A Calculation Method of Process Parameters of Compression and Stretching of Propellant

A calculation method and technology of process parameters, applied in the field of calculation of propellant compression and stretching process parameters, can solve problems such as increased outlet pressure, inability to give a more suitable new formula, and large difference in results, so as to reduce material waste, shorten The effect of development time

Active Publication Date: 2020-12-15
XIAN MODERN CHEM RES INST
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Problems solved by technology

The following problems exist in the existing calculation method of propellant compression-stretching process parameters: (1) The calculation process needs to rely on the existing test data and correct it through manual experience, and the results obtained by experienced personnel and inexperienced personnel are quite different; (2) For the new formula, more suitable process parameters cannot be given, and it is necessary to gradually increase the pressure from a lower pressure, which takes a long time and wastes more medicinal materials when finding a suitable pressure; (3) due to the During the compression and stretching process of the material, the pressure transmission is related to the amount of the material, and the pressure at the drug outlet has a certain delay. Therefore, under the premise that a certain pressure range is not given, the continuous rise of the pressure will lead to a sudden increase in the outlet pressure. Large, resulting in a greater security risk

Method used

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  • A Calculation Method of Process Parameters of Compression and Stretching of Propellant
  • A Calculation Method of Process Parameters of Compression and Stretching of Propellant

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Embodiment Construction

[0020] The specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0021] according to figure 1 , taking Sanji propellant as an example, the nitrogen content of nitrocellulose is 12.8%, the RDX is class 5, and the solvent ratio is 0.27. The calculation steps of the compression and stretching process parameters of the propellant are as follows.

[0022] (1) After weighing the required raw materials, the kneaded medicine is ready for use;

[0023] (2) Take a small amount of medicinal material by using a heat preservation device, and use a capillary rheometer to test the rheological properties of the medicinal material. The data are as follows:

[0024]

[0025] (3) Using modified Bingham model and Power model for fitting, modified Bingham model (fitting degree is 0.98), Power model (fitting degree is above 0.99);

[0026] (4) Select the constitutive equation with a higher degree of f...

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Abstract

The invention discloses a method for calculating the technical parameters of a propellant powder pressure extension, which can carry out calculations for new propellant formulations without relying on empirical data and manual experience, and provides a relatively suitable pressure extension range. According to the method, the Rheological property of the propellant powder material is adopted to carry out tests, a constitutive equation of the propellant powder material is further obtained, suitable parameters of the equation after fitting are obtained, and a model of the propellant powder pressure extension is established; the pressure extension process of the propellant powder can be better described by the constitutive equation based on the performance of the propellant powder material, and for new propellant formulation, relatively good process parameters can also be obtained without empirical data and manual experience. By using the three-dimensional model and the finite element analysis method, the pressure range of the suitable propellant pressing process parameters can be obtained, a relatively suitable pressure range for the technical parameters of propellant powder pressure extension and a suitable pressure range for the technical parameters of the pressure extension can be obtained, it is ensured that the pressure is not exceeded at a medicine discharge mouth in the pressure extension process, and the risk of combustion explosion is avoided.

Description

technical field [0001] The invention relates to a method for calculating process parameters of compression and stretching of propellant, which is suitable for calculating process parameters of compression and stretching process in the manufacturing process of propellant products. Background technique [0002] The process of propellant product preparation includes absorption, water displacement, granulation, gelatinization, compression stretching, drying, etc. Among them, the compression stretching process is the forming process of propellant powder, and the dimensional accuracy, compactness, and surface gloss of propellant powder are uniform. It is determined by the quality of the compression-stretching process, and the core of the compression-stretching process is the design of the compression-stretching process parameters. Under certain mold conditions, the ideal propellant product can be obtained through appropriate process parameters. The existing propellant compression ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/23G06T17/00
CPCG06T17/00G06F30/23
Inventor 张江波魏学涛白娟肖霞刘毅梁磊严文荣闫光虎赵煜华赵晓梅周媛丽
Owner XIAN MODERN CHEM RES INST
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