3results about How to "Reduce recoil" patented technology

The utility model discloses an air storage type air gun, and particularly relates to the technical field of air guns, the air storage type air gun comprises a gun body, bullets and a gun stock fixedly installed on one side of the gun body, a shock absorption box is fixedly installed on one side of the outer surface of the gun stock, a shock absorption air bag is fixedly installed in the shock absorption box, and a rubber pad is slidably connected in the shock absorption box. And the rubber pad is fixedly connected with the outer surface of the damping air bag. According to the air storage type air gun, in actual work, an operator exerts pushing force on the pressing plate, the piston rod pushes the piston to move towards the interior of the air conveying cylinder, the damping air bag is expanded, and the rubber pad is pushed to the exterior of the damping box and makes contact with the body of the operator; the recoil force generated by shot shooting enables the gun stock to push the damping box to move towards an operator, then the damping air bag and the rubber pad are extruded, the recoil force acting on the body of the operator can be effectively reduced through the damping air bag and the rubber pad, and damage to the body of the operator caused by the recoil force is effectively reduced.

The application belongs to the technical field of underwater operation and maintenance process, and discloses an underwater facility generative cavitation cleaning method and system based on a diffusion model. The method comprises the following steps: obtaining sonar images, body attitudes and water depth data of the underwater facility; inputting the data into a conditional diffusion model to obtain a cooperative control action sequence, wherein the sequence comprises propeller thrust instructions and cavitation jet instructions, and the feedforward compensation thrust in the thrust instructions is ahead of the jet opening instruction in time; first, the propeller is controlled to output compensation thrust according to the feedforward compensation thrust instruction, and then the cavitation jet device is controlled to be opened; during the jet process, the real-time output thrust of the propeller is monitored, and if it is less than the recoil force estimated according to the current jet parameter, the jet parameter is reduced. The above-mentioned method generates cooperative sequence actions through a diffusion model, combines feedforward thrust pre-compensation and closed-loop safety clamping, realizes active inhibition of recoil force and self-adaptive cleaning of materials, and effectively improves the stability of underwater operation and the cleaning quality.

This invention provides a buffer structure for a launch system mounted on a drone, comprising a drone and a buffer structure at its bottom. The buffer structure includes a buffer component 1 and a buffer component 2 slidably connected to the buffer component 1. The launch system is mounted on the buffer component 2. The buffer component 2 is connected to a rotating rod assembly, which is connected to the drone. The rotating rod assembly is also connected to an airbag buffer assembly, which is mounted on a support frame at the bottom of the drone. This invention provides a buffer structure for a launch system mounted on a drone, avoiding the problems of insufficient launch accuracy and damage to the drone caused by large recoil during launch.