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8/25/2013 System Dynamics 4.01 Spring & DamperElementsinMechanicalSystemsSpringandDamperElementsinMechanicalSystems HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.03 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §1.Spring Elements 2.Tensile test of a rod System Dynamics 4.02 Spring & DamperElementsinMechanicalSystems HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.04 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §1.Spring Elements 3.Analytical Determination of the Spring Constant - Example 4.1.1 Rod with Axial Loading Derive the spring constant expression for a cylindrical rod subjected to an axial force 𝑓 Solution The force deflection relation of the rod 𝐿 4𝐿 𝑥= 𝑓= 𝑓 𝐸𝐴 𝜋𝐸𝐷 𝑥: axial deformation, 𝑚 𝐿: length of the rod, 𝑚 𝑓: applied axial force, 𝑁 𝐸: modulus of elasticity, 𝑃𝑎 𝐴: cross-sectional area, 𝑚2 𝐷: rod diameter, 𝑚 The spring constant 𝑘 𝑓 𝐸𝐴 𝜋𝐸𝐷 𝑘≡ = = , 𝑁/𝑚 𝑥 𝐿 4𝐿 HCM City Univ of Technology, Mechanical Engineering Department §1.Spring Elements - Example 4.1.2 System Dynamics §1.Spring Elements 1.Force-Deflection Relations Linear force deflection model 𝑓 = 𝑘𝑥 𝑓: the restoring force, 𝑁 𝑥: the compression or extension distance, 𝑚 𝑘: the spring constant, or stiffness, 𝑁/𝑚 For the helical coil spring 𝐺𝑑 𝑘= 64𝑛𝑅 𝑑: the wire diameter, 𝑚 𝑅: the radius of the coil, 𝑚 𝑛: the number of coils 𝐺: the shear modulus of elasticity, 𝑃𝑎 4.05 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystemsSpring Constant of a Fixed-End Beam Derive the spring constant expression of a fixed-end beam HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.06 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §1.Spring Elements - Spring constants of common elements Solution The force-deflection relation of a fixed-end beam 𝐿3 𝐿3 𝑥= 𝑓= 𝑓 192𝐸𝐼𝐴 16𝐸𝑤ℎ3 𝑥: deflection, 𝑚 𝐿: length of the beam, 𝑚 𝑓: applied force, 𝑁 𝐸: modulus of elasticity, 𝑃𝑎 𝐼𝐴 : area moment of inertia, 𝐼𝐴 = 𝑤ℎ3 /12, 𝑚2 The spring constant 𝑘 𝑓 16𝐸𝑤ℎ3 𝑘≡ = , 𝑁/𝑚 𝑥 𝐿3 HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 8/25/2013 System Dynamics 4.07 Spring & DamperElementsinMechanicalSystems §1.Spring Elements - Spring constants of common elements HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.09 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §1.Spring Elements 4.Series and parallel springelements - Series springelements = 𝑘𝑒 𝑛 𝑖=1 𝑘𝑖 𝑘𝑖 4.11 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §1.Spring Elements - Example 4.1.4 Spring Constant of a Lever System Consider a horizontal force 𝑓 acting on a lever that is attached to two springs Assume that the resulting motion is small Determine the expression for the equivalent spring constant that relates the applied force 𝑓 to the resulting displacement 𝑥 Solution For small angles 𝜃, the upper spring deflection is 𝑥 and the deflection of the lower spring is 𝑥/2 For static equilibrium 𝑥𝐿 𝑥 𝑓𝐿 = 𝑘𝑥𝐿 − 𝑘 =0⟹𝑓=𝑘 𝑥+ = 𝑘𝑥 22 4 The equivalent spring constant 𝑘𝑒 = 5𝑘/4 HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.10 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems The equivalent spring constant 1 𝐺𝜋𝐷𝑖4 = + , 𝑘 𝑇𝑖 = , 𝑖 = 1,2 𝑘 𝑇𝑒 𝑘 𝑇1 𝑘 𝑇2 32𝐿𝑖 𝑘 𝑇1 𝑘 𝑇2 ⟹ 𝑘 𝑇𝑒 = 𝑘 𝑇1 + 𝑘 𝑇2 𝑖=1 System Dynamics Spring & DamperElementsinMechanicalSystems Solution Torque applied to the shaft 𝑇 = 𝑘 𝑇1 𝜃1 = 𝑘 𝑇2 𝜃2 𝑛 HCM City Univ of Technology, Mechanical Engineering Department 4.08 §1.Spring Elements - Example 4.1.3 Spring Constant of a Stepped Shaft Determine the expression for the equivalent torsional spring constant for the stepped shaft - Parallel springelements 𝑘𝑒 = System Dynamics §1.Spring Elements - Torsional spring constants of common elements Nguyen Tan Tien HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.12 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §1.Spring Elements 5.Nonlinear springelements - In some case, the use of a nonlinear model is unavoidable This is the case when a system is designed to utilize two or more springelements to achieve a spring constant that varies with the applied load Even if each spring element is linear, the combined system will be nonlinear - Example 4.1.5 Deflection of a Nonlinear System Obtain the deflection of the system model shown in figure as a function of the weight 𝑊 Assume that each spring exerts a force that is proportional to its compression HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 8/25/2013 System Dynamics 4.13 Spring & DamperElementsinMechanicalSystems §1.Spring Elements Solution System Dynamics 4.14 Spring & DamperElementsinMechanicalSystems §1.Spring Elements - Most springelements display nonlinear behavior if the deflection is large enough - Force-deflection relations for three types of springelements • A hardening spring element • A softening spring element • The linear spring element: straight line At equilibrium points: the weight force must balance the spring forces 𝑊 𝑥= 𝑥 𝑥 = 0.1557 > 0.1 ⟹ 𝑥𝑚𝑎𝑥 = 0.1557, 𝐹𝑚𝑎𝑥 = 𝑘1 𝑥𝑚𝑎𝑥 + 2𝑘2(𝑥𝑚𝑎𝑥 − 0.1) = 3240𝑁 HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 8/25/2013 System Dynamics 4.31 Spring & DamperElementsinMechanicalSystems System Dynamics 4.32 Spring & DamperElementsinMechanicalSystems §3.Energy Methods 1.Obtaining Motion Equation - In mass-spring systems with negligible friction and damping, we can often use the principle of conservation of energy to obtain the equation of motion and, for simple harmonic motion, to determine the frequency of vibration without obtaining the equation of motion - Example 