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Design and Analysis of Composite Structures for Automotive Applications

Chassis and Drivetrain

 

Vladimir Kobelev

Department of Natural Sciences, University of Siegen, Germany

 

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Automotive Series

Advanced Battery Management Technologies for Electric Vehicles

Rui Xiong, Weixiang Shen

Noise and Vibration Control in Automotive Bodies

Jian Pang

Automotive Power Transmission Systems

Yi Zhang, Chris Mi

High Speed Off‐Road Vehicles: Suspensions, Tracks, Wheels and Dynamics

Bruce Maclaurin

Hybrid Electric Vehicles: Principles and Applications with Practical Perspectives, 2nd Edition

Chris Mi, M. Abul Masrur

Hybrid Electric Vehicle System Modeling and Control, 2nd Edition

Wei Liu

Thermal Management of Electric Vehicle Battery Systems

Ibrahim Dincer, Halil S. Hamut, Nader Javani

Automotive Aerodynamics

Joseph Katz

The Global Automotive Industry

Paul Nieuwenhuis, Peter Wells

Vehicle Dynamics

Martin Meywerk

Modelling, Simulation and Control of Two‐Wheeled Vehicles

Mara Tanelli, Matteo Corno, Sergio Saveresi

Vehicle Gearbox Noise and Vibration: Measurement, Signal Analysis, Signal Processing and Noise Reduction Measures

Jiri Tuma

Modeling and Control of Engines and Drivelines

Lars Eriksson, Lars Nielsen

Advanced Composite Materials for Automotive Applications: Structural Integrity and Crashworthiness

Ahmed Elmarakbi

Guide to Load Analysis for Durability in Vehicle Engineering

P. Johannesson, M. Speckert


Foreword

From a materials science point of view, composite materials of glass and carbon fibers have a specific potential and already some practical importance in several applications under high dynamic loads. Comparing the fibers, glass fibers are the better material for spring applications because their lower modulus of elasticity compared to carbon fibers. This is favorable in terms of high strokes and deformation requirements. Due to their high specific strength and the stiffness of composite materials, it is in principle possible to achieve weight savings of 30 – 70% of the weight of a steel spring depending on application. In addition to reduce the unsprung masses for suspension, it is also possible to improve driving dynamics as well as noise, vibration and hardness behavior (NVH), since the material properties are better in some significant areas. Furthermore, due to the high corrosion resistance and resistance against other environmental influences, surface protection is not necessary in most of the applications.

However, the usage of composite materials for springs have not reached high quantities due to some limitations. Load transmission requires special designs. Considering suspension coil springs, high loads transverse to the main load direction occur. Therefore, the load transmission does not follow ideally to the fiber direction and only medium loads can act on the matrix. In addition, in the case of large‐scale production and the available manufacturing processes, value adjustments must be made in comparison with units made of steel. These are currently the focus of research and development efforts throughout the world. Endless, unidirectional fiber materials, such as those used for structural elements in automotive engineering, exhibit strong anisotropic, i.e. direction‐dependent, properties. The fibers used are oriented with respect to the loads that occur. Therefore, the leaf spring, where loading results almost in tension stresses of the fibers is the perfect match with composite materials. Huge weight reduction up to 75% is possible to achieve by using the material properties and the design flexibility of glass fiber reinforced composite in the best way. A single composite tension leaf spring can substitute a steel multi‐leaf spring with a progressive spring load characteristic. The special design leads to a very homogenous, progressive spring characteristic and therefore, a better driving performance. Furthermore, we know already some designs for suspension steel coil springs substitution such as one‐by‐one substitution by composite coil spring and a meander spring design. In both case these springs do need special tools for the design and did not reach the market breakthrough due to huge different load‐rate requirements within the platforms.

