Companding moulding method for gun propellant with predetermined design size

A molding method and propellant technology, which is applied in design optimization/simulation, calculation, special data processing applications, etc., can solve problems such as unusable test data, inability to combine organically, and inability to correct and calculate drug shape detection values, so as to improve quality Consistency, the effect of filling the domestic gap

Active Publication Date: 2017-12-15
XIAN MODERN CHEM RES INST
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Problems solved by technology

The existing propellant powder compression stretching method has the following problems: (1) the existing empirical data is used in the design process, and the test data of this time cannot be used. If the design result is not suitable, real-time correction cannot be carried out; (2) the design The p

Method used

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  • Companding moulding method for gun propellant with predetermined design size

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Example Embodiment

[0039] The specific embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0040] Take the three-base propellant as an example.

[0041] Proceed as follows:

[0042] (1) The design of the process parameters is completed by the drug shape parameter design software 1, the compression and stretch process design software 2, the mold design software 3: the number of holes = 19; the pressure = 8MPa; the drug delivery speed = 25mm / s; the arc thickness = 1.9mm ;Outer diameter=19mm;

[0043] (2) Push the process parameters to the propellant compression and stretch forming collaborative platform 11 through the digital design management software 4;

[0044] (3) The propellant compression and stretch forming collaborative platform 11 decomposes the process parameters through the design of a multi-parameter measurement system 10 and a design control system 8. One part is the control parameter of the press: pressure = 8MPa; the...

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Abstract

The invention discloses a gun propellant companding moulding method which can achieve process design, parameter push and parameter measurement cycle operation, and conduct real-time inverse calculation of design data to obtain suitable companding process parameters. The method uses a collaborative platform technology, and achieves process design, parameter push, reading and analyzing of parameter measurement results, and process cycle operation. Compared with the existing technology, the parametric real-time circulation of design, companding and detection links is achieved, and the foundation is provided for synchronous correction feedback; the technology of target parameter and detection parameter data real-time contrast is used to achieve real-time judgment on the dimension parameters of gun propellant products. Compared with the existing technology, the quality criteria of product online parameters can be provided in real time.

Description

technical field [0001] The invention relates to a compression-stretching forming method of propellant, which is suitable for the compression-stretching process of propellant. 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 compression-stretching forming method of propellant powder is to predict the process parameters by using empirical data, input th...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F30/20
Inventor 张江波魏学涛白娟梁磊刘毅肖霞严文荣闫光虎赵煜华周媛丽赵晓梅
Owner XIAN MODERN CHEM RES INST
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