Reverse air jetting air bubble assisting high-speed water inlet reducing impact load mechanism
A technology of impact load and cavitation, which is applied in the field of high-speed entry of moving objects into water, can solve the problem of large area of the navigating body, and achieve the effect of being conducive to stability.
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2019-02-15
- Estimated Expiration
- Not applicable · inactive patent
Smart Images

Figure 1 
Figure 2
Abstract
Description
technical field
[0001] The invention belongs to the technical field of high-speed water entry of moving objects, and in particular relates to a mechanism for assisting high-speed water entry to reduce impact load by reverse jet ventilation cavitation. Background technique
[0002] When the moving body enters the water at high speed, excessive impact loads are generated due to sudden changes in the density of the medium. Excessively high impact loads will cause the equipment in the moving body to fail, and even cause the structure of the moving body to be damaged. In order to avoid this situation, the high-energy jet is used to squeeze the water surface, and a gas cavity is formed to wrap the surface of the vehicle during the water entry process, thereby reducing resistance and playing the role of buffering and guiding the water entry. The cavitation technology in underwater drag reduction has been the focus of attention of various countries since the last century. Foam drag...
Examples
Embodiment Construction
[0010] The present invention will be further described below in conjunction with the accompanying drawings.
[0011] as attached figure 1 Shown, is the schematic diagram of mechanism of the present invention; Comprising high-pressure gas bottle 1, gas circuit 2, fairing 3, engine 4, nozzle 5, empennage 6, air hole 7, high-speed gas jet hole 8, moving body 9, air cavity 10, electronic pressure regulating valve 11, electronic flow meter 12, computer control device 13, threaded connection device 14; Fairing cover 3 is connected on moving body 9 head by thread 14, and some air holes 7 are evenly distributed in the circumferential direction of moving body head, and air hole and The annular air cavity 10 inside the shell is connected, and the engine supplies air to the air cavity through the air circuit 2. The electronic pressure regulating valve 11 and the electronic flow meter 112 are arranged on the air circuit, and the air cavity is connected to the high-speed gas jet hole 8 on ...