with a vertical lifting module, and each vertical lifting module is slidably provided with a completion self-adaption bearing module matched with the annular field magnet to be installed; a tangential adjusting module is integrated on each vertical lifting module, and each tangential adjusting module is in power connection with the corresponding adaptive bearing module; linkage adjustment in the radial direction, the vertical direction and the tangential direction is achieved through the radial adjustment modules, the vertical lifting modules and the tangential adjustment modules, so that free adjustment in the six-degree-of-freedom direction and the installation posture is achieved, the adjustment precision is effectively improved, and then the positioning installation precision of the circumferential field magnet is improved.

The present invention provides a ring-shaped magnetic flux memory motor and magnetic flux method, comprising a stator core; an AC armature winding placed on the stator core; a ring-shaped magnetic flux winding placed on the stator core; a rotor core; a variable flux permanent magnet placed on the rotor core; a constant flux permanent magnet placed on the rotor core; and a rotating shaft. The stator core is provided with a plurality of axial stator slots facing the air gap for accommodating a plurality of AC armature winding coils; the stator core is also provided with an annular stator slot facing the air gap for accommodating a DC ring-shaped magnetic flux memory motor; the rotor core of the motor is divided into two sections along the axial direction, with variable flux permanent magnets and constant flux permanent magnets arranged at intervals placed on the cores at both ends. The ring-shaped magnetic flux memory motor of the present invention is loaded with forward or reverse DC current pulses to change the magnetization state of the variable flux permanent magnet, thereby adjusting the air gap magnetic field strength.

The present invention provides a method for manufacturing a cartridge case by joining its components. The method comprises: providing a base and a case made of the same or different materials; aligning the base and the case in a device using positioning aids; providing a gap between the base and the case; enclosing the area to be joined with an annular field former; passing a current through the field former to induce currents in at least a first electrically conductive component, thereby generating a Lorentz force; accelerating the first component from the field former towards the second component, forming a material-bonded connection between the components.