7 results about "Orbital ring" patented technology

This invention discloses an inlaid, patch-type, dual-track screening machine and a dedicated cylinder, comprising a frame, a power control box, an air source control box, a cylinder, a chassis, a rotating track ring, a pressure ring, a main motor, a main reducer, an auxiliary motor, an auxiliary reducer, an inclined base, air pipes, and a compressed air source. The cylinder is characterized by being composed of an upper ring and a lower ring. The lower ring has an annular outer track groove, a flat-blowing pipe mounting hole, a guide groove, and a conveyor track mounting groove. The inner wall of the lower ring has a flat-blowing hole adapted to the flat-blowing pipe mounting hole. The guide groove is connected to the first end of the outer track groove. The end of the outer track groove is connected to the track groove of the conveyor track fixed on the conveyor track mounting groove. A guide plate is provided on the inner side wall of the upper ring, with the inner end of the baffle at the bottom of the guide plate inserted into the inner track groove. A cover plate is provided on the top of the outer track groove. This invention features two annular track grooves, ensuring smooth operation and normal production of high-speed production lines.

This invention provides a positioning device and method for a surveying instrument used in engineering surveying, relating to the field of surveying instrument technology. In this invention, a first frame and a second frame are rotatably connected by a shaft. An extension frame is slidably connected to the outer surface of the second frame to extend its length. Fasteners are provided between the second frame and the extension frame for fixation. A target positioning component and an inclination sensor are provided on the first frame. The target positioning component also has a protective component to protect the positioning element. In this invention, the protective component, through the cooperation of a track ring, gear transmission, and baffle structure, can be unfolded and folded by rotating a handle. When unfolded, it forms a complete circular protective surface that wraps around the positioning prism, effectively preventing damage to the positioning prism from collisions, dust corrosion, etc., during transportation or when not in use. When folded, it does not affect the signal reception of the positioning prism, thus balancing protection and practicality.

A kind of multi-group independent lifting rotating show device, it is related to performance stage prop technical field, including fixed truss, rotating truss, a certain number of rotating components and a certain number of lifting components, fixed truss is fixed in the top of show stage, a certain number of first support is arranged in the bottom of fixed truss, first support bottom is provided with hanging wheel, rotating truss top is provided with annular hanging track and annular friction track, annular hanging track is hung on hanging wheel, rotating component includes rotating drive motor and rotating friction wheel, rotating friction wheel and the side of annular friction track are in abutment, lifting component includes lifting winch group fixed on rotating truss, steering pulley, hanging point pulley, traction rope is sequentially through steering pulley and hanging point pulley, then vertically downward passes through rotating truss.The utility model can be used for the rotating movement and lifting movement when multiple actors perform in the air, realize the multidimensional position change of multiple actors in the air performance.

This invention discloses a device and method for detecting the water vapor composition and wind field occultation of planetary atmospheres, belonging to the field of planetary atmospheric detection technology. It includes a sealed mounting housing, a modular control unit, and an all-fiber optic unit. The device adopts a layered sealed structure of "upper-layer optics + lower-layer control." The optical unit receives sunlight passing through the planetary atmosphere via a solar telescope, mixes it with one laser beam split by a laser to generate a water vapor absorption spectrum, and extracts the peak wavelength λ'. Another laser beam passes through a built-in calibration gas cylinder to generate a standard absorption spectrum, and extracts the peak wavelength λ. Based on the Doppler frequency shift principle, the line-of-sight wind speed is inverted using the wavelength drift. This invention features strong adaptability to orbital environments, high integration, and high measurement accuracy. It can achieve synchronous in-situ detection of water vapor composition and wind speed in planetary atmospheric orbits, meeting the requirements of lightweight, radiation-resistant, and long-life interplanetary orbit detection, and is suitable for on-orbit occultation detection scenarios in planetary atmospheric orbits.

This invention discloses a lunar orbit space solar power station system, belonging to the field of spacecraft structure and energy system technology. Addressing the problems of traditional solar power generation failure in the lunar polar shadow regions and the inability of existing space power station structures to adapt to the lunar orbit environment, a novel system is proposed, comprising: a double-layered box-type central truss made of carbon fiber composite material; 12 thin-film solar subarrays, achieving independent solar tracking via a first conductive rotary joint; 5 laser transmitting antenna subarrays, achieving precise pointing via a second conductive rotary joint; and a rotary connection module. The system adopts a tree-like topological multibody structure, allowing independent attitude adjustment of the solar energy collection and laser transmitting modules, achieving decoupling between solar tracking and laser pointing. This invention offers advantages such as modular on-orbit assembly, lightweight and high rigidity, and flexible vibration suppression, providing continuous wireless energy transmission to the lunar polar regions.

This invention belongs to the field of space electric propulsion in aerospace propulsion technology, and relates to a microwave DC cathode suitable for oxidizing working fluids and its operating method. The microwave DC cathode includes a discharge cavity body, a microwave antenna, leads, an insulating medium, contact electrodes, a microwave connector, and a high-temperature resistant component. The microwave antenna is horizontally mounted inside the discharge cavity body; the microwave connector is vertically fixed to the discharge cavity body; the high-temperature resistant component is installed between the discharge cavity and the microwave connector; the leads, insulating medium, and contact electrodes are sequentially stacked and fixed at the outlet end of the discharge cavity body from the inside out; lead-out holes are pre-machined at the center of the leads and contact electrodes, and a center hole is pre-machined at the center of the contact electrode; the discharge cavity is formed by the discharge cavity body, leads, and high-temperature resistant component forming an outer envelope, and the microwave antenna is the inner envelope; the head of the microwave antenna is pointed, with the pointed end facing the lead-out hole. This invention addresses the cathode requirements of electric propulsion systems in ultra-low Earth orbit environments.

This utility model discloses a crane anti-sway control system, belonging to the field of crane technology. It includes a track ring located outside the load-bearing rope. A track groove is formed on the upper surface of the track ring, and a movable seat is slidably engaged in the track groove. A control telescopic rod is fixed on the movable seat, and a buffer assembly is fixed to one end of the control telescopic rod. A locking mechanism is installed on the buffer assembly. The buffer assembly includes a movable plate, with edge plates fixed on both sides above the movable plate. Wing plates are fixed on both sides of the edge plates near the load-bearing rope. One end of the control telescopic rod is fixed to the wing plates. A limit protrusion is fixed to the bottom of the movable plate, and a bearing plate is fixed to the side wall of the movable seat. This control system is mainly used to reduce the sway amplitude of the load-bearing rope when lifting heavy objects. When swaying occurs, the drive mechanism can move the buffer assembly and the locking mechanism to the corresponding positions, and then the swaying of the load-bearing rope is slowed down by controlling the telescopic rod.