7results about How to "Eliminate assembly errors" patented technology

The utility model provides a square cell sealing nail welding with anchor clamps, including bottom plate, and set up in the bottom plate's benchmark fixed plate, floating fixed plate, intermediate fixed plate, long side fixed plate and cushion block, wherein: benchmark fixed plate with floating fixed plate opposite setting, intermediate fixed plate with long side fixed plate opposite setting, floating fixed plate at least partial can be close to or far from benchmark fixed plate, long side fixed plate at least partial can be close to or far from intermediate fixed plate, cushion block is used for supporting the battery, and the cushion block is between intermediate fixed plate and long side fixed plate, first guide shaft is configured on the cushion block, first guide shaft with bottom plate sliding connection is established, and first buffer spring is configured between the cushion block and bottom plate. The utility model discloses cushion block floating assembly, can avoid welding plate and battery hard contact, and can eliminate the longitudinal assembly error of battery simultaneously.

This application discloses a three-dimensional ultra-wideband power divider, belonging to the field of radio frequency communication technology. It includes an input port, a strongly coupled line unit, a weakly coupled line unit, a first output port, and a second output port. The input port, strongly coupled line unit, and weakly coupled line unit are connected sequentially. The first terminal of the second end of the weakly coupled line unit is connected to the first output port, and the second terminal of the second end of the weakly coupled line unit is connected to the second output port. The weakly coupled line unit includes any number of coupling lines and multiple first resistors, with the multiple first resistors bridging between two coupling lines of the weakly coupled line unit. The strongly coupled line unit is a three-dimensional integrated vertical substrate circuit structure. This application overcomes the contradiction between ultra-wideband, high isolation, low loss, and mass production through a three-dimensional integrated structure, gradually changing coupling lines, and a multi-level bridging resistor network, providing a high-performance power divider solution for high-frequency communication systems.

This utility model relates to the field of household appliances, and particularly to a rotary dehumidifier and a rotary dehumidifier. It includes a mounting frame and a rotary frame; the rotary frame has a receiving cavity for mounting the dehumidification disc, and the mounting frame has a mounting cavity for rotatably mounting the rotary frame. The front end of the mounting cavity is a mounting opening. The mounting frame also has a drive assembly for driving the rotary frame to rotate within the mounting cavity, and a limiting assembly located around the mounting opening for confining the rotary frame within the mounting cavity. This improved assembly method by limiting the rotary frame eliminates assembly errors of the dehumidification disc, making installation simpler and more convenient.

This utility model discloses an antenna radome flipping assembly device, including a frame, a flipping bearing component, a flipping plate component, and an anti-rotation mechanism. The flipping bearing component consists of two sets, each including: a bearing fixedly installed on the top of the frame; and a stainless steel rotating shaft fixedly fitted inside the inner ring of the corresponding bearing. This utility model, through a series of structures, can prevent mistakenly positioning the antenna array, ensuring that employees cannot place the antenna array in the wrong direction or repeatedly adjust its position, thus eliminating assembly errors and improving efficiency and accuracy. It can press and lock the antenna array after the outer cover is installed, and can rotate and lock the positioned and pressed antenna array and outer cover to prevent rotation, allowing personnel to tighten screws from below. Furthermore, it can precisely guide the screws during tightening, preventing damage to the antenna array during screw tightening and reducing the risk of damaging parts.

This invention discloses a hydraulic thruster propulsion position monitoring mechanism, thruster, and method, which solves the problem in the prior art that displacement sensors cannot accurately locate the assembly position, and has the beneficial effect of improving product consistency. The specific solution is as follows: A hydraulic thruster propulsion position monitoring mechanism includes a transmission component installed radially on the assembly. One end of the transmission component extends into the axial process hole of the assembly. One end of the transmission component at the axial process hole contacts a guide component. An elastic component is provided at the other end of the transmission component. The end of the elastic component away from the transmission component is limited. The transmission component is connected to a position feedback column, which is installed at the axial opening of the assembly. When the assembly shaft moves relative to the assembly, it contacts the guide component, thereby driving the position feedback column to move radially.

The application provides a calibration method of a right-angle prism for aircraft assembly, and belongs to the field of aircraft assembly tools. The application is realized based on a calibration adjustment clamp, a laser radiator positioning seat on the clamp clamps the laser radiator, a prism positioning seat clamps the right-angle prism, an incident light calibration front seat and an incident light calibration rear seat are arranged on an incident light path, the coaxiality of incident light is calibrated by the fact that light rays simultaneously meet the requirements of target center on the two calibration seats, a refracted light calibration front seat and a refracted light calibration rear seat are arranged on a refracted light path, the calibration of the right-angle prism is realized in a way of over-constraint by the fact that refracted light simultaneously meets the requirements of target center on the two calibration seats. The application realizes the calibration of the right-angle prism, guarantees that the perpendicularity is controlled within 0.05mm in the range of 10m, the calibrated prism has been applied in the process of aircraft product manufacturing, and good application effect is obtained, and the positioning and detection precision of the product are improved.

The utility model belongs to aerospace technology field, concretely relates to a propeller integral forming die, the utility model discloses a propeller integral forming die includes first mould and second mould, and the first mould has the profiling groove, and the second mould has the profiling boss, and the second mould and first mould buckle and connect, and the profiling boss is used for and the profiling groove plug-in and form propeller forming cavity. Using the propeller integral forming die in the technical scheme can realize the integrated forming of propeller, and the propeller prepared using the propeller integral forming die can significantly improve the structural reliability of equipment propulsion system, reduces the assembly error, and is convenient for dynamic balance debugging.