There are some processes existing for the production of glass fiber composite springs. Nevertheless, the prepreg process (pre‐impregnated fibers) has proven itself as the best due to the realizable good properties under dynamic loads. Prepreg processes result in an optimal adhesive strength due to low porosity and allows flexibility in design, such as geometry, width and height of the spring. It is also possible to produce the elements of chassis in general and suspension particular using the resin injection process. For this resin injection process, a fiber structure is first produced from the dry reinforcement fibers, which follows the desired component geometry. If required, structural cohesion can be achieved using textile methods, such as sewing or bonding, which bond the fibers together. Such fiber structures are called preforms. The injection of the resin influences the orientation of the fibers and therefore, those springs do not reach the performance of prepreg composites due to potential ondulation.

Automotive manufacturers' requirements for carbon dioxide reduction, lower vehicle weight, the reduction of unsprung masses and the robustness of the springs, especially in the event of corrosion, will further increase in the future. The optimal application of the materials used plays a decisive role, supported by material properties, best technology and processes as well as an efficient design. Therefore, alternative materials, such as composites, may become higher importance for dynamic loaded suspension applications.

Prof. Dr. Vladimir Kobelev was born in Rostow‐na Donu, Russian Federation. He studied Physical Engineering at the Moscow Institute of Physics and Technology. After his PhD at the Department of Aerophysics and Space Research (FAKI), he habilitated at the University of Siegen, Scientific‐Technical Faculty. Today, Prof. Kobelev is lecturer and APL professor at the University of Siegen in the subject area of Mechanical Engineering.

In his industrial career, Prof. Kobelev is an employee at Mubea, a successful automotive supplier located near Cologne/Germany. In the Corporate Engineering Department, Prof. Kobelev is responsible for the development of calculation methods and physical modeling of Mubea components.

Joerg Neubrand

CTO, Managing Director and

Member of the Executice Board of the Mubea Group


Series Preface

Fuel efficiency continues to “drive” significant research and development in the automotive sector. In many instances, this is propelled by regulations that target reduced emissions as well as reduced fuel consumption. Even with more efficient vehicles and electric hybrid or purely electric driven systems, the need for reduced energy consumption is demanded by the market. This is due to the fact that the customer base is demanding increased efficiency as this brings better performance, lower costs and extended range of the vehicle. One clear means by which fuel efficiency can be enhanced is by reducing the weight of the vehicle. Lightweighting can be accomplished by a number of means, one of which is lighter weight material substitution. That is to say, one may substitute a lighter material for a heavier one on a vehicle component. Composites have been used to replace metal components in efforts to lightweight aircraft for decades. More recently, advances in materials, manufacture, and design have made composites cost effective and viable in the automotive sector. Two major stumbling blocks that have hindered composite use in the automotive sector are the cost of the composite components, and the ability to rapidly and economically produce such components in quantities that are needed by the automotive sector. Recently, these stumbling blocks have been overcome. However, for most commercial automotive applications, composites remain relegated to less critical elements of the vehicle system such as body panels. The use of composite for more critical vehicle applications such as suspension and drive train elements have been left to extremely demanding automotive scenarios such as Formula One. However, this scenario is about to change.

Design and Analysis of Composite Structures for Automotive Applications, provides an in‐depth technical analysis of critical suspension and drive train elements with a focus on composite materials. This includes basic principles for the design and optimization of critical vehicle elements using composite materials, as well as classical concepts related to mass reduction in automotive systems. The author, Professor Kobelev, skillfully integrates concepts related to vehicle parameters such as stiffness into overall vehicle dynamics using closed form solutions that are described in exquisite detail. The discussions focus on key elements of the vehicle including suspension and powertrain. These discussions are both comprehensive as well as the first of their kind in a text book, making this text an important reference for any automotive engineer on the leading edge.

Design and Analysis of Composite Structures for Automotive Applications is part of the Automotive Series that addresses new and emerging technologies in automotive engineering, supporting the development of next generation vehicles using next generation technologies, as well as new design and manufacturing methodologies. The series provides technical insight into a wide range of topics that is of interest and benefit to people working in the advanced automotive engineering sector. Design and Analysis of Composite Structures for Automotive Applications is a welcome addition to the Automotive Series as it primary objective is to supply pragmatic and thematic reference and educational materials for researchers and practitioners in industry, and postgraduate/advanced undergraduates in automotive engineering. The text is a state‐of‐the art book written by a leading world expert in composites and its application to suspensions and is a welcome addition to the Automotive Series.

