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BK50A2200 Design Methodologies and Applications of Machine Element Design
Lecture 2 Introduction to the textbook: “Norton: Machine Design” D.Sc Harri Eskelinen
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Goals of this lecture Support the contents of the previous lectures dealing with machine design approaches, reliability design and wear phenomena To get familiar with the main designing and dimensioning criteria of the most important machine elements (according to Norton) Main consecutive designing steps and aspects Fundamental dimensioning equations
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Briefly about the book The textbook presents an integrated approach to the machine elements by combining the usual set of machine element topics with a series of case studies that illustrate the relationships between force, stress and failure analysis in real-world design. The book emphasizes the design and synthesis aspects of machine elements but it forms also a good balance between synthesis and analysis.
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The first part of the book presents the fundamentals of design, materials, stress, strain, deflection, failure and fracture theories. The second part treats of the aspects of machine element design, such as designing springs, shafts, gears, bearings etc.
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PART 1. FUNDAMENTALS
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Chapter 1. Introduction to Design
This chapter partially supports the ideas of systematic design approach (see the yellow items below) : according to Norton the design process consists of the following ten stages: 1 Identification of need 2 Background research 3 Goal statement 4 Task specifications 5 Synthesis 6 Analysis 7 Selection 8 Detailed design 9 Prototyping and testing 10 Production
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Chapter 2. Materials and Processes
The contents of this chapter will be discussed in details during the university course “Introduction to Material Technology” Basic definitions of the most common material properties are presented briefly: Modulus of elasticity Yield strength Ultimate tensile strength Modulus of rigidity Fatigue strength Toughness Hardness Most typical hardening and surface coating processes are presented briefly Basic information about some material groups is given: Steels Cast iron Aluminium Titanium Copper Alloys Polymers Ceramics Composites
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Chapter 3. Load Determination
The content of this chapter produce the fundamentals for the further stress, strain and deflection analysis presented in chapter 4. Main topics are: Different loading cases Free-body diagrams Static loading Dynamic loading Vibration loading Impact loading Beam loading
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Classification of loading cases
Constant Loads Time-Varying Loads Stationary elements Class 1 Class 2 Moving elements Class 3 Class 4
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Identification of different loading cases
Identification of different loading cases in necessary to make it possible to use proper material properties as criteria during the material selection process Tension or compression tensile or compressive stress Bending bending stress Shear shear stress Torsion torsion stress (shear strass) Reverced loading endurance limit (for reverced stress) Pulsating loading endurance limit (for pulsating stress) Pulsating loading Reverced loading
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Free-Body Diagrams Case example: Wire connector crimping tool
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Chapter 4. Stress, Strain and Deflection
This chapter includes the basic theories of “strength of materials”, the following topics are discussed (the most important items are high-lighted with yellow): Principal stresses Axial Tension Bending stresses of beams Deflection of beams Torsion Combined stresses Stress concentration Axial compression Stresses in cylinders
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Critical cross-sections due to stress concentrations:
Combined loading: Axial force Radial force Tangential force Torque combined stresses T1 Fa Fr Ft A B C D Critical cross-sections due to stress concentrations: End of the keyseat at cross-section A Cross-sections B, C and D of a smaller diameter
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Chapter 5. Static Failure Theories
Chapter 5 is divided in three main sections: Failure of ductile materials under static loading The main failure mode is permanent yield under static loading yield strength of the material is exceeded Critical material property is yield strength Failure of brittle materials under static loading Instead on yielding brittle materials fracture Fully hardened steels, cast iron, materials in low temperatures can behave like brittle materials Critical material property is toughness at certain temperature Fracture mechanics This theory presumes the presence of a crack, which starts to grow under the specific loading and finally leas to either ductile or brittle failure
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Toughness Temperature Brittle behaviour Ductile Transition zone
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Modes of crack displacement
Loading Modes of crack displacement Mode I = load tends to pull the crack open in tension Mode II = shear crack in-plane Mode III = shear the crack out-of-plane
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Chapter 6. Fatigue Failure Theories
The use of typical Wöhler’s strength-life- diagrams is presented The main principles of the use of Paris-Equation are presented The use of Goodman’s diagram for fatigue life analysis is presented Schematic fatigue-fracture surfaces of a shaft cross-sections are presented to support further failure mode analysis
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Wöhler’s diagram
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Schematic fatigue-fracture surfaces
Rotating bending Low nominal stress Mild stress concentration
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Paris-equation The crack growth “speed” is presented as a function of loading cycles: Where a = crack width N = number of cycles A, n = material coefficients ΔK = stress intensity factor range
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D A M G I N S P E Region I Crack initiation stage Region II Crack propagation Region III Unstable fracture No crack growth Stress intensity
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Chapter 7. Surface Failure
This chapter contains the following topics Mathematical theory of surface contacts Characteristics to describe the value of surface roughness Spherical contact Cylindrical contact Dynamic contact stresses Designing rules to avoid surface failure Wear phenomena (discussed earlier during this course) Abrasive wear Adhesive wear Fatigue wear Tribochemical wear or corrosive wear
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Mathematical definition of Ra:n
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Designing rules to avoid surface failure
1 Remember the rules which were presented during the special lesson dealing with wear phenomena 2 Choose proper materials Hardness Surface roughness Use of coatings 3 Choose proper lubricants Take care of EHD- or HD- lubrication (avoid boundary lubrication) Use EP-lubricants if needed(extreme pressure) 4 Take care of cleanliness Use proper sealing constructions Select proper material pairs (e.g. hardness pairs) 5 Avoid and minimize stress concentrations Select proper stiffness and/or geometry 6 Avoid fretting problems by taking care of possible vibration phenomena (near joints or fits)
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Case example: How to minimize the stress concentrations in a cylindrical roller bearing by using a proper geometry of the roller elements.
