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A Prediction Method of Axial Compression Load Reduction Factor of Grid Slotted Shell

An axial compression and grid technology, applied in the field of structural strength design and analysis of tactical missiles, can solve the problems that are difficult to apply to the rapid and low-cost design requirements of tactical models, and achieve the effect of simple defect mode and efficient modeling

Active Publication Date: 2020-08-14
CHINA ACAD OF LAUNCH VEHICLE TECH
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Problems solved by technology

However, this method still needs a lot of experimental verification to provide the probability density information needed to determine the reduction factor, and it is difficult to apply to the design requirements of rapid and low-cost tactical models

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  • A Prediction Method of Axial Compression Load Reduction Factor of Grid Slotted Shell
  • A Prediction Method of Axial Compression Load Reduction Factor of Grid Slotted Shell
  • A Prediction Method of Axial Compression Load Reduction Factor of Grid Slotted Shell

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Embodiment Construction

[0039] In order to make the purpose, technical solution and advantages of the present invention clearer, the following will further describe the public implementation manners of the present invention in detail with reference to the accompanying drawings.

[0040] The prediction method of the axial load reduction factor of the grid slotted shell in the present invention is mainly aimed at the thin-walled grid slotted shell, considering the thin-walled grid slotted shell during processing, assembly, transportation and service For the most easily generated external force impact dent, the axial load reduction factor of the thin-walled grid slotted shell is predicted by means of defect sensitivity numerical analysis method.

[0041] refer to figure 1 , shows a flow chart of the steps of a method for predicting the reduction factor of the axial load of the grid slotted shell in the embodiment of the present invention. In this embodiment, the prediction method of the axial pressure ...

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Abstract

The invention discloses a prediction method for an axial compression bearing reduction factor of a grid slotted shell. The method comprises the steps of building a finite element model corresponding to the grid slotted shell; applying a specified displacement load to a horizontal-vertical slotted intersection position of the middle of the grid slotted shell and performing static force analysis to obtain a non perfect structure model with an initial single-point recess defect; based on this, obtaining a defect sensitivity curve of a single-point recess degree to axial compression bearing, and a defect sensitivity curve of a single-point recess position to the axial compression bearing; and according to the defect sensitivity curve of the single-point recess degree to the axial compression bearing, and the defect sensitivity curve of the single-point recess position to the axial compression bearing, obtaining a predicted result of the axial compression bearing reduction factor of the grid slotted shell. According to the method, the prediction of the axial compression limit load reduction factor of the thin-walled grid slotted shell is realized, so that whether the axial compression bearing capacity of the shell meets design requirements or not can be determined.

Description

technical field [0001] The invention belongs to the technical field of structural strength design and analysis of tactical missiles, and in particular relates to a method for predicting an axial pressure bearing reduction factor of a grid slotted casing. Background technique [0002] The thin-walled structure has the characteristics of light weight and good load-bearing performance, and is widely used in the structural design of the rocket body compartment. In order to meet the laying requirements of the optical fiber for impact measurement, the metal shell of the final repair cabin and the instrument cabin of a certain type of target missile adopts a structural form in which optical fiber grooves are engraved on the outside of the optical tube shell. Compared with the traditional grid-reinforced and skinned stringer-type thin-walled structure, designers lack engineering experience in the mechanical load-bearing performance of this new grid-slotted shell, especially its stab...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/23
CPCG06F30/23
Inventor 牛飞陈剑峰管飞吴瑞华严佳民方泽平杨东生梁祖典范新中姚重阳刘鹏于贺齐歆陈增奎丁国元孟令涛蔡亚楠万舒晨林启龙钱昕
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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