Structure features of braided materials make unobvious possibilities of using traditional multilayered material models, or so-called layer-by-layer analysis models (LLAM), successfully used for composites manufactured by winding or laying. The objective of the article is to demonstrate applicability of using LLAM to predict the elasticity constants for the composites manufactured by braiding. The conclusion is based on comparing the results of calculations and experiments. Experimental values of elasticity characteristics (elastic moduli and Poisson’s ratios) of five different carbon fiber reinforced plastic (CFRP) structures under study were determined during tension tests of strip samples and ring specimens cut-out from thin-walled CFRP braided shells with an internal diameter of 270 mm. Deformations in the tests were measured using strain gauges, elasticity characteristics were determined from linear approximation of initial parts of stress-strain curves. Structural elements with the same direction of fibers were combined into conditional unidirectional plies (CUP). Experimental values of elasticity characteristics of all structures were used as input data for solving the problem of identifying the CUP characteristics. Relationship between the CUP characteristics and the characteristics of complex structures was set in accordance with the traditional LLAM. Two types of CUP were considered in braided structures: a) the yarns were laid along the rectilinear shell generator, b) the yarns were laid along the helix line at specified angles to the rectilinear generator. It was supposed that mentioned CUPs had different elasticity characteristics despite of the same types of fibers and binder. The solution of identification problems enabled one to determine elasticity characteristics of two types of CUP which give minimal possible differences between predicted and experimental values of the elasticity characteristics for all examined structures. These differences did not exceed the experimental data scatter. Such result is proof that traditional LLAM can be used for calculating and predicting elasticity characteristics of braided structures.

1.
Kablov
,
E.N.
(
2012
).
Strategic directions in materials development and technologies of their machining for the period of up to 2030
.
Aviation materials and technologies
, (S),
7
.
2.
Grashscenkov
,
D.V.
, &
Chursova
,
L. V.
(
2012
).
Strategy of development of composite and functional materials
.
Aviation materials and technologies, (S)
,
231
242
.
3.
McClain
,
M.
, &
Goering
,
J.
(
2012
).
Overview of recent developments in 3D structures
.
Albany Eng Compos
,
1
12
.
4.
Lebel
,
L. L.
, &
Nakai
,
A.
(
2012
).
Design and manufacturing of an L-shaped thermoplastic composite beam by braid-trusion
.
Composites Part A: Applied Science and Manufacturing
,
43
(
10
),
1717
1729
.
5.
Donetskiy
.
K.I.
,
Khrulkov
,
A.V.
,
Kogan
,
D.I.
,
Belinis
,
P.G.
, &
Lukyanenko
,
Yu. V.
(
2013
).
Use of volume reinforcing performs in PCM components manufacture
.
Aviation materials and technologies
, (
1
(
26
)).
6.
Carey
,
J. P.
,
Melenka
,
G. W.
,
Hunt
,
A. J.
, &
Ayranci
,
C.
(
2017
). Introduction to braided composite material behavior. In
Handbook of Advances in Braided Composite Materials
(pp.
207
237
).
Woodhead Publishing
.
7.
Donetskiy
,
K.I.
,
Karavaev
,
R.Yu.
,
Raskutin
,
A.E.
, &
Dun
,
V.A.
(
2019
).
Carbon fiber reinforced plastic based on volume reinforcing triaxial braided preform
.
Works of ARIAM
, (
1
(
73
))
8.
Dushin
,
M.I.
,
Khrulkov
,
A.V.
,
Mukhametov
,
R.R.
, &
Chursova
,
L. V.
(
2012
).
Characteristic features of manufacturing products of PCM using the method of impregnation under pressure
.
Aviation materials and technologies
, (
1
(
22
)). DOI:
9.
Tao
,
G.
,
Liu
,
Z.
,
Lv
,
M.
, &
Chen
,
S.
(
2011
).
Research on manufacture and test of advanced composite material flange
.
Open Mechanical Engineering Journal
,
5
,
87
96
.
10.
Donetskiy
,
K.I.
,
Kogan
,
L.I.
, &
Khrulkov
,
A. V.
(
2014
).
Properties of polymer composite materials manufactured on the basis of braided preforms
.
Works of ARIAM
, (
3
).
11.
Zinoviev
,
P.A.
(
1990
).
Strength, thermoelastic and dissipative characteristics of composites
.
Composite materials: Reference book
/ Ed.
V. V.
Vasiliyev
,
Yu.M.
Tarnopolkiy
–М.:
Mashinostroyenie
,
232
267
.
12.
Alfutov
,
N.A.
(
1984
).
Calculation of multilayered plates and shells made of composite materials
.
Ripol Classic.
13.
Zinoviev
,
P. A.
, &
Tairova
,
L. P.
(
1995
).
Identifying the properties of individual plies constituting hybrid composites
.
Inverse Problems in Engineering
,
2
(
2
),
141
154
.
14.
Kayumov
,
R.A.
,
Strakhov
,
D.Ye.
,
Shakirzyanov
,
F.R.
,
Gimranov
,
L.R.
, &
Mangusheva
,
A.R.
(
2016
).
Composites rigidity characteristics identification
.
Bulletin of the Kazan technological university
,
19
(
24
).
15.
Sarbayev
,
B.S.
, &
Baryshev
,
A.N.
(
2017
).
Calculation of deformation diagrams of composite materials with woven filler using plasticity endochronic theory
.
Bulletin of Bauman Moscow State Technological University. Machine building series
, (
4
(
115
)).
16.
Smerdov
,
A.A.
, &
Tairova
,
L. P.
(
2015
).
Identification of elasticity and strength characteristics of a unidirectional ply in multilayered carbon fiber reinforced plastics - implementation peculiarities when studying the effect of nano-additives
.
Structures of composite materials
, (
2
),
52
58
.
17.
Smerdov
,
A.A.
,
Tairova
,
L. P.
&
Timofeyev
,
I.A.
(
2018
).
Experimental study of tube samples made of composite materials based on braided seamless multilayered carbon frames and polymer, carbon and ceramic matrices
.
Structures of composite materials
, (
2
),
52
59
.
18.
Zinoviev
,
P. A.
, &
Smerdov
,
A. A.
(
1994
).
General Composite Analyzer & Designer: Software and User’s Manual.
19.
Adamov
,
A.A.
,
Laptev
,
M.Yu.
, &
Gorshkova
,
E.G.
(
2012
).
Analysis of domestic and foreign normative base on mechanical tests of polymer composite materials
.
Structures of composite materials
, (
3
),
72
77
20.
Bechtel
,
A. J.
, &
Zureick
,
A. H.
(
2018
).
Structural Engineering Test for Determining the Circumferential Modulus of Circular Pipes and Tubes
.
Materials Performance and Characterization
,
7
(
1
),
259
274
.
This content is only available via PDF.
You do not currently have access to this content.