4.3.2 Equation of Motion of a Mass-Spring System Use the energy method to derive the equation of motion of the mass 𝑚 attached to a springand moving in the vertical direction §3.Energy Methods Solution Take the reference at 𝑥 = , the total potential energy of the system (𝑘𝛿𝑠𝑡 = 𝑚𝑔) 𝑉 = 𝑉𝑠 + 𝑉𝑔 = 𝑘(𝑥 + 𝛿𝑠𝑡 )2 −𝑚𝑔𝑥 1 1 = 𝑘𝑥 + 𝑘𝛿𝑠𝑡 𝑥 + 𝑘𝛿𝑠𝑡 − 𝑚𝑔𝑥 = 𝑘𝑥 + 𝑘𝛿𝑠𝑡 2 2 The total energy of the system 1 𝑇 + 𝑉 = 𝑚𝑥 + 𝑘𝑥 + 𝑘𝛿𝑠𝑡 = 𝑐𝑜𝑛𝑠𝑡𝑎𝑛𝑡 2 𝑑 𝑇+𝑉 ⟹ = ⟹ 𝑚𝑥𝑥 + 𝑘𝑥𝑥 = 𝑑𝑡 The equation of motion: 𝑚𝑥 + 𝑘𝑥 = HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.33 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §3.Energy Methods 2.Reileigh’s Method - Based on the principle of conservation of energy - In simple harmonic motion • at the equilibrium position 𝑥 = 𝑇 = 𝑇𝑚𝑎𝑥 𝑉 = 𝑉𝑚𝑖𝑛 • when 𝑥 = 𝑥𝑚𝑎𝑥 𝑉 = 𝑉𝑚𝑎𝑥 𝑇 = 𝑇𝑚𝑖𝑛 = - From conservation of energy 𝑇𝑚𝑎𝑥 + 𝑉𝑚𝑖𝑛 = 𝑇𝑚𝑖𝑛 + 𝑉𝑚𝑎𝑥 = + 𝑉𝑚𝑎𝑥 ⟹ 𝑇𝑚𝑎𝑥 = 𝑉𝑚𝑎𝑥 − 𝑉𝑚𝑖𝑛 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.35 4.34 Spring & DamperElementsinMechanicalSystems §3.Energy Methods - Example for a mass-spring system 𝑇 = 𝑚𝑥 /2 𝑉 = 𝑘 𝑥 + 𝛿𝑠𝑡 /2 − 𝑚𝑔𝑥 From conservation of energy 𝑇𝑚𝑎𝑥 = 𝑉𝑚𝑎𝑥 − 𝑉𝑚𝑖𝑛 1 2 ⟹ 𝑚𝑥𝑚𝑎𝑥 = 𝑘(𝑥𝑚𝑎𝑥 + 𝛿𝑠𝑡 )2 −𝑚𝑔𝑥𝑚𝑎𝑥 − 𝑘𝛿𝑠𝑡 2 with 𝑘𝛿𝑠𝑡 = 𝑚𝑔 1 2 ⟹ 𝑚𝑥𝑚𝑎𝑥 = 𝑘𝑥𝑚𝑎𝑥 2 In simple harmonic motion |𝑥𝑚𝑎𝑥 | = 𝜔𝑛 |𝑥𝑚𝑎𝑥 | 1 ⟹ 𝑚(𝜔𝑛 |𝑥𝑚𝑎𝑥 |)2 = 𝑘𝑥𝑚𝑎𝑥 2 ⟹ 𝜔𝑛 = 𝑘/𝑚 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §3.Energy Methods - Example 4.3.3 Natural Frequency of a Suspension System Consider the suspension of one front wheel of a car: 𝐿1 = 0.4𝑚, 𝐿2 = 0.6𝑚, spring constant 𝑘 = 3.6 × 104 𝑁/𝑚, and the car weight associated with that wheel is 3500𝑁 Determine the suspension’s natural frequency for vertical motion Solution Frame moving: 𝐴𝑓 = 𝐶𝐶′ Spring deflection: 𝐴𝑠 = 𝐷𝐸 − 𝐷 ′𝐸′ ≈ 𝐸𝐸′ From ∆𝐹𝐶𝐶′, approximately: 𝐿2 − 𝐿1 𝐴𝑠 ≈ 𝐴𝑓 = 𝐴𝑓 𝐿2 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics Nguyen Tan Tien Nguyen Tan Tien HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.36 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §3.Energy Methods The change in potential energy (𝑘𝛿𝑠𝑡 = 𝑚𝑔) 𝑉𝑚𝑎𝑥 − 𝑉𝑚𝑖𝑛 = 𝑘 𝐴𝑠 + 𝛿𝑠𝑡 2 1 2 = 𝑘𝐴2𝑠 = 𝑘 − 𝑚𝑔𝐴𝑠 − 𝑘𝛿𝑠𝑡 𝐴𝑓 The amplitude of the velocity of the mass in simple harmonic motion is 𝜔𝑛 𝐴𝑓 , and thus the maximum kinetic energy 𝑇𝑚𝑎𝑥 = 𝑚(𝜔𝑛 𝐴𝑓 )2 From Rayleigh’s method, 𝑇𝑚𝑎𝑥 = 𝑉𝑚𝑎𝑥 − 𝑉𝑚𝑖𝑛 , we obtain 1 𝑚(𝜔𝑛 𝐴𝑓 )2 = 𝑘 ⟹ 𝜔𝑛 = 𝐴𝑓 𝑘 3.6 × 104 = = 3.345𝑟𝑎𝑑/𝑠 3500 𝑚 9.8 HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 8/25/2013 System Dynamics 4.37 Spring & DamperElementsinMechanicalSystems System Dynamics 4.38 Spring & DamperElementsinMechanicalSystems §3.Energy Methods 3.Equivalent Mass of Elastic Elements - In an elastic element is represented as in the figure, we assume the mass of the element • is negligible compared to the rest of the system’s mass, or • has been included in the mass attached to the element - In the second case, this included mass is called the equivalent mass of the element and to be computed by using kinetic energy equivalence - Example 4.3.4 Equivalent Mass of a Rod The rod shown in the figure acts like a spring when an axially applied force stretches or compresses the rod Determine the equivalent mass of the rod §3.Energy Methods Solution Mass of an infinitesimal element 𝑑𝑚𝑟 = 𝜌𝑑𝑦 Kinetic energy of the element 𝑑𝐾𝐸 = 𝑑𝑚𝑟 𝑦 /2 Kinetic energy of the entire rod 𝐿 𝐿 𝐾𝐸 = 𝑦 𝑑𝑚𝑟 = 𝑦 𝜌𝑑𝑦 2 HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.39 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems Assume that the velocity 𝑦 of the element is linearly proportional to its distance from the support, then 𝑦 = 𝑥𝑦/𝐿 𝐾𝐸 = 𝐿 𝑥 𝑦 𝐿 𝜌𝑑𝑦 = 𝜌𝑥 2 𝐿2 𝐿 𝑦 𝑑𝑦 = 𝜌𝑥 𝑦 𝐿2 𝜌𝑥 𝐿3 𝜌𝐿 𝑚𝑟 𝑚𝑟 ⟹ 𝐾𝐸 = = 𝑥 = 𝑥 ⟹ 𝑚𝑒 = 𝐿2 3 3 Then 𝑚 = 𝑚𝑐 + 𝑚𝑒 = 𝑚𝑐 + 𝑚𝑟 /3 System Dynamics 4.40 𝐿 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §3.Energy Methods Equivalent masses of common elements – translational systems §3.Energy Methods Equivalent masses of common elements – translational systems HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.41 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems System Dynamics 4.42 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §3.Energy Methods Equivalent inertias of common elements – rotational systems §3.Energy Methods Equivalent inertias of common elements – rotational systems HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien Nguyen Tan Tien 8/25/2013 System Dynamics 4.43 Spring & DamperElementsinMechanicalSystems §3.Energy Methods - Example 4.3.5 Equivalent Mass of a Fixed-End Beam A motor mounted on a beam with two fixed-end supports An imbalance in the motor’s rotating mass will produce a vertical force 𝑓 that oscillates at the same frequency as the motor’s rotational speed The resulting beam motion can be excessive if the frequency is near the natural frequency of the beam, and excessive beam motion can eventually cause beam failure Determine the natural frequency of the beam-motor system System Dynamics 4.44 The system model Treating this system as if it were a single mass located at the middle of the beam results in the equivalent system, where 𝑥 is the displacement of the motor from its equilibrium position Equivalent mass of the system 𝑚𝑒 = 𝑚𝑐 + 0.38𝑚𝑑 Equivalent spring constant of the beam 4𝐸𝑤ℎ3 𝑘= 𝐿3 𝑚𝑒 𝑥 + 𝑘𝑥 = 𝑓 The natural frequency HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.45 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §3.Energy Methods - Example 4.3.6 Torsional Vibration with Fixed Ends An inertia 𝐼1 rigidly connected to two shafts, each with inertia 𝐼2 The other ends of the shafts are