Fatigue wear is a critical concern in friction and wear engineering. It involves progressive damage accumulation in materials subjected to , leading to eventual failure. Understanding fatigue wear mechanisms helps engineers design more durable and reliable systems.
Fatigue wear occurs in three stages: , propagation, and material removal. Various factors influence this process, including material properties, surface conditions, loading conditions, and environmental factors. Engineers must consider these elements when designing wear-resistant systems for different applications.
Definition of fatigue wear
Progressive damage accumulation in materials subjected to cyclic loading or stress
Occurs below the of the material, leading to eventual failure
Crucial concept in friction and wear engineering due to its impact on component lifespan and safety
Mechanisms of fatigue wear
Involves three main stages crack initiation, propagation, and material removal
Occurs at stress concentrations or material defects, gradually weakening the component
Understanding these mechanisms helps engineers design more durable and reliable systems
Crack initiation
Top images from around the web for Crack initiation
Investigation of the Relation between Rolling Contact Fatigue Property and Microstructure on the ... View original
Is this image relevant?
Frontiers | Characterization of Surface Fatigue Crack Nucleation and Microstructurally Small ... View original
Is this image relevant?
Investigation of the Relation between Rolling Contact Fatigue Property and Microstructure on the ... View original
Is this image relevant?
Frontiers | Characterization of Surface Fatigue Crack Nucleation and Microstructurally Small ... View original
Is this image relevant?
1 of 2
Top images from around the web for Crack initiation
Investigation of the Relation between Rolling Contact Fatigue Property and Microstructure on the ... View original
Is this image relevant?
Frontiers | Characterization of Surface Fatigue Crack Nucleation and Microstructurally Small ... View original
Is this image relevant?
Investigation of the Relation between Rolling Contact Fatigue Property and Microstructure on the ... View original
Is this image relevant?
Frontiers | Characterization of Surface Fatigue Crack Nucleation and Microstructurally Small ... View original
Is this image relevant?
1 of 2
Begins at points (surface irregularities, inclusions, or grain boundaries)
Involves formation of persistent slip bands due to cyclic plastic deformation
Microstructural changes lead to the nucleation of microcracks
Crack propagation
Microcracks grow and coalesce into larger cracks under continued cyclic loading
Follows Paris' Law, relating crack growth rate to stress intensity factor range
Influenced by material properties, loading conditions, and environmental factors
Material removal
Final stage where cracks reach critical size, causing material separation
Results in the formation of wear particles and surface degradation
Can lead to catastrophic failure if not detected and addressed in time
Factors influencing fatigue wear
Multiple variables affect the fatigue wear process and component lifespan
Understanding these factors is crucial for designing wear-resistant systems
Engineers must consider the interplay of these factors in friction and wear applications
Material properties
Yield strength affects resistance to plastic deformation and crack initiation
Wheel bearings and CV joints are subject to rolling contact fatigue
Aerospace structures
Aircraft fuselage and wings experience cyclic pressurization and depressurization
Turbine blades in jet engines undergo high-frequency vibrations and thermal cycling
Landing gear components face high-impact loads during takeoff and landing
Industrial machinery
Gears and bearings in power transmission systems experience rolling contact fatigue
Pressure vessels and pipelines undergo cyclic pressurization and thermal stresses
Robotic arms and manufacturing equipment face repetitive loading cycles
Modeling and prediction of fatigue wear
Accurate modeling and prediction of fatigue wear are essential for reliable component design
These approaches help engineers estimate component lifespan and optimize maintenance schedules
Combining different modeling techniques provides a comprehensive understanding of fatigue behavior
Stress-life approach
Based on S-N curves relating stress amplitude to cycles to failure
Utilizes or endurance limit for infinite life design
Incorporates factors for surface finish, size effect, and loading type (Marin factors)
Strain-life approach
Considers both elastic and plastic strain components in fatigue life prediction
Uses Coffin-Manson relationship and cyclic stress-strain curves
Accounts for local plasticity and notch effects more accurately than stress-life approach
Fracture mechanics approach
Applies linear elastic fracture mechanics (LEFM) principles to fatigue crack growth
Utilizes Paris' Law to predict crack growth rate based on stress intensity factor range
Incorporates threshold and critical stress intensity factors for crack initiation and final failure
Fatigue wear standards and specifications