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Case example: Fretting wear on a shaft beneath a press-fit hub.
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PART 2. Machine Design
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Chapter 8. Design Case Studies
This brief chapter is written just to form “a bridge” between the theories of material science, strength of materials, failure theories (presented in part 1) and practical dimensioning and analysing instructions of some typical machine elements (to be presented in part 2). The iterative nature of designing process is emphasized.
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Chapter 9. Shafts, Keys and Couplings
Designing of shafts step-by-step (iterative analysis): 1 Determine the affecting loading cases E.g. gear forces, torque, forces due to belt drives etc. 2 Collect contacting dimensions from the construction and select possble shaft materials E.g. shaft-hub joints, diameters of bearing seats, width of gears etc. 3 Produce the free-body diagram and calculate the teaction forces 4 Draw loading (force), shear and moment diagrams 5 Find the critical cross-sections of the shaft E.g. key seats, changes of the diameters, grooves, threads etc. 6 Calculate the affecting stresses and deflections E.g. tensile stress, bending stress, shear stress, 7 Calculate the critical rotating speed due to vibration and resonance 8 Calculate safety factors Constant and time-varying loading
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The dimensioning procedure of shafts is based on ASME-method:
Soderberg’s hypothesis (in Finland several hypothesis are used and usually compared in university text books) Goodman’s line (in Finland the use of Smith’s diagram is more common)
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Estimation of shaft diameter:
Some rules of thumbs Estimation of shaft diameter: d = required shaft diameter Tmax = affecting torque Tsall = allowed shear stress of the material
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Critical angular velocity:
Bending vibration ncr = critical angular velocity δmax = maximum deflection of the shaft
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Critical angular velocity:
Torsinal vibration fcr = critical angular velocity kv = torsional stiffness coefficient J1 = moment of inertia (input) J2 = moment of inertia (output) d = diameter of the shaft G = modulus of rigidity L = length of the shaft m = weight of (each) component r = rotating radius of (each) component
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Loading cases of shaft-hub-joints
Torque Fr Ft Fa Moment Torque
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If the joint is able to withstand also axial loading, its torque transmission capacity can be estimated according to the following equation: Where Ttheor = theoretical maximum allowed torque which joint could transmit without any axial loading T = torque, which can be transmitted even though Fa is affecting simultaneously (usually the value which is calculated) Fatheor = theroretical maximum allowed axial force, which joint could transmit without any torque loading Fa = axial load, which is decreasing the torque transmission capacity (“the disturbing factor”)
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Main designing steps are as follows:
Dimensioning of parallel keys is based on SFS-standards (we skip the presentation presented by Norton): Main designing steps are as follows: Check the maximum surface stress of the hub Check the maximum surface stress of the key Check the maximum shear stress of the key Ensure that the required torque transmission capapacity is achieved
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Chapter 10. Bearings and Lubrication
This chapter includes the following important topics: Lubricants and types of lubrication Briefly about sliding bearings and their material combinations Rolling-element bearings Failure of rolling-element bearings Selection of rolling bearings
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Types of lubrication Hydrodynamic lubrication (HD or HL)
HD refers to the supply of oil to the sliding interface to allow the relative velocity of the mating surfaces to pump oil within the gap and separate the surfaces on the dynamic film of liquid. Elastohydrodynamic lubrication (EHD or EHL) When the contacting surfaces are nonconforming, as with gears or cam mechanisms, it is difficult to form a full film of oil.The affecting load creates a contact area from the elastic deflections of the surfaces. This area can be large and flat enough to provide full hydrodynamic film if the relative sliding velocity is high enough. This is possible, because the high pressure between the surfaces increase the viscosity of the fluid. Boundary Lubrication (BL) Either the insufficient geometry, too high load level, low velocity or insufficient oil quantity may prevent hydrodynamic lubrication and cause metallic contacts between the surfaces (e.g. at the beginning or end of the rolling)
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Selection of rolling bearings
Allowed dynamic load Allowed maximum angular velocity Facilities of the selected bearing type Ability to withstand axial loads Ability to withstand axial bending moments or angular assembly errors Allowed friction Required stiffness and accuracy Allowed static load Required reliability
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Some examples A detailed guide to select an appropriate bearing type will be given out as a hand-out… Spherical roller bearings Especially for cases in which bending moment could cause additional loading on the bearing or where possible assembly errors may cause some misaligning of the shaft Tapered roller bearings Especially for cases in which good axial load standing capacity is required
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Basic equations of bearing design