rigidly attached to the supports The applied torque is 𝑇1 a Derive the equation of motion b The cylinder 𝐼1 is a cylinder 𝜙100𝑚𝑚 × 75𝑚𝑚; the shafts 𝐼2 are cylinders 𝜙50𝑚𝑚 × 150𝑚𝑚 The three cylinders are made of steel with a shear modulus 𝐺 = 75𝐺𝑃𝑎 and a density 𝜌 = 7850𝑘𝑔/𝑚3 Calculate the system’s natural frequency HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.47 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §3.Energy Methods b System’s natural frequency The value of 𝑘 𝐺𝜋𝐷 75 × 103 × 𝜋 × 504 𝑘= = 32𝐿 32 × 150 = 3.078 × 105 𝑁𝑚𝑚/𝑟𝑎𝑑 The moment of inertia of a cylinder of 𝐷 2 𝐼= 𝑚 𝐼1 = 𝜋 7.85 × 10−6 75 50 𝐼2 = 𝜋 7.85 × 10−6 150 25 ⟹ 𝐼𝑒 = 5.78 × 10 +2 𝐷 2 𝜔𝑛 = 𝑘 𝑚𝑒 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.46 = 16𝐸𝑤ℎ3 /𝐿3 𝑚𝑐 +0.38𝑚𝑑 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §3.Energy Methods Solution a Equation of motion The equivalent inertia 𝐼𝑒 = 𝐼1 + 𝐼2 The spring constant 𝐺𝜋𝐷 𝑘= 32𝐿 Equation of motion is derived from the free body diagram 𝐼𝑒 𝜃 = 𝑇1 − 𝑘𝜃 − 𝑘𝜃 = 𝑇1 − 2𝑘𝜃 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.48 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §4.Damping Elements - A spring element exerts a reaction force in response to a displacement, either compression or extension, of the element - A damping element is an element that resists relative velocity across it - A common example of a damping element, or damper, is a cylinder containing a fluid and a piston with one or more holes = 5.78 × 10−3 𝑘𝑔𝑚2 −3 = 𝜋𝜌𝐿 Spring & DamperElementsinMechanicalSystems Đ3.Energy Methods Solution = 0.73 ì 103 0.73 × 10−3 = 6.67 × 10−3 𝑘𝑔𝑚2 System’s natural frequency: 𝜔𝑛 = HCM City Univ of Technology, Mechanical Engineering Department 𝑘/𝐼𝑒 = 6793𝑟𝑎𝑑/𝑠 Nguyen Tan Tien HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 8/25/2013 System Dynamics 4.49 Spring & DamperElementsinMechanicalSystems System Dynamics 4.50 Spring & DamperElementsinMechanicalSystems §4.Damping Elements 1.A Door Closer An example from everyday life of a device that contains a damping element as well as a spring element is the door closer §4.Damping Elements 2.Shock Absorbers - A typical shock absorber is very complex but the basic principle of its operation is the damper concept - The damping resistance can be designed to be dependent on the sign of the relative velocity - If the two spring constants are different or if the two valves have different shapes, then the flow resistance will be dependent on the direction of motion HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department Oleo strut: an aircraft shock absorber System Dynamics 4.51 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems System Dynamics 4.52 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §4.Damping Elements 3.Ideal Dampers - Real damping elements have mass, such as the masses of the piston and the cylinder in a shock absorber - If the system consists of an object attached to a damper, a simplifying assumption is to neglect the damper mass relative to the mass of the object and take the mass center of the system to be located at the mass center of the object - If the piston mass and cylinder mass are substantial, the damper must be modeled as two masses, one for the piston and one for the cylinder - An ideal damping element is one that is massless §4.Damping Elements 4.Damper Presentations - The linear model for the damping force 𝑓 = 𝑐𝑣 𝑐: the damping coefficient, 𝑁𝑠/𝑚 𝑣: relative velocity, 𝑚/𝑠 - The damping coefficient of a piston-type damper with a single hole HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.53 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §4.Damping Elements 4.Damper Presentations - Symbols for translational and torsional damperelements - The linear model of a torsional damper 𝑇 = 𝑐𝑇 𝜔 𝑐𝑇 : the torsional damping coefficient, 𝑁𝑚𝑠/𝑟𝑎𝑑 𝜔: the angular velocity, 𝑟𝑎𝑑/𝑠 𝑇: the torque, 𝑁𝑚 HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 𝐷 −1 𝑑 𝜇: the viscosity of the fluid, 𝑁𝑠/𝑚2 𝐿: the length of the hole through the piston, 𝑚 𝑑: the diameter of the hole, 𝑚 𝐷: the diameter of the piston, 𝑚 For two holes, multiply the result by 𝑐 = 8𝜋𝜇𝐿 System Dynamics 4.54 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §4.Damping Elements 5.Modeling Mass-Damper Systems - Example 4.5.1 Damped Motion on an Inclined Surface Derive and solve the equation of motion of the block sliding on an inclined, lubricated surface Assume that the damping force is linear For this application the damping coefficient 𝑐 depends on the contact area of the block, the viscosity of the lubricating fluid, and the thickness of the fluid layer Solution The equation of motion 𝑚𝑣 = 𝑚𝑔𝑠𝑖𝑛𝜃 − 𝑐𝑣 𝑚𝑔𝑠𝑖𝑛𝜃 −𝑐 𝑡 𝑚𝑔𝑠𝑖𝑛𝜃 ⟹𝑣 𝑡 = 𝑣 − 𝑒 𝑚+ 𝑐 𝑐 HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 8/25/2013 System Dynamics 4.55 Spring & DamperElementsinMechanicalSystems System Dynamics 4.56 Spring & DamperElementsinMechanicalSystems §4.Damping Elements - Example 4.5.2 A Wheel-Axle System with Bearing Damping A wheel-axle system in which the axle is supported by two sets of bearings that produce damping Each bearing set has a torsional damping coefficient 𝑐𝑇 The torque 𝑇 is supplied by a motor The force 𝐹 is the friction force due to the road surface Derive the equation of motion Solution The damping torque from each bearing 𝑐𝑇 𝜔 Inertia of the wheel and shafts 𝐼 = 𝐼𝑤 + 2𝐼𝑠 The equation of motion 𝐼𝜔 = 𝑇 − 𝑅𝐹 − 2𝑐𝑇 𝜔 §4.Damping Elements - In a journal bearing, the axle passes through an opening in a support A commonly used formula for the