Standards and specifications provide guidelines for fatigue testing, analysis, and design
These documents ensure consistency and reliability in fatigue-related engineering practices
Engineers must stay updated on relevant standards to maintain compliance and best practices
ASTM standards
ASTM E466 Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials
ASTM E606 Standard Test Method for Strain-Controlled Fatigue Testing
ASTM E647 Standard Test Method for Measurement of Fatigue Crack Growth Rates
ISO standards
ISO 1143 Metallic materials — Rotating bar bending fatigue testing
ISO 12106 Metallic materials — Fatigue testing — Axial-strain-controlled method
ISO 12107 Metallic materials — Fatigue testing — Statistical planning and analysis of data
Industry-specific guidelines
Aerospace MMPDS (Metallic Materials Properties Development and Standardization) handbook
Automotive SAE J1099 Technical Report on Low Cycle Fatigue Properties Ferrous and Non-Ferrous Materials
Nuclear ASME Boiler and Pressure Vessel Code Section III Rules for Construction of Nuclear Facility Components
Key Terms to Review (21)
Composites: Composites are materials made from two or more constituent materials with significantly different physical or chemical properties. When combined, these materials produce a composite that has enhanced properties compared to the individual components, making them particularly valuable in applications requiring high strength-to-weight ratios and improved fatigue resistance.
Crack initiation: Crack initiation is the initial phase in the development of cracks within a material, often leading to failure or fracture. This process typically occurs due to various stressors such as fatigue, environmental factors, or material defects. Understanding crack initiation is crucial for predicting the lifespan of materials and components, especially under cyclic loading conditions that contribute to fatigue wear.
Crack Propagation: Crack propagation refers to the growth and advancement of a crack within a material, often influenced by various stresses and environmental factors. It plays a critical role in the failure of materials under cyclic loading, where repeated stress can lead to fatigue wear, causing small cracks to expand over time until catastrophic failure occurs. Understanding how cracks propagate is essential for predicting material durability and designing components that can withstand cyclic stress without failing.
Cyclic Loading: Cyclic loading refers to the application of repeated loads on a material or component over time, causing variations in stress and strain. This process is critical to understanding how materials behave under conditions that mimic real-world usage, where loads may not be constant. The effect of cyclic loading can lead to fatigue wear, which ultimately contributes to the failure of materials through the initiation and propagation of cracks.
Design optimization: Design optimization is the process of adjusting and improving a design to achieve the best performance or efficiency while meeting specific constraints and requirements. This concept involves analyzing various design parameters, considering trade-offs, and utilizing mathematical and computational tools to enhance functionality and reduce costs or risks.
Fatigue crack growth test: The fatigue crack growth test is an experimental method used to evaluate how cracks propagate in materials under cyclic loading conditions. This test simulates real-world service environments where materials experience repeated stresses, allowing researchers to measure the rate at which cracks grow and ultimately lead to material failure, making it essential in understanding fatigue wear.
Fatigue limit: The fatigue limit, also known as the endurance limit, is the maximum stress level a material can withstand for an infinite number of loading cycles without experiencing failure. This concept is crucial in understanding how materials behave under repeated loading conditions, particularly when elastic and plastic deformations occur, as well as in the context of fatigue wear which leads to the eventual failure of materials.
High-cycle fatigue: High-cycle fatigue refers to the phenomenon where materials experience failure after a large number of loading cycles, typically greater than 10,000 cycles, at relatively low stress levels. This type of fatigue is crucial in understanding the durability of materials and components that undergo repetitive loading, making it essential for designing parts in various engineering applications.
Low-cycle fatigue: Low-cycle fatigue refers to the failure of materials due to cyclic loading at relatively low numbers of cycles, typically less than 10,000. This type of fatigue occurs when a material is subjected to high levels of stress that lead to significant plastic deformation, making it distinct from high-cycle fatigue, where the stresses are lower and the number of cycles is higher. Understanding low-cycle fatigue is crucial in assessing the durability and longevity of components subjected to fluctuating loads, especially in critical engineering applications.
