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Method for predicting compression rigidity and compression strength of composite material spiral structure by considering geometric nonlinearity

A geometrically nonlinear, composite technology, applied in the field of predicting the compressive stiffness and compressive strength of composite helical structures, which can solve the problems of complex calculation, high cost of compressive stiffness and compressive strength, and difficult to guarantee calculation accuracy.

Active Publication Date: 2020-12-15
BEIHANG UNIV
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AI Technical Summary

Problems solved by technology

Experimental means to directly measure the compression stiffness and compressive strength of the helical structure of composite materials is expensive, and the test process is easily affected by many accidental factors
The finite element numerical simulation method needs to establish a complex finite element model, the calculation is complicated, the calculation efficiency is low, and the calculation accuracy is difficult to guarantee

Method used

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  • Method for predicting compression rigidity and compression strength of composite material spiral structure by considering geometric nonlinearity
  • Method for predicting compression rigidity and compression strength of composite material spiral structure by considering geometric nonlinearity
  • Method for predicting compression rigidity and compression strength of composite material spiral structure by considering geometric nonlinearity

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Embodiment Construction

[0108] Step 1, defining the geometric shape and size of the helical structure of the composite material, and determining the mathematical expression of the relationship between various geometric parameters.

[0109] The overall appearance of the helical helix structure of the composite material is helical, and the cross section is circular. The composite material used can be a unidirectional reinforced composite material or a plane braided composite material. The helical structure of the composite material has elastic deformation ability along the direction of the helical axis. A compressive load is applied along the helical axis at both ends of the helical helical antenna of the composite material, and the pitch decreases. After the compressive load is removed, the helical structure of the composite material recovers to initial configuration.

[0110] In order to establish a theoretical prediction model for the compression performance of the composite helical structure, the fol...

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Abstract

A method for predicting compression rigidity and compression strength of a composite material spiral structure by considering geometrical nonlinearity comprises the following four steps: step 1, defining the geometrical shape and size of the spiral structure of the composite material, and determining a mathematical expression of a relationship among geometrical parameters; 2, carrying out stress analysis on any cross section A, and calculating the deformation and compression rigidity of the composite material spiral structure based on an energy principle; 3, through the compression deformationincrement and the compression load increment in the cumulative loading process, establishing a load displacement relation considering geometric nonlinearity of the composite material spiral structure, and linearly fitting a load displacement curve according to a least square method; 4, deriving a composite material helical structure compression strength analytical expression by adopting principaldirection stress and a TsaiHill failure criterion; the invention is convenient and efficient, and the compression rigidity and the compression strength of the spiral structure of the composite material can be conveniently and quickly predicted only by determining performance parameters and geometrical parameters of component materials.

Description

technical field [0001] The invention provides a method for predicting compression stiffness and compression strength of a helical structure of composite materials considering geometric nonlinearity, and belongs to the field of composite material design. Background technique [0002] Helical structures can store and release strain energy through elastic deformation, and have been widely used in aerospace and automotive fields. The traditional helical structure is generally made of metal materials. Although the manufacturing process is simple and the price is low, there is an obvious problem of large weight, which does not meet the requirements of lightweight design. Using a composite material helical structure instead of a metal helical structure can effectively reduce the weight of the helical structure and take into account excellent mechanical properties. The cost of directly measuring the compression stiffness and compressive strength of the helical structure of composit...

Claims

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Application Information

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IPC IPC(8): G06F30/20G06F30/17G06F113/26G06F119/14
CPCG06F30/20G06F30/17G06F2113/26G06F2119/14
Inventor 白江波刘天伟
Owner BEIHANG UNIV
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