damping coefficient of such a bearing is Petrov’s law 𝜋𝐷 𝐿𝜇 𝑐𝑇 = 4𝜖 𝐿: the length of the opening 𝐷: the axle diameter 𝜖: the thickness of the lubricating layer (the radial clearance between the axle and the support) HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.57 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §4.Damping Elements - Example 4.4.3 A Generic Mass-Spring-Damper System The figure represents a generic mass-springdamper system with an external force 𝑓 Derive its equation of motion and determine its characteristic equation Solution The equation of motion 𝑚𝑥 = −𝑐 𝑥 − 𝑘 𝑥 + 𝛿𝑠𝑡 + 𝑚𝑔 + 𝑓 with 𝑘𝛿𝑠𝑡 = 𝑚𝑔 𝑚𝑥 = −𝑐 𝑥 − 𝑘𝑥 + 𝑓 ⟹ 𝑚𝑥 + 𝑐 𝑥 + 𝑘𝑥 = 𝑓 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.59 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §4.Damping Elements The solution 𝑐 = 0: 𝑥 𝑡 = 𝑐𝑜𝑠4𝑡 𝑐 = 4: 𝑐 = 8: 3 𝑐 = 10: 𝑥 𝑡 = 𝑒 −2𝑡 − 𝑒 −8𝑡 HCM City Univ of Technology, Mechanical Engineering Department 4.58 Spring & DamperElementsinMechanicalSystems §4.Damping Elements - Example 4.4.4 Effects of Damping For the system shown in the figure, the mass is 𝑚 = and the spring constant is 𝑘 = 16 Investigate the free response as we increase the damping for the four cases: 𝑐 = 0,4,8,10 Use the initial conditions 𝑥(0) = and 𝑥(0) = Solution The characteristic equation 𝑚𝑥 + 𝑐 𝑥 + 𝑘𝑥 = 𝑓 ⟹ 𝑠 + 𝑐𝑠 + 16 = The roots −𝑐 ± 𝑐 − 64 𝑠= HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.60 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §4.Damping Elements - Example 4.4.5 A Two-Mass System Derive the equations of motion of the two-mass system shown in the figure Solution For the mass 𝑚1 𝑚1 𝑥1 + 𝑐1 𝑥1 + 𝑐2 𝑥1 − 𝑥2 + 𝑘1 𝑥1 +𝑘2 𝑥1 − 𝑥2 = For the mass 𝑚2 𝑚2 𝑥2 + 𝑐2 𝑥2 − 𝑥1 + 𝑘2 𝑥2 − 𝑥1 = 𝑓 or 𝑚1 𝑥1 + (𝑐1 +𝑐2 )𝑥1 − 𝑐2 𝑥2 + 𝑘1 + 𝑘2 𝑥1 − 𝑘2 𝑥2 = 𝑚2 𝑥2 + 𝑐2 𝑥2 − 𝑐2 𝑥1 + 𝑘2 𝑥2 − 𝑘2 𝑥1 = 𝑓 𝑥 𝑡 = 1.155𝑒 −2𝑡 sin( 12𝑡 + 1.047) 𝑥 𝑡 = (1 + 4𝑡)𝑒 −4𝑡 System Dynamics Nguyen Tan Tien Nguyen Tan Tien HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 10 8/25/2013 System Dynamics 4.61 Spring & DamperElementsinMechanicalSystems §4.Damping Elements 6.Motion Inputs with Damping Elements Equation of motion 𝑚𝑥 + 𝑐 𝑥 − 𝑦 + 𝑘𝑥 = or 𝑚𝑥 + 𝑐 𝑥 + 𝑘𝑥 = 𝑐 𝑦 Note that 𝑦 is given input to the system HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.63 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems 4.65 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples - Example 4.5.4 A Two-Mass System with Displacement Input The figure shows a two-mass system where the displacement 𝑦(𝑡) of the right-hand end of the spring is a given function The masses slide on a frictionless surface When 𝑥1 = 𝑥2 = 𝑦 = 0, the springs are at their free lengths Derive the equations of motion HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.64 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples - Example 4.5.3 Displacement Input and Negligible System Mass Obtain the equation of motion of point 𝐴 for the system shown in the figure The displacement 𝑦(𝑡) is given and the spring is at its free length when 𝑥 = 𝑦 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.66 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples - Example 4.5.5 ATwo-Inertia SystemwithAngular Displacement Input The figure shows a system with two inertia elementsand two torsional dampers The left-hand end of the shaft is twisted by the angular displacement 𝜙 The shaft has a torsional spring constant 𝑘 𝑇 and negligible inertia The equilibrium position corresponds to 𝜙 = 𝜃1 = 𝜃2 = Derive the equations of motion Solution Equation of motion 𝐼1 𝜃1 + 𝑐𝑇1 𝜃1 − 𝜃2 + 𝑘 𝑇 𝜃1 = 𝑘 𝑇 𝜙 Solution The equation of motion 𝑚1 𝑥1 + 𝑘1 (𝑥1 − 𝑥2 ) = 𝑚2 𝑥2 + 𝑘1 𝑥2 − 𝑥1 + 𝑘2 𝑥2 = 𝑘2 𝑦 HCM City Univ of Technology, Mechanical Engineering Department Spring & DamperElementsinMechanicalSystems Solution Place a fictitious mass 𝑚𝐴 at point 𝐴 and write the equation of motion 𝑚𝐴 𝑥 + 𝑐 𝑥 + 𝑘(𝑥 − 𝑦) = Let 𝑚𝐴 = to obtain the answer 𝑐𝑥 + 𝑘𝑥 = 𝑘𝑦 Solution Equation of motion 𝐼 𝜃 + 𝑐𝑇 𝜃 + 𝑘 𝑇 (𝜃 − 𝜙) = or 𝐼 𝜃 + 𝑐𝑇 𝜃 + 𝑘 𝑇 𝜃 = 𝑘 𝑇 𝜙 System Dynamics 4.62 Solution Equation of motion 𝑚𝑥 + 𝑐 𝑥 + 𝑘(𝑥 − 𝑦) = or 𝑚𝑥 + 𝑐 𝑥 + 𝑘𝑥 = 𝑘𝑦 §5.Additional Modeling Examples - Example 4.5.2 A Rotational System with Displacement Input Derive the equation of motion for the system shown in the figure The input is the angular displacement 𝜙 of the left-end of the rod, which is modeled as a torsional spring The output is the angular displacement 𝜃 of the inertia 𝐼 There is no torque in the rod when 𝜙 = 𝜃 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics §5.Additional Modeling Examples - Example 4.5.1 A Translational System with Displacement Input Derive the equation of motion for the system shown in the figure The input is the displacement 𝑦 of the right-end of the spring The output is the displacement 𝑥 of the mass The spring is at its free length when 𝑥 = 𝑦 or Nguyen Tan Tien 𝐼2 𝜃2 + 𝑐𝑇1 𝜃2 − 𝜃1 + 𝑐𝑇2 𝜃2 = HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 11 8/25/2013 System Dynamics 4.67 Spring & DamperElementsinMechanicalSystems System Dynamics 4.68 Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples - Example 4.5.6 A Single-Inertia Fluid-Clutch Model The figure shows a driving disk rotating at a specified speed 𝜔𝑑 There is a viscous fluid layer between this disk and the driven disk whose inertia plus that of the shaft is 𝐼1 Through the action of the viscous damping, the rotation of the driving disk causes the driven disk to rotate, and this rotation is opposed by the torque 𝑇1, which is due to whatever load is being driven