Metals: Metals are a class of materials characterized by their high electrical and thermal conductivity, malleability, ductility, and metallic luster. They play a crucial role in various engineering applications, especially concerning friction and wear, due to their unique properties that influence adhesion, deformation, and wear mechanisms.
Paris Law: Paris Law describes the relationship between the stress intensity factor and the rate of fatigue crack growth in materials, stating that the rate of crack growth is proportional to the stress intensity factor range. This law is vital for understanding how materials behave under cyclic loading conditions and helps in predicting fatigue life, especially in engineering applications where structural integrity is crucial.
Repeated stress: Repeated stress refers to the application of cyclic loads or forces on a material, leading to the potential for fatigue over time. This kind of stress is crucial in understanding how materials behave under conditions where they are subjected to loading and unloading repeatedly, which is common in mechanical systems and components. The impact of repeated stress can lead to microstructural changes in materials, contributing to failure mechanisms such as fatigue wear.
Rotating bending test: The rotating bending test is a method used to evaluate the fatigue properties of materials by subjecting a specimen to bending stresses while it rotates. This test simulates real-world conditions where components experience cyclic loads and helps determine how materials behave under repeated stress, which is crucial for understanding fatigue wear.
S-n curve: The s-n curve, also known as the stress-number curve or Wöhler curve, represents the relationship between the cyclic stress amplitude (s) applied to a material and the number of cycles to failure (n). This graph is essential in understanding fatigue wear, as it illustrates how materials behave under repeated loading conditions and helps predict their lifespan.
Stress Concentration: Stress concentration refers to the localization of stress in a material at points of geometric discontinuity or changes in material properties. This phenomenon can significantly affect the fatigue life of a material, as areas of high stress can lead to the initiation of cracks and subsequent fatigue wear under cyclic loading conditions.
Subsurface Fatigue: Subsurface fatigue refers to the progressive failure that occurs beneath the surface of a material due to cyclic loading or repeated stress. This phenomenon is particularly relevant in engineering, where components experience fluctuating loads during operation, leading to the formation of cracks or defects below the surface that can ultimately result in catastrophic failure. Understanding subsurface fatigue is crucial for predicting material performance and longevity in various applications, especially those subjected to fatigue wear.
Surface Fatigue: Surface fatigue refers to the progressive and localized structural damage that occurs when a material experiences repeated or cyclic loading, leading to the initiation and growth of cracks at or near the surface. This phenomenon is particularly significant in applications involving components like bearings and gears, where constant motion and contact stresses contribute to wear over time.
Surface Hardening: Surface hardening is a heat treatment process used to increase the hardness and wear resistance of the surface of a material, particularly metals, while maintaining a tougher and more ductile interior. This technique is crucial for enhancing the performance of materials in applications where wear and fatigue are significant concerns, allowing them to withstand greater loads and extend their service life.
Tensile Strength: Tensile strength is the maximum amount of tensile (stretching) stress that a material can withstand before breaking. This property is crucial for understanding how materials, particularly in engineering applications, will behave under tension, which is relevant for polymers and composites used in structural applications as well as for analyzing fatigue wear in materials that undergo repeated loading cycles.
Thermal fatigue: Thermal fatigue refers to the progressive and localized structural damage that occurs in materials due to cyclic thermal loading. This phenomenon is particularly relevant when materials experience repeated temperature fluctuations, causing them to expand and contract, which can lead to the formation of cracks and eventual failure. Understanding thermal fatigue is crucial when considering the wear and longevity of materials in environments where temperature changes are frequent.
Yield Strength: Yield strength is the amount of stress a material can withstand before it begins to deform plastically. This means that once the yield strength is exceeded, the material will not return to its original shape when the load is removed. Understanding yield strength is crucial because it relates directly to how materials behave under different loads, impacting processes like friction, deformation, and wear.