A drug-wound stress release device

A stress-releasing and drug-carrying technology, applied in jet propulsion, rocket engine, machine/engine, etc., can solve the problems of changing engine work, short range, and low energy of double lead-2 propellant, so as to reduce stress, Easy batch winding effect

Inactive Publication Date: 2016-07-06
XIAN MODERN CHEM RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The current generation of rain-enhancing rocket charge uses screw-pressed double lead-2 propellant. This type of propellant has high strength and high hardness and is suitable for the winding process with charge. The specific winding process is that the two ends of the charge are supported by core rods and fastened with nuts. , due to the good strength of this type of propellant, the winding stress and the tightening force of the nut have little influence on it, but the energy of the double-lead-2 propellant is low and the range is relatively short, so the use of screw pressure modified double-base propellant is currently proposed. The propellant replaces the double-lead-2 propellant to increase the range of the engine, but the strength of the modified double-base propellant is poor. If the original winding method is used directly, the winding stress on the charge will be too large. It is found that the winding stress makes the propellant Changes in the ballistic performance of the agent will cause the engine to work abnormally, or even disintegrate

Method used

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  • A drug-wound stress release device

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Embodiment Construction

[0008] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.

[0009] Such as figure 1 As shown, it is an assembly drawing of the medicine-wrapped stress relief device of the present invention when in use.

[0010] The front positioning ring 4a is inserted into the front clamping groove 3a and tightened by the throat clamp 5 to form a front positioning tool; the rear positioning ring 4b is inserted into the rear clamping groove 3b and is tightened by the throat clamp 3b to form a rear positioning tool, which is positioned before the mold core 1 is inserted successively. Frock, powder charge 6, rear positioning frock are also limited by the front stop ring 2a and the back stop ring 2b. Then install the assembled grain on the winding machine for winding. The grain is stressed by the tension of the fiber during winding. Excessive stress will lead to abnormal operation of the propellant or even dis...

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Abstract

The invention discloses a charged winding stress release device which resolves the problems that an engine works abnormally or even shuts down when the charging is subjected to winding stress in the winding process. The charged winding stress release device is composed of a mould core, a front check ring, a rear check ring, a front clamping groove, a rear clamping groove, a front positioning ring, a rear positioning ring and throat hoops, wherein the front positioning ring and the rear positioning ring are arranged in the front clamping groove and the rear clamping groove respectively to form two independent positioning tools and hooped tightly through the throat hoops, the front and rear positioning tools are arranged at the two ends of the charging respectively, and the mould core is inserted and positioned through the front and rear check rings. The charged winding stress release device is suitable for releasing the stress generated in the charged winding process of a screwing star hole.

Description

technical field [0001] The invention relates to a stress release device, in particular to a propellant winding stress release device, which is suitable for winding a non-metal shell of a propellant. Background technique [0002] In the solid propellant engine manufacturing process, compared with the traditional process of winding the shell first and then casting the propellant, the new process of winding with powder eliminates the necessary mandrel tooling and mandrel making in the traditional process. Relatively simple; compared with the steel casing, it is light in weight and low in cost, and is a promising method for manufacturing the engine casing. There are now a small number of rain-enhancing rockets in China using this method for engine casing manufacturing. The current generation of rain-enhancing rocket charge uses screw-pressed double lead-2 propellant. This type of propellant has high strength and high hardness and is suitable for the winding process with charge. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02K9/10B65H81/06
Inventor 陈国辉舒慧明刘晨田军李鹏杨士山李旸吴淑新路向辉李冬史爱娟曹继平张艳时艺娟
Owner XIAN MODERN CHEM RES INST
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