Thomas Kurfess

March 2019

List of Symbols and Abbreviations

EL
Longitudinal modulus of elasticity of composite parallel to fiber direction
ET
Transverse modulus of elasticity of composite perpendicular to the fiber direction
GTL
Transverse‐longitudinal shear modulus of composite
GTT
Transverse shear modulus of composite
rf
Radius of the fiber
images
External radii of hypothetical matrix cylinders
Vf
Fiber volume content
Vm
Matrix volume content, Vm = 1 − Vf
νTL
Transverse‐longitudinal Poisson ratio of a composite
νTT
Transverse Poisson's ratio of a composite
Ef
Longitudinal modulus of elasticity of fibers
Ef. T
Transverse modulus of elasticity of fibers
Em
Modulus of elasticity of matrix (resin)
νm
Poisson's ratio of matrix (resin)
Gm
Shear modulus of matrix (resin)
Gf. TL
Transverse‐longitudinal shear modulus of fibers
νf. TL
Transverse‐longitudinal Poisson's ratio of fibers
νf. TT
Transverse Poisson's ratio of fibers
S = [Sijpq]
Compliance tensor of rank four, i, j, p, q = 1, 2, 3
C = [Cijpq]
Elasticity tensor of rank four
C(0) = [cijpq]
Elasticity tensor of rank four, in the layer coordinate system
S(0) = [sijpq]
Compliance tensor of rank four, in the layer coordinate system
I = [Iijpq]
Fourth rank identity tensor
σ
Voigt's stress vector
ɛ
Voigt's strain vector
C
Voigt's elasticity matrix
images
Kelvin's stress vector
images
Kelvin's strain vector
images
Kelvin's elasticity tensor
S(0)
Compliance matrix in Voigt's notation in intrinsic coordinates
images
Compliance matrix in Kelvin's notation in intrinsic coordinates
t = [tlk]
Transformation (rotation) square 3×3 or 2×2 matrix
Tσ
σ‐transformation (rotation) square 6×6 matrix, in Voigt's notation
Tε
ε‐transformation (rotation) square 6×6 matrix, in Voigt's notation
images
Transformation (rotation) square 6×6 matrix, in Kelvin's notation
A
Plane modulus quadrant, square 3×3 matrix (entries for the membrane elasticity tensor) in Voigt's notation
B
Coupling quadrant, square 3×3 matrix (entries for the coupling elasticity tensor) in Voigt's notation
D
Plate quadrant, square 3×3 matrix (entries for the bending elasticity tensor) in Voigt's notation
ɛT = [ε11, ε22, γ12 = 2ε12]
Strain vector in Voigt's notation
κT = [κ11, κ22, 2κ12]
Curvature vector in Voigt's notation
NT = [N11, N22, N12]
In‐plane forces vector in Voigt's notation
MT = [M11, M22, M12]
Bending moments vector in Voigt's notation
Q
Reduced stiffness matrix in Voigt's notation
images
σ‐transformation (rotation), square 3×3 matrix in Voigt's notation
images
ε‐Transformation (rotation) square 3×3 matrix in Voigt's notation
images
Plane modulus quadrant, square 3×3 matrix (entries for the membrane elasticity tensor) in Kelvin's notation
images
Coupling quadrant, square 3×3 matrix (entries for the coupling elasticity tensor) in Kelvin's notation
images
Plate quadrant, square 3×3 matrix (entries for the bending elasticity tensor in Kelvin's notation
images
Strain vector in Kelvin's notation
images
Curvature vector in Kelvin's notation
images
In‐plane reaction forces, vector in Kelvin's notation
images
Bending moments, vector in Kelvin's notation
images
Reduced stiffness matrix in Kelvin's notation
images
Transformation matrix for rotation (3×3) in Kelvin's notation
Xt, Xc
Tensile or compressive strengths in the fiber direction
Yt, Yc
Tensile or compressive strengths in the transverse direction
images
Matrix of the Mises–Hill criterion, Voigt's notation in intrinsic coordinates
F, G, H, L, M, N
Characteristic values of the Mises–Hill criterion
Λi
Eigenvalues of the Mises–Hill criterion, i = 1..6
images
Ultimate normal stresses in the Mises–Hill criterion
