Presentation on Design for Fatigue strength.pptx

Fatigue strength is a measure of the maximum stress that a material can withstand under repeated or cyclic loading without failing or breaking. Fatigue strength is typically expressed in units of stress, such as megapascals (MPa).

In mechanics of materials, fatigue strength is an important property that is used to describe the behavior of materials under repeated or cyclic loading and to predict the response of the material to different loads and strains. It is commonly used in engineering design to select materials for different applications and to analyze and design structures and components for strength and performance.

Fatigue strength is related to other material properties, such as the ultimate tensile strength, which is the maximum stress that the material can withstand before breaking under a single application of load, and the fatigue limit, which is the maximum stress that the material can withstand under repeated or cyclic loading without failing. It is also related to the fatigue life of the material, which is the number of cycles of loading that the material can withstand before failing.

In engineering design, it is important to consider the fatigue strength of a material and to select materials that have the desired strength and performance characteristics for a given application. To optimize the strength and behavior of materials, it is often necessary to use advanced modeling techniques that take into account the fatigue strength and other material properties and to properly test and evaluate the material’s performance under different loading conditions.

1. Module 2: Design for Fatigue Strength

2. Introduction In static loading, failure is gradual and has enough time for elongation. Ex: Elastic deformation, General yielding, Fracture In Fatigue, loading is repeated cyclically. Usually failure begins with minor crack more likely due to Discontinuities, Irregularities and Internal defects Since there is no visible deformation in material due to fatigue loading condition, failure would be catastrophic Definition : Damage accumulated through the application of repeated stress cycles Variable amplitude loadings cause different levels of fatigue Fatigue is cumulative through the life of an engineering element Fatigue failure depends on various factors as Number of stress cycles, mean stress, stress amplitude, stress concentration, residual stresses, corrosion and creep.

3. Three factors play an important role in fatigue failure: (i) value of tensile stress (maximum), (ii) magnitude of variation in stress, (iii) number of cycles. Geometrical (specimen geometry) and microstructural aspects also play an important role in determining fatigue life (and failure). Stress concentrators from both these sources have a deleterious effect. Residual stress can also play a role. A c orrosive environment can have a deleterious interplay with fatigue. Factors affecting fatigue failure Factors necessary to cause fatigue failure Large variation/fluctuation in stress Sufficiently high maximum tensile stress Sufficiently large number of stress cycles

4. Typical cyclic loading parameters Stress Cycle: It is smallest portion of stress time plot which is repeated periodically and identically. Maximum stress: Largest algebraic stress in a stress cycle Minimum stress: Smallest algebraic stress in a stress cycle Mean stress: Algebraic mean of the Maximum and Minimum stress values Range of Stress: It is algebraic difference between the maximum and minimum stress values. Stress amplitude or Variable stress: Stress ratio: Ratio of minimum stress to Maximum stress value

5. Types of variable loads

6. RR Moore test: Rotating Bending beam testing

7. Endurance limit Endurance limit: Maximum amplitude of completely reversed stress that the standard specimen can sustain for an unlimited number of cycles without failure Fatigue Life: It is number of stress cycles that the standard test specimen can complete before first crack appears.

8. Low and High cycle fatigue Fatigue failure occurring below 1000 stress cycles is called as Low cycle fatigue failure. Mainly due to High load and plastic deformation Fatigue failure occurring above 1000 stress cycles is called High cycle fatigue Mainly due to low loads and elastic deformation

9. Factors effecting Endurance limit Surface finish; Shape and distribution of inclusions; Grain size and direction; Specimen or component size; Load type; Surface treatments; Temperature; Environment (corrosion).

10. Soderberg Criteria

11. Module 3: Design of Joints and Couplings Presented by : Prof. Manjunath S. B.

12. Couplings Purpose of using Couplings For the connection of shafts of units that are manufactured separately To provide disconnections To compensate the misalignment of shafts To reduce transmission shocks To provide required length of the shaft. Couplings are classified into Rigid coupling 2. Flexible coupling 3. Fluid coupling 4. Magnetic coupling Example for Rigid type coupling: Sleeve or muff coupling, Marine type flange coupling and Rigid type Protected & Unprotected flange coupling

13. Unprotected type Flange coupling

14. Protected type flange coupling

15. Terms for Rigid type flange coupling design d = diameter of shaft D = outside diameter of flange D 2 = Hub diameter l = length of hub or length of key h = thickness of key τ s = allowable shear stress of shaft material τ d2 = allowable shear stress in key material M t = Torque transmitted N = power in kW n = speed in rpm η = keyway factor d 1 = core diameter of the bolt D 1 = Bolt circle diameter t = thickness of flange neat the throat i = number of bolts b = width of the key τ b = allowable shear stress of bolt material