This model represents the situation in a fluid clutch, which avoids the wear and shock that occurs in friction clutches a Derive a model for the speed 𝜔1 b Find the speed 𝜔1 𝑡 for the case where the load torque 𝑇1 = and the speed 𝜔𝑑 is a step function of magnitude Ω𝑑 §5.Additional Modeling Examples Solution HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.69 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples b Find the speed 𝜔1 𝑡 If 𝜔𝑑 is a step function of magnitude Ω𝑑 , and if 𝑇1 = 𝐼1 𝜔1 + 𝑐𝑇 𝜔1 = 𝑇1 + 𝑐𝑇 𝜔𝑑 ⟹ 𝐼1 𝜔1 + 𝑐𝑇 𝜔1 = 𝑐𝑇 Ω𝑑 𝑐𝑇 𝑐𝑇 ⟹ 𝜔1 + 𝜔1 = Ω𝑑 𝐼1 𝐼1 the solution for 𝜔(𝑡) can be found 𝜔1 𝑡 = Ω𝑑 − 𝜔1 − Ω𝑑 𝑒 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.71 𝑐 − 𝑇𝑡 𝐼1 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples Solution a Derive the equations of motion for the speeds 𝜔𝑑 and 𝜔1 Model this system with two inertias, the equation of motion 𝐼𝑑 𝜔𝑑 + 𝑐𝑇 (𝜔𝑑 − 𝜔1 ) = 𝑇𝑑 𝐼1 𝜔1 + 𝑐𝑇 𝜔1 − 𝜔𝑑 = −𝑇1 HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien a Derive a model for the speed 𝜔1 Lacking a more detailed model of the fluid forces in the viscous fluid layer, we will assume that the effect can be modeled as a massless rotational damper obeying the linear damping law as shown in the figure The equation of motion with the given input velocity 𝜔𝑑 𝐼1 𝜔1 + 𝑐𝑇 𝜔1 − 𝜔𝑑 = 𝑇1 or 𝐼1 𝜔1 + 𝑐𝑇 𝜔1 = 𝑇1 + 𝑐𝑇 𝜔𝑑 System Dynamics 4.70 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples - Example 4.5.7 A Two-Inertia Fluid-Clutch Model The figure is a fluid clutch model that can be used when the torque on the driving shaft is not sufficient to drive the disk on that side at the specified speed 𝜔𝑑 To account for this situation, we must include the inertia of the driving side in the model Assume that the torques 𝑇𝑑 and 𝑇1 are specified functions of time a Derive the equations of motion for the speeds 𝜔𝑑 and 𝜔1 b Obtain the transfer functions Ω𝑠 (𝑠)/𝑇1 (𝑠) and Ω𝑠 (𝑠)/𝑇𝑑 (𝑠) c Obtain the expression for the response 𝜔1(𝑡) if the initial conditions are zero, 𝑇1 = 0, and 𝑇𝑑 is a step function of magnitude 𝑀 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.72 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples b Obtain the transfer functions Ω𝑠 (𝑠)/𝑇1 (𝑠) and Ω𝑠 (𝑠)/𝑇𝑑 (𝑠) Applying the Laplace transform to the equations of motion with zero initial conditions 𝐼𝑑 𝑠Ω𝑑 (𝑠) + 𝑐𝑇 [Ω𝑑 𝑠 − Ω1 𝑠 ] = 𝑇𝑑 (𝑠) ⟹ 𝐼𝑑 𝑠 + 𝑐𝑇 Ω𝑑 𝑠 − 𝑐𝑇 Ω1 𝑠 = 𝑇𝑑 (𝑠) (1) 𝐼1 𝑠Ω1 𝑠 + 𝑐𝑇 [Ω1 𝑠 − Ω𝑑 𝑠 ] = −𝑇1(𝑠) ⟹ 𝑐𝑇 Ω𝑑 𝑠 − [𝐼1 𝑠 + 𝑐𝑇 ]Ω1 𝑠 = 𝑇1 (𝑠) (2) Eliminate Ω𝑑 𝑠 from equations (1) and (2) 𝑐𝑇 𝐼𝑑 𝑠 + 𝑐𝑇 Ω1 𝑠 = 𝑇 𝑠 − 𝑇 𝑠 𝑠 𝐼1 𝐼𝑑 𝑠 + 𝑐𝑇 𝐼1 + 𝑐𝑇 𝐼𝑑 𝑑 𝑠 𝐼1 𝐼𝑑 𝑠 + 𝑐𝑇 𝐼1 + 𝑐𝑇 𝐼𝑑 The transfer functions Ω1 𝑠 𝑐𝑇 Ω1 𝑠 𝐼𝑑 𝑠 + 𝑐𝑇 = = 𝑇𝑑 𝑠 𝑠 𝐼1 𝐼𝑑 𝑠 + 𝑐𝑇 𝐼1 + 𝑐𝑇 𝐼𝑑 𝑇1 𝑠 𝑠 𝐼1 𝐼𝑑 𝑠 + 𝑐𝑇 𝐼1 + 𝑐𝑇 𝐼𝑑 HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 12 8/25/2013 System Dynamics 4.73 Spring & DamperElementsinMechanicalSystems System Dynamics 4.74 Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples c Obtain the expression for the response 𝜔1(𝑡) Setting 𝑇1 𝑠 = and 𝑇𝑑 𝑠 = 𝑀/𝑠 gives 𝑐𝑇 𝑀 Ω1 𝑠 = 𝑠 𝐼1 𝐼𝑑 𝑠 + 𝑐𝑇 𝐼1 + 𝑐𝑇 𝐼𝑑 𝑠 Define 𝑐𝑇 𝐼1 + 𝑐𝑇 𝐼𝑑 𝑐𝑇 𝑎≡ , 𝑏≡ 𝐼1 𝐼𝑑 𝐼1 𝐼𝑑 𝑏 𝑀 𝑏𝑀 1 ⟹ Ω1 𝑠 = = − + 𝑠 𝑠+𝑎 𝑠 𝑎 𝑠 𝑎𝑠 𝑎(𝑠 + 𝑎) and the corresponding response 𝑏𝑀 1 𝜔1 𝑡 = 𝑡 − + 𝑒 −𝑎𝑡 𝑎 𝑎 𝑎 The time constant is 𝜏 = 1/𝑎 For 𝑡 > 4/𝑎 approximately, the speed increases linearly with time §5.Additional Modeling Examples - Example 4.5.8 The Quarter-Car Model The quarter-car model of a vehicle suspension is shown in the figure The masses of the wheel, tire, and axle are neglected, and the mass 𝑚 represents one fourth of the vehicle mass The spring constant 𝑘 models the elasticity of both the tire and the suspension spring The damping constant 𝑐 models the shock absorber The equilibrium position of 𝑚 when 𝑦 = is 𝑥 = The road surface displacement 𝑦(𝑡) can be derived from the road surface profile and the car’s speed Derive the equation of motion of 𝑚 with 𝑦(𝑡) as the input, and obtain the transfer function HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.75 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems System Dynamics 4.76 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples Solution Obtain the equation of motion from the free body diagram 𝑚𝑥 + 𝑐 𝑥 − 𝑦 + 𝑘 𝑥 − 𝑦 = ⟹ 𝑚𝑥 + 𝑐 𝑥 + 𝑘𝑥 = 𝑐 𝑦 + 𝑘𝑦 The transfer function is found by applying the Laplace transform to the equation, with the initial conditions set to zero 𝑚𝑠 𝑋 𝑠 + 𝑐𝑠𝑋 𝑠 = 𝑘𝑋 𝑠 = 𝑐𝑠𝑌 𝑠 + 𝑘𝑌(𝑠) 𝑋(𝑠) 𝑐𝑠 + 𝑘 ⟹ = 𝑌(𝑠) 𝑚𝑠 + 𝑐𝑠 + 𝑘 §5.Additional Modeling Examples - Example 4.5.9 A Quarter-Car Model with Two-Masses The suspension model shown in the figure includes the mass of the wheel-tire-axle assembly The mass 𝑚1 is one-fourth the mass of the car body, and 𝑚2 is the mass of the wheel-tire-axle assembly The spring constant 𝑘1 represents the suspension’s elasticity, and 𝑘2 represents the tire’s elasticity Derive the equations of motion for 𝑚1 and 𝑚2 in terms of 𝑥1 and 𝑥2 Solution The equation of motion 𝑚1 𝑥1 + 𝑐1 𝑥1 − 𝑥2 + 𝑘1 𝑥1 − 𝑥2 = 𝑚2 𝑥2 + 𝑐1 𝑥2 − 𝑥1 + 𝑘1 𝑥2 − 𝑥1 + 𝑘2 (𝑥2 − 𝑦) = HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.77 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems System Dynamics 4.78 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples - Example 4.5.10 Stability of an Inverted Pendulum Determine the effects of stiffness and damping on the stability properties of an inverted pendulum with small 𝜙 Solution The equation of motion (𝑠𝑖𝑛𝜙 ≈ 𝜙, 𝑐𝑜𝑠𝜙 ≈ 1) 𝐼𝑂 𝜙 = 𝑀𝑂 ⟹ 𝑚𝐿2 𝜙 = 𝑚𝑔𝐿𝜙 − 𝐿1 𝑐𝐿1 𝜙 −𝐿1 𝑘𝐿1 𝜙 𝑐𝐿21 𝑘𝐿21 − 𝑚𝑔𝐿 ⟹𝜙+ 𝜙+ 𝜙=0 𝑚𝐿2 𝑚𝐿2 Define 𝑐𝐿21 𝑘𝐿21 − 𝑚𝑔𝐿 𝑎≡ , 𝑏≡ 𝑚𝐿2 𝑚𝐿2 ⟹ 