Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Method for predicting transverse tensile strength of coreless brittle fibers

A technology of transverse stretching and brittle fibers, applied in the direction of strength characteristics, using stable tension/pressure test material strength, measuring devices, etc., can solve the problem of not considering the influence of the internal stress distribution of the fiber, etc. High calculation accuracy, efficient and convenient calculation process

Pending Publication Date: 2020-10-30
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
View PDF6 Cites 4 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In the prior art, Jeffrey I. Eldridge proposed a method for testing the transverse tensile strength of a cored fiber, which did not consider the influence of the local pressure on the load contact surface on the internal stress distribution of the fiber
A method for solving the transverse tensile strength considering the local pressure of the loaded contact surface has not been found in the prior art

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Method for predicting transverse tensile strength of coreless brittle fibers
  • Method for predicting transverse tensile strength of coreless brittle fibers
  • Method for predicting transverse tensile strength of coreless brittle fibers

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0064] In the following, the present invention will be further described in conjunction with an example of testing the transverse tensile strength of a coreless silicon carbide fiber and the accompanying drawings, but the test object is not limited to the silicon carbide fiber.

[0065] The invention discloses a method for testing the transverse tensile strength of coreless brittle fibers. The researchers first prepared a single fiber sample with a length of about 200 μm for the brittle fiber to be tested, and performed a single fiber compression test on the sample to obtain the failure load Fcr for the fiber to undergo radial tensile failure. Then calculate the transverse tensile strength of the fiber by Fcr and fiber properties.

[0066] step 1:

[0067] Test a coreless SiC fiber with a diameter of 28μm, such as image 3 Shown. The longitudinal elastic modulus of the fiber is 420 GPa, the transverse elastic modulus is 240 GPa, and the Poisson's ratio is 0.15. Twenty coreless SiC...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention provides a method for predicting the transverse tensile strength of coreless brittle fibers. The method comprises the following steps of: step 1, preparing a fiber sample; 2, carrying out a fiber compression test by using a nanoindentor to obtain fracture load data; and 3, calculating a load contact angle according to the fracture load, establishing a fiber compression model, and substituting the fracture load and the load contact angle into the fiber compression model to calculate the stress of the vertical radial surface of a fiber, the stress at the circle center of the vertical radial surface of the fiber being the maximum transverse tensile strength of the fiber sample. The method is high in calculation precision; the influence of the size of a compression contact surface on the internal stress distribution of the fiber is considered; the comparison conformity of a calculation result and a finite element analysis result is high. The calculation process of the methodis efficient and convenient; the transverse tensile strength of the fiber can be calculated only by modifying the contact surface angle and the fracture load, and a series of complex operations such as establishing a model by a finite element method, dividing a load area with a certain angle on a curved surface, applying a constraint load and dividing grids are avoided.

Description

Technical field [0001] The invention relates to a method for predicting the transverse tensile strength of coreless brittle fibers, in particular to a method for predicting the transverse tensile strength of coreless brittle fibers by using a nanoindenter to perform a fiber compression test. Background technique [0002] Fiber-reinforced composite materials have the advantages of (1) high specific strength and large specific modulus (2) designability of material properties (3) good corrosion resistance and durability (4) small thermal expansion coefficient, etc., and are used in aerospace, automotive, Sports and other industries are widely used. Brittle fibers such as silicon carbide fibers, carbon fibers, and boron fibers have the advantages of high hardness and high specific modulus, and are widely used in the reinforcement phase of composite materials. [0003] When the composite material is laterally compressed, because the lateral stiffness of the fiber is usually greater tha...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): G01N3/08G01N1/36G01N3/06
CPCG01N3/08G01N1/36G01N3/068G01N2001/366G01N2001/364G01N2203/0017G01N2203/0082G01N2203/028G01N2203/0647G01N2203/0676G01N2203/0682
Inventor 孙志刚邹鹏健陈西辉刘茜牛序铭宋迎东
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products