16. Design Procedure Determine torque transmitted by coupling (19.3C) Determine diameter of shaft using torque equation (d) : (19.2) Determine bolt circle diameter (D 1 ) : (19.12b) Design the Hub for suitable dimension (D 2 ) & (l) = (19.13b) & (19.14d) Design of flange: Outer diameter and thickness: (19.14b) Check the dimensions of flange for shear stress induced (19.6) Design the bolts: Number of bolts and Diameter: (19.1b) & (19.4) Check the diameter of bolt for crushing stresses induced Design of Key: Identify suitable size of key (width, thickness and length): Choose suitable thickness and width of the key from 17.4 table Choose the length of the key from table 17.5 Check the design of key for stresses: Width of the key: For possible shearing stresses induced during operation Thickness of the key : For possible Crushing stresses induced during operation

17. Design of Socket and Spigot cotter Joint

18. Socket and Spigot cotter Joint

19. Important Dimensions for design

20. Design terms for Socket and spigot joint F= Axial load d = diameter of rod d 1 = diameter of spigot d 2 = diameter of spigot collar d 3 = Outside diameter of socket d 4 = diameter of socket collar h = thickness of socket at the rod end t = thickness of cotter b = mean width of cotter a = rod end distance from end of slot c = socket end distance from end of slot (thickness of socket collar) e = thickness of spigot collar τ = allowable shear stress σ = permissible normal stress σ c = allowable crushing stress

21. Failure in Socket and spigot cotter joint

22. Design of Spigot : Tensile failure of Spigot

23. Shear failure of Spigot ( Check Shear stress induced)                                                                                            

24. Design of Socket { ‘d1’,’d4’,’c’}

25. Shear failure of Socket ( Check Shear stress induced)

26. Design of Cotter { ‘t’, ‘b’ and ‘l’  of cotter}

27. Design Procedure Design of rod (d) : Evaluate axial stress in rod : (17.62) Design of spigot and cotter (d 1 , b, a) : Evaluate crushing stress in cotter (17.69), Axial stress across slot (17.63) double shear stress at rod end (17.66) Design of spigot collar (d 2 , e): Evaluate crushing failure in collar(d 2 ) (17.68), Shear failure in collar (e) (17.72) Design of socket (d 3 , d 4 , c, h): Socket failure in tension and compression (d 3 ) : (17.64) Crushing of socket collar (d 4 ) : (17.70) Shear failure of socket end (c): (17.67) Shear failure of socket (h): (17.73) Evaluate bending stress in cotter: (17.74)

28. Sleeve and Cotter joint

29. P = Load carried by the rods, d = Diameter of the rods, d1 = Outside diameter of sleeve, d2 = Diameter of the enlarged end of rod, t = Thickness of cotter, l = Length of cotter, b = Width of cotter, a = Distance of the rod end from the beginning to the cotter hole (inside the sleeve end), c = Distance of the rod end from its end to the cotter hole, σt , τ and σc = Permissible tensile, shear and crushing stresses respectively for the material of the rods and cotter. Terms in Sleeve and Cotter Joint Design

30. Knuckle Joint

31. Knuckle Joint

32. Stresses in Knuckle Joint

33. Stresses in Knuckle Joint

34. Shear failure of eye end

35. Threaded Fasteners Screw Threads and their uses To transmit power To hold parts together To control movement as in micrometer To increase the effort as in screw jack Terminology Pitch (p) : It is the distance from a point on one thread to corresponding point on the adjacent thread measured parallel to the axis. Lead (l): It is the distance moved by the nut in the axial direction in one complete revolution. Major diameter (d): Its largest diameter of the screw thread. It is also called as nominal diameter. Pitch diameter(d1): It is the smallest diameter of a screw thread. Slope: Slope of thread is equal to half the lead Its is the top portion of the surface of a thread Helix Angle( β ) : Angle made by the helix of the thread at the pitch diameter with the plane perpendicular to the axis.

36. ISO Metric Thread

37. Stresses in Screw Fastening due to static loading Initial Stresses due to screwing up forces Tensile stress due to stretching of bolt Torsional shear stress Shear stress across threads Crushing stress across threads Bending stresses Stresses due to External Forces Tensile stress Shear Stress Combined stress Stresses due to combination of initial stresses and external forces Resultant axial load