𝜙 + 𝑎 𝜙 + 𝑏𝜙 = §5.Additional Modeling Examples 𝑐𝐿21 𝑘𝐿21 − 𝑚𝑔𝐿 𝜙 + 𝑎𝜙 + 𝑏𝜙 = 0, 𝑎≡ , 𝑏≡ 𝑚𝐿 𝑚𝐿2 If 𝑎 > 0, 𝑏 > 0: the system is stable For parameter 𝑎 • 𝑎 ≮ for physically realistic values of 𝑐, 𝐿1 , 𝑚, 𝐿 • 𝑎 = if there is no damping, 𝑐 = ⟹ some damping is necessary for the system to be stable HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien Nguyen Tan Tien 13 8/25/2013 System Dynamics 4.79 Spring & DamperElementsinMechanicalSystems System Dynamics 4.80 Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples 𝑐𝐿21 𝑘𝐿21 − 𝑚𝑔𝐿 𝜙 + 𝑎𝜙 + 𝑏𝜙 = 0, 𝑎≡ , 𝑏≡ 𝑚𝐿2 𝑚𝐿2 For parameter 𝑏 • If 𝑏 < (𝑘𝐿21 < 𝑚𝑔𝐿): the system is unstable The torque from the spring is not great enough to overcome the torque due to gravity, and thus the mass will fall • If 𝑏 = 0, 𝑐 = 0: the two roots are both zero→neutral stability If slightly displaced with zero initial velocity, the mass will remain in that position • If 𝑏 > 0, 𝑐 = 0: the two roots are imaginary→neutrally stable If slightly displaced, the mass will oscillate about 𝜙 = with a constant amplitude §5.Additional Modeling Examples Step Response with an Input Derivative - Consider the following first-order model contains an input derivative 𝑚𝑣 + 𝑐𝑣 = 𝑏𝑓 + 𝑓 The transfer function 𝑉(𝑠) 𝑏𝑠 + = 𝐹(𝑠) 𝑚𝑠 + 𝑐 The presence of an input derivative is indicated by an 𝑠 term in the numerator This presence is called numerator dynamics Inmechanical systems, numerator dynamics occurs when a displacement input acts directly on a damper - An example of a device having numerator dynamics 𝑋(𝑠) 𝑐𝑠 + 𝑘1 𝑐 𝑥 − 𝑦 + 𝑘1 𝑥 − 𝑦 + 𝑘2 𝑥 = ⟹ = 𝑌(𝑠) 𝑐𝑠 + 𝑘1 + 𝑘2 or 𝑐 𝑥 + 𝑘1 + 𝑘2 𝑥 = 𝑐 𝑦 + 𝑘1 𝑦 HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.81 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples Constant Inputs versus Step Inputs - Consider the model 𝑚𝑣 + 𝑐𝑣 = 𝑏𝑓 + 𝑓 • 𝑓(𝑡) = 𝐹 = 𝑐𝑜𝑛𝑠𝑡𝑎𝑛𝑡 𝑓(𝑡) = 𝐹 for −∞ ≤ 𝑡 ≤ ∞ ⟹ 𝑓(𝑡) = for −∞ ≤ 𝑡 ≤ ∞ The existence of the input derivative in the model does not affect the response, the model reduces to 𝑐 𝐹 𝑚𝑣 + 𝑐𝑣 = 𝐹 ⟹ 𝑣 + 𝑣 = 𝑚 𝑚 𝐹 𝐹 ⟹ 𝑣 𝑡 = + 𝐶𝑒 −𝑐𝑡/𝑚 = 𝑣 𝑒 −𝑐𝑡/𝑚 + (1 − 𝑒 −𝑐𝑡/𝑚 ) 𝑐 𝑐 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.83 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples - Comparing • 𝑓 𝑡 constant: 𝑣 𝑡 = 𝑣 𝑒 −𝑐𝑡/𝑚 + • 𝑓(𝑡) is a step: 𝑣 𝑡 = 𝑣 + 𝑏𝐹 𝑚 𝐹 𝑐 𝑐𝑡 − 𝑒 −𝑚 𝐹 𝑒 −𝑐𝑡/𝑚 + (1 − 𝑒 −𝑐𝑡/𝑚 ) 𝑐 ⟹ The effect of the term 𝑏𝑓(𝑡) is to increase the initial value for 𝑣(𝑡) by the amount 𝑏𝐹/𝑚 - No physical variable can be discontinuous, and therefore the step function is only an approximate description of an input that changes quickly - The reason for using a step function is to reduce the complexity of the mathematics required to find the response HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien System Dynamics 4.82 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems Đ5.Additional Modeling Examples () is a step function of magnitude 𝐹 Using the Laplace transform to derive the response 𝑚 𝑠𝑉 𝑠 − 𝑣 + 𝑐𝑉 𝑠 = 𝑏 𝑠𝐹 𝑠 − 𝑓 + 𝐹 𝑠 𝐹 𝐹 = 𝑏 𝑠 − 𝑓(0) + 𝑠 𝑠 with 𝑓(0) = 𝑚𝑣 𝑏𝐹 𝐹 𝑉 𝑠 = + + 𝑚𝑠 + 𝑐 𝑚𝑠 + 𝑐 𝑠(𝑚𝑠 + 𝑐) The inverse transform gives 𝑏𝐹 −𝑐𝑡/𝑚 𝐹 𝑣 𝑡 = 𝑣 𝑒 −𝑐𝑡/𝑚 + 𝑒 + (1 − 𝑒 −𝑐𝑡/𝑚 ) 𝑚 𝑐 HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.84 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples - Example 4.5.11 An Approximation to the Step Function Consider the following model 𝑣 + 10𝑣 = 𝑓 + 𝑓 where 𝑓(𝑡) is the input and 𝑣(0) = a Obtain the expression for the unit-step response b Obtain the response to the input 𝑓(𝑡) = − 𝑒 −100𝑡 and compare with the results of part (a) Solution a Obtain the expression for the unit-step response Apply the previous result with 𝑚 = 1, 𝑐 = 10, 𝑏 = 1, 𝐹 = 𝑣(𝑡) = 0.1 + 0.9𝑒 −10𝑡 HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien 14 8/25/2013 System Dynamics 4.85 Spring & DamperElementsinMechanicalSystems System Dynamics 4.86 Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples b Obtain the response to the input 𝑓(𝑡) = − 𝑒 −100𝑡 𝑓(𝑡) = − 𝑒 −100𝑡 resembles a step function except that it is continuous 𝑠+1 𝑣 + 10𝑣 = 𝑓 + 𝑓 ⟹ 𝑉 𝑠 = 𝐹(𝑠) 𝑠 + 10 100 𝑓 = − 𝑒 −100𝑡 ⟹ 𝐹 𝑠 = 𝑠(𝑠 + 100) 𝑠+1 100 0.1 1.1 ⟹𝑉 𝑠 = = − + 𝑠 + 10 𝑠(𝑠 + 100) 𝑠 𝑠 + 100 𝑠 + 10 ⟹ 𝑣 𝑡 = 0.1 − 1.1𝑒 −100𝑡 + 𝑒 −10𝑡 §5.Additional Modeling Examples - Example 4.5.12 Damper Location and Numerator Dynamics HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.87 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems By obtaining the equations of motion and the transfer functions of the two systems shown in the figure, investigate the effect of the location of the damper on the step response of the system The displacement 𝑦(𝑡) is a given function Obtain the unit-step response for each system for the specific case 𝑚 = 1, 𝑐 = 6, and 𝑘 = 8, with zero initial conditions System Dynamics 4.88 Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples Solution The equation of motion 𝑚𝑥 + 𝑐(𝑥 − 𝑦) + 𝑘(𝑥 − 𝑦) = ⟹ 𝑚𝑥 + 𝑐 𝑥 + 𝑘𝑥 = 𝑐 𝑦 + 𝑘𝑦 The transfer function 𝑋(𝑠) 𝑐𝑠 + 𝑘 = 𝑌(𝑠) 𝑚𝑠 + 𝑐𝑠 + 𝑘 Substituting the given values and using step function 𝑌 𝑠 = 1/𝑠 6𝑠 + 1 𝑋 𝑠 = = + − 𝑠(𝑠 + 6𝑠 + 8) 𝑠 𝑠 − 𝑠 + ⟹ 𝑥 𝑡 = + 𝑒 −2𝑡 − 2𝑒 −4𝑡 §5.Additional Modeling Examples HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.89 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems The equation of motion 𝑚𝑥 + 𝑐 𝑥 + 𝑘(𝑥 − 𝑦) = ⟹ 𝑚𝑥 + 𝑐 𝑥 + 𝑘𝑥 = 𝑘𝑦 The transfer function 𝑋(𝑠) 𝑘 = 𝑌(𝑠) 𝑚𝑠 + 𝑐𝑠 + 𝑘 Substituting the given values and using step function 𝑌 𝑠 = 1/𝑠 𝑋 𝑠 = = − + 𝑠(𝑠 + 6𝑠 + 8) 𝑠 𝑠 − 𝑠 + ⟹ 𝑥 𝑡 = − 2𝑒 −2𝑡 + 𝑒 −4𝑡 System Dynamics 4.90 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §5.Additional