P = combined dynamic equivalent load of the bearing Fr = applied radial load Fa = applied axial load X = a radial factor Y = an axial factor p = exponent, the value depends on the bearing type Ball bearings p=3 Roller bearings p= 10/3 L10h = Nominal life-time (e.g h) C = Dynamic load rating
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Chapter 11. Spur Gears Spur gears are used to present principles of gear dimensioning in general Specialized terminology is presented in details Gear tooth theory is discussed Equations for dimensioning gears are presented Also gear manufacturing processes are presented briefly Different casting processes Machining Powder metallurgical processes (sintering) Extruding and cold drawing processes Different finishing processes The presentation is based on standards published by the American Gear Manufacturers Association (AGMA)
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At first the applying forces on gear teeth must be established! T1 T2
Fa Fr Ft At first the applying forces on gear teeth must be established!
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Main dimensioning criteria: Main characteristics:
Equations are based on experimental factors, parameters and characteristics describing e.g.: Geometric accuracy of gears Lubrication conditions Material properties of gears Stress concentration phenomena Surface properties of gears Loading conditions of gears Main dimensioning criteria: Bending stresses of the teeth Surface stresses of the teeth Main characteristics: Gear ratio i=Z1/Z2 Module m=d1/Z1 Contact ratio Functions: To transimit Torque Angular velocity
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Basic equations for spur gear design
Power transmission capacity according to allowed bending stresses of the teeth Power transmission capacity according to allowed surface stresses of the teeth
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Chapter 12. Helical,Bevel and Worm Gears
Helical gears Teeth are angled with respect to the axis of rotation Contact surface between teeth is increased Axial load component is caused Bevel gears Shafts are located usually at 90 degrees angle Worm gears Shafts are located at crossing position and high gear ratios are achieved
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The dimensioning of helical gears is based on the equations of spur gears, so-called virtual number of teeth should be established and then the theory of spur gears is applied For bevel gears either the theories of dimensioning of spur or helical gears can be applied: Straight bevel gears spur gears Spiral bevel gears helical gears
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Two main additional aspects of tooth geometry should be considered
Use of single- or double-enveloping tooth forms Number of teeth in contact with worm and worm wheel Worm gears are discussed very briefly, however the main dimensioning aspects consist of four main steps: Durability against pitting (surface fatigue) Durability against wear (abrasive wear due to different material properties of the worm and the worm wheel) Durability against overheat Allowable bending deflection of the worm (shaft)
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Example of dimensioning equations of worm gear design
Safety factor SW against wear Wlim = kulumislujuus WP = kulumisparikerroin (mm. kovuus) WR = pinnankarheuskerroin Wv = liukunopeuskerroin ZE = materiaalikerroin (E1 ja E2) Z = kosketuskerroin (kierremuoto) Materials wear strength Coefficient depending on materials hardness Coefficient depending on surface roughnesses Coefficient depending on the sliding velocity Coefficient depending on modulus of elasticity Coefficient depending on the tooth geometry
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Chapter 13. Spring Design Main contents of this chapter:
Definition of the spring rate is presented Various spring configurations and materials are presented briefly Dimensioning and designing criteria is presented for the following spring configurations: Helical compression springs Helical extension springs Helical torsion springs Belleville spring washers
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Example: Designing steps of helical compression springs
1 Decide spring configuration 1.1 Length 1.2 End details and number of active coils 1.3 Tentative material selection 2 Establish functional properties 2.1 Sprind index C = D/d (coil diameter/wire diameter) 2.2 Spring deflection y 2.3 Spring rate k = F/y 3 Loading cases and stress analysis 3.1 Shear stress 3.2 Torsional shear stress 3.3 Stress concentrations 3.4 Residual stresses due to manufacturing stages (e.g coiling into the form of helix causes tensile stress) 3.5 Buckling 3.6 Vibration and resonance phenomena 3.7 Fatigue analysis 3.8 Final material selection
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Chapter 14. Screws and Fasteners
This chapter deals with the following topics: Standardized thread dimensions Power screws Screw fasteners Stresses in threads Tensile, torsion and shear Joint stiffness Preloaded fasteners
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A bolted assembly
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A bolted assembly The clamped construction may include two or more pieces and they may be of different material. Also a long bolt usually has threads over only a portion of its length having at least two different cross-sectional areas. These different stiffness-sections act as springs in series and their function can be described according to the following equation: When we know the dimensions and geometry of the bolt and pieces to be joined it is possible to calculate the partial spring rates and combine them according to this simple equation. Analogical with spring analysis we can now write the relationship between the total spring rate, deflection and applying force.
