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Simple small projectile launcher enabling projectile to obliquely enter water at medium and low speeds

A technology for launching devices and projectiles, which is applied to the testing of launching devices, ammunition, and ammunition, can solve the problems of small adjustment range of projectile entering water speed, inability to guarantee experimental results, etc., and achieves easy disassembly, guaranteed experimental results, and controllable speed variables. Effect

Pending Publication Date: 2019-08-23
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The device has a small adjustment range of the projectile entering the water speed, which cannot guarantee the experimental effect

Method used

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  • Simple small projectile launcher enabling projectile to obliquely enter water at medium and low speeds
  • Simple small projectile launcher enabling projectile to obliquely enter water at medium and low speeds
  • Simple small projectile launcher enabling projectile to obliquely enter water at medium and low speeds

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0013] Such as figure 2 As shown, a simple launching device for small projectiles inclined into the water at medium and low speeds, including guide rails 3, springs 4, projectiles 6, strings 2, fixing devices 1 and baffles 5;

[0014] Such as image 3 As shown, the guide rail is divided into a hollow cylindrical part with double holes in the front section and a hollow semi-cylindrical part in the rear section. The hollow cylindrical part in the front section is the main load-bearing part of the launching device, and a spring is placed inside. It is necessary to ensure the stability of the spring. Complete hollow cylinder; the upper part of the hollow semi-cylinder in the rear section is hollowed out, and the lower part is used as the movement track of the projectile body; the string 2 is tied to the baffle plate 5 and passed through the small hole at the front end of the guide rail, and the spring is placed on the Between the baffle plate 5 and the guide rail 3, the spring e...

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PUM

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Abstract

The invention discloses a simple small projectile launcher enabling a projectile to obliquely enter water at medium and low speeds. The simple small projectile launcher comprises a guide rail, a spring, the projectile, strings, a fixing device and a baffle. The guide rail comprises a hollow cylinder part located on the front section and provided with double holes and a half hollow cylinder part located on the rear section, the spring is put in the hollow cylinder part on the front section, the upper half portion of the hollow cylinder on the rear section is hollowed out, and the lower half portion of the hollow cylinder on the rear section serves as a projectile movement rail. The strings are bound on the baffle and penetrate out of the small holes in the front end of the guide rail, the spring is put between the baffle and the guide rail, the fixing device is used for pressing the projectile on the guide rail, and the tail of the projectile makes contact with the baffle. The simple small projectile launcher has the beneficial effects that the device is simple, the operation is easy, disassembly is easy and convenient, speed variables can be controlled, and the cost is low.

Description

technical field [0001] The invention relates to the technology of oblique entry of projectiles into water at medium and low speeds, in particular to a simple launching device for small projectiles obliquely entering water at medium and low speeds. Background technique [0002] Entering the water at medium and low speeds will produce air-entry cavitation. Water-entry cavitation is a physical phenomenon accompanying the process of projectile entering water. The formation, expansion, closure, and collapse of cavitation will affect the motion characteristics and hydrodynamic characteristics of projectiles entering water. The study of complex cavitation flow is the basis for the design of air-dropped torpedoes, water-entry missiles, and supercavitating projectiles. [0003] In order to study the evolution process of the cavitation and the ballistic characteristics of the projectile during the oblique entry into the water at low and medium speeds, in the experiment of oblique ent...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F1/00F42B35/00
CPCF41F1/00F42B35/00
Inventor 黄振贵罗驭川陈志华侯宇唐楚淳
Owner NANJING UNIV OF SCI & TECH
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