Modeling Examples Effect of numerator dynamics on step response • (a) corresponds to the system with numerator dynamics, and (b) corresponds to the system without numerator dynamics • The numerator dynamics causes an overshoot in the response but does not affect the steady-state response ⟹ The damper location can affect the response • The damper location does not affect the time constants, because both systems have the same characteristic roots ⟹ both take about the same length of time to approach steady state §6.Collisions and Impulse Response HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien Nguyen Tan Tien - Ramp function An input that changes at a constant - Step function An input that rapidly reaches a constant value - Rectangular pulse function A constant input that is suddenly removed - The impulsive function Similar to the pulse function, but it models an input that is suddenly applied and removed after a very short (infinitesimal) time Nguyen Tan Tien 15 8/25/2013 System Dynamics 4.91 Spring & DamperElementsinMechanicalSystems §6.Collisions and Impulse Response - The strength of an impulsive input is the area under its curve The Dirac delta function 𝛿(𝑡) is an impulsive function with a strength equal to unity 0+ - The Dirac function is an analytically convenient approximation of an input applied for only a very short time, such as the interaction force between two colliding objects It is also useful for estimating the system’s parameters experimentally and for analyzing the effect of differentiating a step or any other discontinuous input function - The response to an impulsive input is called the impulse response In particular, the response to 𝛿(𝑡) is called the unit impulse response System Dynamics 4.93 4.92 Spring & DamperElementsinMechanicalSystems - Impulse-momentum principle 𝑚𝑣(𝑡) − 𝑚𝑣(0) = 𝛿 𝑡 𝑑𝑡 = HCM City Univ of Technology, Mechanical Engineering Department System Dynamics §6.Collisions and Impulse Response Initial Conditions and Impulse Response - An example of a force often modeled as impulsive is the force generated when two objects collide Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems 𝑡 𝑓 𝑢 𝑑𝑢 - In the terminology of mechanics, the force integral, the area under the force-time curve, is called the linear impulse The linear impulse is the strength of an impulsive force, but a force need not be impulsive to produce a linear impulse - If 𝑓(𝑡) is an impulsive input of strength 𝐴, 𝑓(𝑡) = 𝐴𝛿(𝑡), then 0+ 𝑚𝑣 + − 𝑚𝑣 = 0+ 𝐴𝛿 𝑢 𝑑𝑢 = 𝐴 𝛿 𝑢 𝑑𝑢 = 𝐴 since the area under the 𝛿(𝑡) curve is So the change in momentum equals the strength of the impulsive force HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.94 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems §6.Collisions and Impulse Response - Example 4.6.1 Inelastic Collision Suppose a mass 𝑚1 = 𝑚 moving with a speed 𝑣1 becomes embedded in mass 𝑚2 after striking it Suppose 𝑚2 = 10 Determine the expression for the displacement 𝑥(𝑡) after the collision Solution If we take the entire system to consist of both masses, then the force of collision is internal to the system Because the displacement of 𝑚2 immediately after the collision will be small, we may neglect the spring force initially Thus, the external force 𝑓(𝑡) is zero 𝑚 + 10𝑚 𝑣 + − 𝑚𝑣1 + 10𝑚 × = 𝑚𝑣1 ⟹𝑣 0+ = = 𝑣 11𝑚 11 §6.Collisions and Impulse Response The equation of motion for the combined mass 11𝑚𝑥 + 𝑘𝑥 = We can solve it for 𝑡 ≥ + by using the initial conditions at 𝑡 = 0; namely, 𝑥(0+) = and 𝑥(0+) = 𝑣(0+) The solution is HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.95 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems 𝑥 𝑡 = 𝑣(0+) 𝑣1 11𝑚 𝑘 𝑠𝑖𝑛𝜔𝑛 𝑡 = 𝑠𝑖𝑛 𝑡 𝜔𝑛 11 𝑘 11𝑚 Note that it was unnecessary to determine the impulsive collision force Note also that this force did not change 𝑥 initially; it changed only 𝑥 System Dynamics 4.96 Spring & DamperElementsinMechanicalSystems §6.Collisions and Impulse Response Consider the two colliding masses shown in the figure • part (a): the situation before collision • part (b): the situation after collision When the two masses are treated as a single system, no external force is applied to the system, the momentum is conserved 𝑚1 𝑣1 + 𝑚2 𝑣2 = 𝑚3 𝑣3 + 𝑚4 𝑣4 ⟹ 𝑚1 𝑣1 − 𝑣3 = −𝑚2 (𝑣2 − 𝑣4 ) If the collision is perfectly elastic, kinetic energy is conserved 1 1 𝑚 𝑣2 + 𝑚 𝑣2 = 𝑚 𝑣2 + 𝑚 𝑣2 1 2 2 2 1 ⟹ 𝑚1 (𝑣12 − 𝑣32 ) = − 𝑚2 (𝑣22 − 𝑣42 ) 2 1 ⟹ 𝑚1 (𝑣1 − 𝑣3 )(𝑣1 + 𝑣3 ) = − 𝑚2 (𝑣2 − 𝑣4 )(𝑣2 + 𝑣4 ) 2 §6.Collisions and Impulse Response HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien Nguyen Tan Tien ⟹ 𝑣1 + 𝑣3 = 𝑣2 + 𝑣4 or 𝑣1 − 𝑣2 = 𝑣4 − 𝑣3 This relations says that in a perfectly elastic collision the relative velocity of the masses changes sign but its magnitude remains the same The most common application is where we know 𝑣1 and mass 𝑚2 is initially stationary, so that 𝑣2 = In this case, the velocities after collision as follows 𝑚1 − 𝑚2 𝑣3 = 𝑣 𝑚1 + 𝑚2 2𝑚1 𝑣4 = 𝑣 𝑚1 + 𝑚2 Nguyen Tan Tien 16 8/25/2013 System Dynamics 4.97 Spring & DamperElementsinMechanicalSystems System Dynamics 4.98 Spring & DamperElementsinMechanicalSystems §6.Collisions and Impulse Response - Example 4.6.2 Perfectly Elastic Collision Consider the system as shown The mass 𝑚1 = 𝑚 moving with a speed 𝑣1 rebounds from the mass 𝑚2 = 10𝑚 after striking it Assume that the collision is perfectly elastic Determine the expression for the displacement 𝑥(𝑡) after the collision Solution For a perfectly elastic collision, the velocity 𝑣3 of the mass 𝑚 after the collision