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Other dimensioning aspects of bolted joints
1 Washers Decrease the surface stresses at the joint Ensure the tightness of the joint Prevents the possible bending moment of the bolt due to slant surface 2 Bolt’s straight length without threads The stress concentration at the end of the straight length before the first thread could be critical The straight length is planed to function “as a spring” 3 Parts to be clamped together In many cases the friction coefficient between the parts to be clamped together is in key-role There should be enough distance between the mounting holes of the screws and edges of the parts to be clamped to avoid fractures of the base material
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Possible failure modes of bolted joints
1 The bolt breaks under the static tensile loading Tensile stress exceeds the ultimate tensile strength of the bolt The first thread of the bolt is cut off The first thread of the nut is cut off 2 The fatigue strength of the bolt is exceeded Typically the fatigue limit is only 10% of screw material’s yield strength 3 The failures of the parts to be clamped The shear stress is too large near the edges
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Means to improve the fatigue strength of the bolted joint:
Select a taller nut (to increase the number of load standing threads) Select more suitable material pair for the nut and the bolt combination (lower coefficient of elasticity for the nut compared to that of the screw’s e.g. aluminium or cast iron for nuts with and steel for bolts) Use sufficient pre-loading of the bolts (equalize the stresses applying at each thread of the bolt and nut) Improve the surface quality of the bolt, Select the bolt (and thread) geometry with the smallest stress concentration coefficient Select the advantageous manufacturing technology of the bolts (usually cold forming is recommended)
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Chapter 15. Clutches and Brakes
This chapter forms only a brief overall picture of various types of clutches and brakes to give the reader a sight of possible constructions. Classification according to the actuation (impulse to start the function) Electrical (press the button) Mechanical (push the bedal) Pneumatic or hydraulic Automatic Classification according to the function (what phenomenon the contact is based on) Friction between (two) surfaces Locked geometry (e.g. toothed components) Magnetic Fluid coupling
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SUMMARY : STRESS AND DEFLECTION ANALYSIS
Failure theories • Static failure theories - ductile materials - brittle materials • Fracture mechanics theory • Fatigue failure theories - Wöhler - Paris –Eguation - Soderberg - Goodman • Surface failure theories - wear - surface contact theories Load determination and different load cases • utilization of free-body diagrams • static or dynamic loading • vibration loading - bending vibration - torsional vibration • impact loading • tension, compression, bending shear or torsion • reversed or pulsating loading Pulsating loading Reverced loading Stress, strain and deflection • allowed stress and deflection • due to affecting load cased • combined stresses • stress concentrations Material properties • metallic materials - steels - aluminium - cast iron • polymers • ceramics • composites • nanomaterials
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Exercise 2 Exercise 2A Exercise 2B
Present typical applications of power transmission or guiding shafts under different loading cases. Explain the reasons for the affecting combined loading. Use illustrative figures. Present at least the following loading cases: Tension or compression + bending Tension or compression + bending + torsion Bending + torsion Shear + any other loading case Reversed loading Pulsating loading Exercise 2B Compare different fatigue failure theories and approaches by presenting typical applications of different types of mechanical components or constructions. Compare at least the following approaches: Wöhler’s strength-life-theory Goodman’s theory Paris-equation Utilization of schematic fatigue-fracture surfaces Fracture mechanics
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