8results about How to "Simple switching process" patented technology

The invention discloses an office chair which can realize quick switching of rest modes and can adapt to arm supporting requirements in a lying state. Comprising a seat plate, two chair legs arranged on the lower portion of the seat plate and a backrest arranged on the upper portion of the seat plate, a driving mechanism is arranged at the bottom of the seat plate, the backrest is connected with the driving mechanism, and the driving mechanism is used for driving the backrest to rotate; handrails are arranged on the left side and the right side of the seat plate, the two handrails are connected with a driving mechanism, and the driving mechanism drives the backrest to rotate and is also used for synchronously driving the two handrails to move in the sitting depth direction of the seat plate; a pedal is arranged below the seat plate, and the driving mechanism is used for driving the pedal to move in the sitting depth direction of the seat plate while driving the backrest to rotate and the two armrests to move.

The utility model discloses a kind of three-stage tool for vehicle-mounted radar controller assembly, applied in vehicle-mounted radar controller assembly tool technical field, and its technical solution main point is: including the first carrier for positioning circuit board, the first carrier is sequentially detachably equipped with the second carrier for positioning fiber connector and the third carrier for positioning controller shell from bottom to top based on positioning fixed assembly, the second carrier and the third carrier are equipped with carrier identification code for identifying carrier model;With technical effect is: simple structure, can flexibly switch tool, wide adaptation range.

The invention provides monocrystalline silicon wafer cleaning equipment and method, and relates to the technical field of monocrystalline silicon, the monocrystalline silicon wafer cleaning equipment comprises a cleaning box, a partition plate is arranged in the cleaning box, the cleaning box is divided into an upper heating area and a lower cleaning area by the partition plate, a moving plate is arranged in the cleaning box, the moving plate moves in the upper heating area and the lower cleaning area, and a monocrystalline silicon wafer is installed on the moving plate; a water tank and a pickling tank are arranged on the cleaning tank, the water tank and the pickling tank are both connected with pipelines in a penetrating mode, the other ends of the pipelines extend into the lower cleaning area, and a liquid storage tank is arranged in the lower cleaning area and matched with the movable plate. The cleaning box is divided into the upper heating area and the lower cleaning area through the partition plate, the moving plate directly drives the monocrystalline silicon wafer to move between the two areas, manual or auxiliary mechanism carrying is omitted, and the cleaning period is greatly shortened; the whole process of heating, cooling, acid pickling and water washing of the monocrystalline silicon wafer is completed in the closed cleaning box, the monocrystalline silicon wafer does not need to be exposed in the external environment, and the surface cleanliness of the cleaned silicon wafer is ensured.

The application provides a spacecraft docking assembly system and method based on logistics automation, the system comprising an automated logistics subsystem, a multi-station serial layout assembly platform subsystem, a shipment-integrated tray device, and an auxiliary operation robot subsystem; the assembly platform subsystem is divided according to assembly functions and mainly comprises a cabin docking platform and an extravehicular direct subordinate component mounting platform, wherein the cabin docking platform is used for completing docking of each cabin of a spacecraft, and the extravehicular direct subordinate component mounting platform is used for completing installation of extravehicular air rudders, cable covers and other direct subordinate components of the spacecraft; the shipment-integrated tray device is divided into a full missile tray and a cabin tray and is used for supporting a full missile and each cabin of the spacecraft respectively; and the auxiliary operation robot subsystem uses a suction cup to realize grabbing and positioning and placing of the direct subordinate components and assists an operator to complete installation of the direct subordinate components.

The utility model relates to the technical field of carburizing devices, and discloses a low-carbon alloy steel carburizing device which comprises a base plate, a carburizing assembly, a driving assembly and a gas homogenizing assembly. According to the low-carbon alloy steel carburizing device, by optimizing the structural design, gas distribution is more uniform, the depth and uniformity of a carburized layer are remarkably improved, when a first servo motor is started, a base and a first spiral guide plate can be driven to rotate, and therefore low-carbon alloy steel placed on the base can be driven to rotate; the surface of the low-carbon alloy steel is uniformly exposed in carburizing gas, a first spiral guide plate drives the gas to spirally flow, the contact area and time of the gas and the low-carbon alloy steel are increased, meanwhile, a second servo motor is started to enable the first spiral guide plate and a second spiral guide plate to form a convection effect, gas distribution is further optimized, and carburizing efficiency is improved. And the arranged gas conveying assembly can ensure rapid switching work of carburizing gas and inert gas, and the gas switching process is simplified.

The utility model discloses a filling machine for lubricating oil production relates to lubricating oil processing technical field. The utility model discloses a base and the casing of fixed connection at the top of base, the top of base is provided with a plurality of oil pipes, the base bottom is fixedly connected with a plurality of support columns, the casing inner wall is fixedly connected with the support plate no.

The utility model discloses a spot welding clamp quick-change structure which comprises a fixed base and a quick-change structure body, and the quick-change structure body can move to the upper side of the fixed base and is fixed to the fixed base through a fixing piece. A guide structure and a first limiting block are arranged on the fixed base; the quick-change structure comprises a clamp mounting plate, and a guide block and a second limiting block which are arranged on the clamp mounting plate; the guide structure and the guide block are used for guiding the quick-change structure in the process that the quick-change structure moves to the upper side of the fixed base, and after the first limiting block abuts against the second limiting block, the quick-change structure moves in place. Through the arranged guide structure, guide block, first limiting block and second limiting block, the fixture mounting plate and the fixture on the fixture mounting plate can be quickly switched on the fixed base, and the fixture mounting plate can be accurately positioned through the cooperation of the first limiting block and the second limiting block, so that the switching efficiency of the fixture is further improved; by means of the structure, the switching process of the clamp is simple, and switching operation can be completed by one person.

The invention discloses a mounting device for a multi-rotor aircraft. The multi-rotor aircraft mounting device comprises a mounting mechanism and a task cabin, the mounting mechanism is provided with a mounting table, a movable bolt, a bolt motor and a sectional force control locking controller, and the task cabin is provided with a locking butt joint part; the mounting platform is connected with the aircraft body of the multi-rotor aircraft and is matched with the locking butt joint part; the movable bolt is provided with a locking positioning assembly, a locking movable assembly and an unlocking assembly; the locking and positioning assembly is connected with the mounting table, the locking and positioning assembly is connected with the locking movable assembly, and the locking and positioning assembly is connected with the unlocking assembly; the locking movable assembly is matched with the unlocking assembly, the locking positioning assembly and the locking butt joint part to lock the hanging platform and the locking butt joint part mutually; the unlocking assembly is used for releasing mutual locking of the hanging platform and the locking butt joint part by the locking movable assembly, and the sectional force control locking control is matched with the bolt motor to control the locking movement process. The method and the device are used for realizing rapid multi-task switching of the multi-rotor aircraft.