is given by 𝑚1 − 𝑚2 𝑚 − 10𝑚 𝑣3 = 𝑣 = 𝑣 = − 𝑣1 𝑚1 + 𝑚2 𝑚 + 10𝑚 11 The change in the momentum of 𝑚 0+ 𝑚 − 𝑣1 − 𝑚𝑣1 = 𝑓 𝑡 𝑑𝑡 11 §6.Collisions and Impulse Response The linear impulse applied to the mass 𝑚 during the collision 0+ 20 𝑓 𝑡 𝑑𝑡 = − 𝑚𝑣1 11 From Newton’s law of action and reaction, the linear impulse applied to the 10𝑚 mass is +20𝑚𝑣1 /11 , and equation of motion 20 10𝑚𝑥 + 𝑘𝑥 = 𝑚𝑣1 𝛿(𝑡) 11 The Laplace transform gives 20 2𝑣1 10𝑚𝑠 + 𝑘 𝑋 𝑠 = 𝑚𝑣1 ⟹ 𝑋 𝑠 = 11 11 𝑠 + 𝑘/10𝑚 HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.99 Nguyen Tan Tien Spring & DamperElementsinMechanicalSystems ⟹𝑥 𝑡 = System Dynamics 2𝑣1 10𝑚 𝑘 𝑠𝑖𝑛 𝑡 11 𝑘 10𝑚 Nguyen Tan Tien 4.100 Spring & DamperElementsinMechanicalSystems §7.Matlab Applications residue: to obtain the coefficients of a partial-fraction expansion conv: to multiply polynomials step: to compute the step responses from transfer functions impulse: to compute the impulse responses from transfer functions §7.Matlab Applications - Example 4.7.2 Determining the Free Response with MATLAB Use the MATLAB step function to obtain a plot of the free response of the following model, with 𝑥(0) = and 𝑥 = 5𝑥 + 3𝑥 + 10𝑥 = Solution Applying the Laplace transform gives 𝑠2𝑋 𝑠 − 𝑠𝑥 − 𝑥 + 𝑠𝑋 𝑠 − 𝑥 + 10𝑋 𝑠 = ⟹ 5𝑠2 + 3𝑠 + 10 𝑋 𝑠 = 20𝑠 + 22 20𝑠 + 22 20𝑠2 + 22𝑠 1 ⟹𝑋 𝑠 = = = 𝑇(𝑠) 5𝑠 + 3𝑠 + 10 5𝑠 + 3𝑠 + 10 𝑠 𝑠 Matlab sys = tf([20, 22, 0],[5, 3, 10]); step(sys) HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department System Dynamics Nguyen Tan Tien 4.101 Spring & DamperElementsinMechanicalSystems System Dynamics Nguyen Tan Tien 4.102 Spring & DamperElementsinMechanicalSystems §7.Matlab Applications - Example 4.7.1 Obtaining the Free Response with the step Function For the system shown in the figure, suppose that 𝑚1 = 𝑚2 = 1, 𝑐1 = 2, 𝑐2 = 3, 𝑘1 = 1, and 𝑘2 = a Obtain the plot of the unit-step response of 𝑥2 for zero initial conditions b Use two methods with MATLAB to obtain the free response for 𝑥1(𝑡) , for the initial conditions 𝑥1 (0) = 3, 𝑥1 (0) = 2, 𝑥2 (0) = 1, and 𝑥2 (0) = Solution Equations of motion 𝑚1 𝑥1 + (𝑐1 +𝑐2 )𝑥1 − 𝑐2 𝑥2 + 𝑘1 + 𝑘2 𝑥1 − 𝑘2 𝑥2 = 𝑚2 𝑥2 + 𝑐2 𝑥2 − 𝑐2 𝑥1 + 𝑘2 𝑥2 − 𝑘2 𝑥1 = 𝑓 §7.Matlab Applications with the given parameters 𝑥1 + 5𝑥1 + 5𝑥1 − 3𝑥2 − 4𝑥2 = 𝑥2 + 3𝑥2 + 4𝑥2 − 3𝑥1 − 4𝑥1 = 𝑓 Transforming the equations with the given initial conditions 𝑠2𝑋1 𝑠 − 𝑠𝑥1 − 𝑥1 + 𝑠𝑋1 𝑠 − 𝑥1 + 5𝑋1 𝑠 −3 𝑠𝑋2 𝑠 − 𝑥2 − 4𝑋2 𝑠 = 𝑠2𝑋2 𝑠 − 𝑠𝑥2 − 𝑥2 + 𝑠𝑋2 𝑠 − 𝑥2 + 4𝑋2 𝑠 −3 𝑠𝑋1 𝑠 − 𝑥1 − 4𝑋1 𝑠 = 𝑓 Collecting terms results in 𝑠 + 5𝑠 + 𝑋1 𝑠 − 3𝑠 + 𝑋2 𝑠 = 𝐼1 (𝑠) (1) − 3𝑠 + 𝑋1 𝑠 + 𝑠 + 3𝑠 + 𝑋2 𝑠 = 𝐼2 (𝑠) + 𝐹(𝑠) (2) with 𝐼1 𝑠 ≡ 𝑥1 𝑠 + 𝑥1 + 5𝑥1 − 3𝑥2 𝐼2 (𝑠) ≡ 𝑥2 𝑠 + 𝑥2 + 3𝑥2 − 3𝑥1 HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien Nguyen Tan Tien 17 8/25/2013 4.103 Spring & DamperElementsinMechanicalSystems System Dynamics 4.104 Spring & DamperElementsinMechanicalSystems §7.Matlab Applications a Obtain the plot of the unit-step response of 𝑥2 for zero initial conditions The transfer functions for the input 𝑓(𝑡) are found by setting 𝐼1 (𝑠) = 𝐼2 (𝑠) = in 𝐷1 (𝑠) and 𝐷2 (𝑠) 𝑋1 (𝑠) 𝐷1(𝑠) 3𝑠 + 𝑋2 (𝑠) 𝐷2 (𝑠) 𝑠 + 5𝑠 + = = , = = 𝐹(𝑠) 𝐷(𝑠) 𝐷(𝑠) 𝐹(𝑠) 𝐷(𝑠) 𝐷(𝑠) Matlab D = conv([1,5,5], [1,3,4])-conv([0,3,4], [0,3,4]); x2 = tf([1,5,5],D); step(x2) Step Response 1.4 1.2 Amplitude System Dynamics §7.Matlab Applications The determinant of the left-hand side of the equations (1) & (2) 𝐷 𝑠 = 𝑠 + 5𝑠 + 2−3𝑠 − −3𝑠 − 𝑠 + 3𝑠 + = 𝑠 + 5𝑠 + 𝑠 + 3𝑠 + − (3𝑠 + 4)2 𝐼1 (𝑠) −3𝑠 − 𝐷1 𝑠 = 𝐼2 𝑠 + 𝐹(𝑠) 𝑠 + 3𝑠 + = 𝑠 + 3𝑠 + 𝐼1 𝑠 + (3𝑠 + 4)𝐼2 (𝑠) + (3𝑠 + 4)𝐹(𝑠) 𝑠 + 5𝑠 + 𝐼1 (𝑠) 𝐷2 𝑠 = −3𝑠 − 𝐼2 𝑠 + 𝐹(𝑠) = 𝑠 + 5𝑠 + 𝐼2 𝑠 + (3𝑠 + 4)𝐼1 (𝑠) + 𝑠 + 5𝑠 + 𝐹(𝑠) The solutions for 𝑋1 (𝑠) and 𝑋2 (𝑠) can be expressed as 𝐷1 (𝑠) 𝐷2 (𝑠) 𝑋1 𝑠 = , 𝑋2 𝑠 = 𝐷(𝑠) 𝐷(𝑠) 0.8 0.6 0.4 0.2 0 10 12 14 Time (sec) HCM City Univ of Technology, Mechanical Engineering Department System Dynamics Nguyen Tan Tien 4.105 Spring & DamperElementsinMechanicalSystems HCM City Univ of Technology, Mechanical Engineering Department System Dynamics 4.106 Spring & DamperElementsinMechanicalSystems §7.Matlab Applications b Use two methods with MATLAB to obtain the free response for 𝑥1(𝑡) Matlab % Specify the initial conditions x10 = 3; x1d0 = 2; x20 = 1; x2d0 = 4; % Form the initial-condition arrays I1 = [x10,x1d0+5*x10-3*x20]; I2 = [x20,x2d0+3*x20-3*x10]; % Form the determinant D1 D1 = conv([1,3,4,0],I1)+conv([0,3,4,0],I2); % Form the determinant D D = conv([1,5,5],[1,3,4])-conv([0,3,4],[0,3,4]); sys = tf(D1,D); step(sys) §7.Matlab Applications Matlab % Specify the initial conditions x10 = 3; x1d0 = 2; x20 = 1; x2d0 = 4; HCM City Univ of Technology, Mechanical Engineering Department HCM City Univ of Technology, Mechanical Engineering Department Nguyen Tan Tien Nguyen Tan Tien % Form the initial-condition vectors I1 = [x10,x1d0+5*x10-3*x20]; I2 = [x20,x2d0+3*x20-3*x10]; % Form the determinant D1 D1 = conv([1,3,4],I1)+conv([0,3,4],I2); % Compute the partial fraction expansion [r,p,K] = residue(D1,D); % Use time constants to estimate the simulation time tmax = floor(-5/max(real(p))); t = (0:tmax/500:tmax); % Evaluate the time functions x1 = real(r(1)*exp(p(1)*t)+r(2)*exp(p(2)*t)+ r(3)*exp(p(3)*t)+r(4)*exp(p(4)*t)); plot(t,x1),xlabel('t'),ylabel('x 1') Nguyen Tan Tien 18 ... Dynamics 4.13 Spring & Damper Elements in Mechanical Systems §1 .Spring Elements Solution System Dynamics 4.14 Spring & Damper Elements in Mechanical Systems §1 .Spring Elements - Most spring elements. .. Tien Spring & Damper Elements in Mechanical Systems §1 .Spring Elements 4.Series and parallel spring elements - Series spring elements =