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Two-grade buffering and stopping mechanism of free piston

A buffer structure and piston technology, applied in mechanical equipment, springs, shock absorbers, etc., can solve the problems of large impact load of equipment, easy damage of elastic buffer pads, limited absorption of piston kinetic energy by buffer pads, etc. The effect of the rebound of the small piston

Active Publication Date: 2017-05-31
CHINA ACAD OF AEROSPACE AERODYNAMICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to overcome the shortcomings of the elastic buffer pads in the current international free piston shock wave tunnel equipment, which are easily damaged, have a large impact load on the equipment, and have limited absorption of piston kinetic energy by the buffer pads.

Method used

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  • Two-grade buffering and stopping mechanism of free piston
  • Two-grade buffering and stopping mechanism of free piston
  • Two-grade buffering and stopping mechanism of free piston

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Embodiment Construction

[0027] The accompanying drawing discloses a schematic structural view of a preferred embodiment of the present invention without limitation, and the technical solution of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0028] A free piston and pneumatic buffer stop mechanism design, such as figure 2 , 5 As shown, the free piston 1 is a cavity structure, including a rear end cover 11, a wear ring 12, a piston body 13, a retaining ring 14, a sealing ring 15 and a front end cover 16; the rear end cover 11 is fixed on the piston body by screws, The wear-resistant ring 12 is set on the piston body 13. The outer diameter of the wear-resistant ring 12 is larger than the outer diameter of the piston body. The seal ring 15 is set on the piston body. 45° included angle), the front end cover 16 is fixed on the piston body by screws, and the front end cover 16 has 12 vent holes with a diameter of 12mm, and the vent holes act on th...

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PUM

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Abstract

The invention provides a two-grade buffering and stopping mechanism of a free piston. The free piston is composed of a rear end cover, a wearing-resisting ring, a piston body, a retainer ring, a sealing ring and a front end cover; acceleration-phase resistance reduction, decelerating-phase resistance increasing and sealing functions of the piston can be realized; the whole body of the piston is of a concave cavity structure; the two-grade buffering and stopping mechanism is composed of a buffering cushion, a supporting ring, a sleeve and a base and is of a convex through structure. In order to realize soft landing requirements of the piston, an annular pneumatic buffering cavity is formed by the sleeve, the base and an inner wall of a compression pipe; when the piston enters, primary buffering can be realized and most of kinetic energy of the piston is absorbed; the buffering cushion forms secondary buffering and the residual kinetic energy of the piston is absorbed through elastic deformation or plastic deformation of a material, so that the soft landing of the piston is realized. According to the two-grade buffering and stopping mechanism provided by the invention, the disadvantages of the type of equipment at present in the world that the elastic buffering cushion is easy to damage, the impact load in equipment is relatively great, the capability of absorbing the kinetic energy of the piston by the buffering piston is limited are overcome.

Description

technical field [0001] The invention relates to the technical field of drive for high-enthalpy shock wave wind tunnels, in particular to the design of a free piston and a buffer stop mechanism in the free piston drive technology. Background technique [0002] The free-piston shock tunnel is a high-enthalpy shock wind tunnel using free-piston drive technology. This type of wind tunnel drives the free piston to isentropically compresses single-atom driving gas through a heavy-piston compressor, and drives the shock tube to run after reaching a high temperature and high pressure state. , after the test gas stagnates at the end of the shock tube, it expands and accelerates through the nozzle to achieve the purpose of high-speed and high-enthalpy flow simulation. [0003] combine figure 1 Describe the movement process of the piston: at the initial moment, the piston starts to accelerate from rest under the action of the pressure difference between the upstream and downstream (up...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16F9/02F16F9/32
CPCF16F9/02F16F9/0218F16F9/0281F16F2222/126
Inventor 张冰冰刘煊江海南毕志献陈星林键朱浩蒋博吴健李辰
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS
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