images
Ultimate shear stresses in the Mises–Hill criterion
images
Matrix of the Mises–Hill criterion, Kelvin's notation in intrinsic coordinates
Φ
Rotation angle of fibers in the plane “1–2”
images
Matrix of the Mises–Hill criterion in the rotated axes, Kelvin's notation
images
Matrix of the pressure‐sensitive Mises–Hill criterion, Voigt's notation in intrinsic coordinates
images
Matrix of the pressure‐sensitive Mises–Hill criterion, Kelvin's notation in intrinsic coordinates
F(2), F(4), F(6)
Tensors of the 2nd, 4th and 6th ranks of the Goldenblat–Kopnov tensor fracture criterion
σf
Axial stresses in cylindrical fibers
σm
Axial stresses in hollow matrix cylinders
τ
Shear stress at the fiber surface
τp
Yield point of the matrix
p(z), q(z)
Auxiliary functions, p = um − uf, q = um + uf.
um,uf
Axial displacements of matrix and fiber cylinders
λ, μ,images
Parameters of the length dimension
images
Parameters of the inverse length dimension
lp
Length of the plastic zone
Rf, Rf
Crack extension resistance of fibers and matrix
images
Auxiliary modules
Kf, Km
Fracture toughness of fibers and matrix
dUe/da
Energy release rate per thickness unit
dUf/da
Crack extension resistance per thickness unit
ϕi(ρ, η)
Potential functions,i = 1, 2
a = lc/2rf
Dimensionless length of adhesive or debonding region
Kmax, Kmax
Maximum and minimum stress intensity factor
Y(a)
Dimensionless parameter that reflects the geometry
cf = cf(Rσ)
Material constant of matrix or resin for a given stress ratio Rσ
Rσ = Kmin/Kmax
Stress ratio of cyclic load
pc(K) = Kp
Paris–Erdogan crack propagation function
CT
Torsional rigidity of bar (driveshaft)
Ib1, Ib2
Moment of inertia of cross section with respect to both bending axes
images
Critical torque in Greenhill's problem
We(Φ)
Density of elastic energy
We*(Φ)
Elastic energy per mass unit (specific elastic energy)
images
Ultimate elastic energy per mass unit (specific ultimate elastic energy)
images
Ultimate elastic energy
XE,YE,ZE
Axes of the earth‐fixed coordinate system
XV,YV,YV
Axes of the vehicle‐fixed coordinate system
X, Y, Z
Axes of the horizontal coordinate system
XW, YW,ZW
Axes of the wheel coordinate system
ϕ
Roll angle
θ
Pitch angle
ψ
Yaw angle
β
Sideslip angle of a vehicle
ς =  ψ − β
Course angle
SX;V
Circumferential slip
ω
Rotational speed of a wheel
ω0
The rotational speed of a straight and freely rolling wheel
α
Sideslip angle of a wheel
μX,W
Coefficients of circumferential force
μY,W
Coefficients of lateral force
Cα
Cornering stiffness
Cαf,Cαr
Cornering stiffness of front and rear tire
Iz
Mass moment of inertia of the vehicle around the vertical axis
m
Mass of a vehicle
Lf
Horizontal distance from front axle to center of mass
Lr
Horizontal distance from rear axle to center of mass
Lw = Lf + Lr
Wheel base
δ
Steer angle at the wheel (part of steer angle due to steer)
images
Steer angle gradient
δa
Steer angle according to Ackermann
ΔV
External excitation in the course of steering
ωV
Yaw circular frequency of a vehicle
DV
Damping factor of a vehicle's yaw oscillation
L0
Free length of a helical spring
Lrel
Released length of a helical spring
Lcomp
Compressed length of a helical spring
Lc
Close up length of a compressed spring
s = Lrel − Lcomp
Spring travel
c
Axial compression or extension spring constant
cθF
Compression‐twist spring rate
cθ
Twist spring rate
Ue
Elastic energy
Uf
Work of applied forces
F
Axial force on a helical spring
Mθ
Axial torque on a helical spring
c*
Design value for a spring constant
τw
Ideal stress at solid height
dopt
Optimal diameter of a wire
mopt
Lower boundary for spring mass
ϖ
Middle surface of an undeformed conical spring
Ω
Middle surface of a deformed conical spring
tc
Thickness of an anisotropic conical spring
ra,rb
Inner and outer radius of the middle surface of a free conical spring
Ra,Rb
Outer radius of the middle surface of a deformed conical spring
Δ = rb/ra
Ratio of the outer radius to inner radius of a conical spring
images
Inversion point of a conical spring
za, zb
Heights of the inner and outer edges of a free spring
Za, Zb
Heights of the inner and outer edges of a deformed spring
ε1
Circumferential mid‐surface strain of a conical spring
κ1
Circumferential curvature changes of a conical spring
images
Effective elastic modulus
images
Effective orthotropic elastic modulus
sQ = sb + ss
Total transversal displacement of a helical spring
Q
Shear force of equivalent column for a helical spring
MB
Bending moment of a helical spring
mB
External torque per unit length of a helical spring
fQ
External load in the transverse direction of a helical spring
C44IT
Twist stiffness of a wire with respect to its axis
C33Ib
Stiffness of a spring wire in the case of bending in a binormal direction
C33In
Stiffness of a spring wire in the case of bending in a normal direction
so(z)
Initial transverse deflection of a helical spring
vo(z)
Initial transverse velocity of a helical spring
ωk
Circular natural frequency in the order of k of a helical spring
ξ = L0/D
Slenderness ratio of a helical spring
μ = L/L0
Dimensionless length of a helical spring
Ωk
Dimensionless frequency of transverse oscillations in the order of k of a helical spring
images
Critical deflection during compression from the free length of a helical spring
images
Critical deflection during expansion from the flattened state of a helical spring
f(σeff, t)
Anisotropic stress function for creep
t
Time for creep
images
Deviatoric component of creep strain
sij
Deviatoric component for creep stress
σeq
Mises equivalent stress
cτ
Creep constant for shear strain
cσ
Creep constant for uniaxial strain
γe
Elastic component of shear strain
γc
Creep component of shear strain
images
Torque at the moment t = 0
MT(t)
Torque as a function of time
images
Spring force at the moment t = 0
Fz(t)
Spring force as a function of time
images
Bending moment at the moment t = 0
MB(t)
Bending moment as a function of time
ΦT(t),ΦB(t),ΦH(t)
Relaxation functions for twisting, bending and helical spring
f = ∂f/∂z, or ∂f/∂x1, or ∂f/∂ξ1
“Prime” denotes a derivative with respect to a coordinate: z, or x1, or ξ1
images
“Dot” denotes a time derivative

Abbreviations

AF
Aramid fiber
AFRP
Aramid fiber reinforced plastic
Autoclave
Heated pressure tank
CE
Cyanate ester resin
CF
Carbon fiber
CFRP
Carbon fiber reinforced plastic
DSA
Driveshaft axis
EP
Epoxy resin
Fabric
Biaxially woven textile
FRP
Fiber reinforced plastic
GF
Glass fiber
GFRP
Glass fiber reinforced plastic
HM
High modulus
HT
High tensile strength
Laminate
Layer construction of cured, individual plies
Matrix
Resin in which the fibers are embedded
NVH
Noise, vibration and hardness
PA
Polyamide
PEEK
Polyetheretherketone
PF
Phenolic resin
PMMA
Polymethyl‐methylacrylate
PPS
Polyphenyl sulfide
Prepreg
Preimpregnated fibres – fibers or textiles pre‐saturated with resin
PU
Polyurethane resin
Roving
Soft strand of twisted, attenuated, freed of external matter fiber ready to conversion into yarn
RTM
Resin transfer molding – resin is injected into an enclosed mold in which fibers have been placed
Tg
Glass transition temperature
UD
Unidirectional fibers are oriented in only one direction
UP
Unsaturated polyester
VE
Vinyl ester resin