WEEK 1 Dynamics of Machinery

Similar documents
WEEKS 2-3 Dynamics of Machinery

FORCE ANALYSIS OF MACHINERY. School of Mechanical & Industrial Engineering, AAiT

Rotational & Rigid-Body Mechanics. Lectures 3+4

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

Chapter 4 Statics and dynamics of rigid bodies

Engineering Mechanics Prof. U. S. Dixit Department of Mechanical Engineering Indian Institute of Technology, Guwahati

Chapter 5. The Laws of Motion

Physics 111 Lecture 4 Newton`s Laws

Physics 101 Lecture 5 Newton`s Laws

Vector Mechanics: Statics

General Physics I. Lecture 8: Rotation of a Rigid Object About a Fixed Axis. Prof. WAN, Xin ( 万歆 )

Static Equilibrium. University of Arizona J. H. Burge

JNTU World. Subject Code: R13110/R13

Chapter 9 TORQUE & Rotational Kinematics

General Physics I. Lecture 8: Rotation of a Rigid Object About a Fixed Axis. Prof. WAN, Xin ( 万歆 )

MEE224: Engineering Mechanics Lecture 4

Figure Two. Then the two vector equations of equilibrium are equivalent to three scalar equations:

Final Exam April 30, 2013

Dynamics of Machinery

Chapter 5. The Laws of Motion

RIGID BODY MOTION (Section 16.1)

Equilibrium of a Rigid Body. Engineering Mechanics: Statics

PLANAR KINETICS OF A RIGID BODY FORCE AND ACCELERATION

1. Replace the given system of forces acting on a body as shown in figure 1 by a single force and couple acting at the point A.

3.1 CONDITIONS FOR RIGID-BODY EQUILIBRIUM

General Definition of Torque, final. Lever Arm. General Definition of Torque 7/29/2010. Units of Chapter 10

Università degli Studi di Bari. mechanics 1. Load system determination. Joint load. Stress-strain distribution. Biological response 2/45 3/45

DEPARTMENT OF MECHANICAL ENGINEERING Dynamics of Machinery. Submitted

where G is called the universal gravitational constant.

DEVIL PHYSICS BADDEST CLASS ON CAMPUS IB PHYSICS

The Laws of Motion. Newton s first law Force Mass Newton s second law Gravitational Force Newton s third law Examples

7. FORCE ANALYSIS. Fundamentals F C

Hong Kong Institute of Vocational Education (Tsing Yi) Higher Diploma in Civil Engineering Structural Mechanics. Chapter 1 PRINCIPLES OF STATICS

PLANAR RIGID BODY MOTION: TRANSLATION &

Chapter 5. The Laws of Motion

Chapter 8. Rotational Equilibrium and Rotational Dynamics. 1. Torque. 2. Torque and Equilibrium. 3. Center of Mass and Center of Gravity

Similar to trusses, frames are generally fixed, load carrying structures.

Introduction to Dynamics

INTRODUCTION. The three general approaches to the solution of kinetics. a) Direct application of Newton s law (called the forcemass-acceleration

Class XI Chapter 7- System of Particles and Rotational Motion Physics

TUTORIAL SHEET 1. magnitude of P and the values of ø and θ. Ans: ø =74 0 and θ= 53 0

Engineering Mechanics: Statics in SI Units, 12e

Lecture 14. Rotational dynamics Torque. Give me a lever long enough and a fulcrum on which to place it, and I shall move the world.

PLANAR KINETIC EQUATIONS OF MOTION (Section 17.2)

1 MR SAMPLE EXAM 3 FALL 2013

*Definition of Mechanics *Basic Concepts *Newton s Laws *Units

6. Find the net torque on the wheel in Figure about the axle through O if a = 10.0 cm and b = 25.0 cm.

Physics for Scientists and Engineers 4th Edition, 2017

A B Ax Bx Ay By Az Bz

STATICS & DYNAMICS. Engineering Mechanics. Gary L. Gray. Francesco Costanzo. Michael E. Plesha. University of Wisconsin-Madison

ME 230 Kinematics and Dynamics

ME 201 Engineering Mechanics: Statics. Final Exam Review

General Physics I. Lecture 9: Vector Cross Product. Prof. WAN, Xin ( 万歆 )

STATICS. FE Review. Statics, Fourteenth Edition R.C. Hibbeler. Copyright 2016 by Pearson Education, Inc. All rights reserved.

Phys101 Lectures 19, 20 Rotational Motion

What is a Force? Free-Body diagrams. Contact vs. At-a-Distance 11/28/2016. Forces and Newton s Laws of Motion

Ground Rules. PC1221 Fundamentals of Physics I. Force. Zero Net Force. Lectures 9 and 10 The Laws of Motion. A/Prof Tay Seng Chuan

LANMARK UNIVERSITY OMU-ARAN, KWARA STATE DEPARTMENT OF MECHANICAL ENGINEERING COURSE: MECHANICS OF MACHINE (MCE 322). LECTURER: ENGR.

ME101: Engineering Mechanics ( )

Engineering Problem Solving ENG1101. Physics 101 For The Design Project Mathematical Model

Chapter 8 Rotational Motion

EQUATIONS OF EQUILIBRIUM & TWO- AND THREE-FORCE MEMBERS

Lectures Chapter 10 (Cutnell & Johnson, Physics 7 th edition)

Balancing of Masses. 1. Balancing of a Single Rotating Mass By a Single Mass Rotating in the Same Plane

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA ADVANCED MECHANICAL PRINCIPLES AND APPLICATIONS UNIT 18 NQF LEVEL 3

Lecture Outline Chapter 11. Physics, 4 th Edition James S. Walker. Copyright 2010 Pearson Education, Inc.

The Concept of Force Newton s First Law and Inertial Frames Mass Newton s Second Law The Gravitational Force and Weight Newton s Third Law Analysis

PEMP-AML2506. Day 01B. Session Speaker Dr. M. D. Deshpande. M.S. Ramaiah School of Advanced Studies - Bangalore 1 01B

VALLIAMMAI ENGINEERING COLLEGE SRM NAGAR, KATTANKULATHUR DEPARTMENT OF MECHANICAL ENGINEERING

Models and Anthropometry

Engineering Problem Solving ENG1101. Physics 101 For The Design Project Mathematical Model

Tenth Edition STATICS 1 Ferdinand P. Beer E. Russell Johnston, Jr. David F. Mazurek Lecture Notes: John Chen California Polytechnic State University

CEE 271: Applied Mechanics II, Dynamics Lecture 24: Ch.17, Sec.1-3

PHYS-2010: General Physics I Course Lecture Notes Section V

Chapter 8 Lecture Notes

EQUATIONS OF MOTION: CYLINDRICAL COORDINATES

Plane Motion of Rigid Bodies: Forces and Accelerations

11.1 Virtual Work Procedures and Strategies, page 1 of 2

Practice. Newton s 3 Laws of Motion. Recall. Forces a push or pull acting on an object; a vector quantity measured in Newtons (kg m/s²)

WEEKS 8-9 Dynamics of Machinery

Engineering Mechanics: Statics. Chapter 7: Virtual Work

K.GNANASEKARAN. M.E.,M.B.A.,(Ph.D)

PLANAR RIGID BODY MOTION: TRANSLATION & ROTATION

Lecture Outline Chapter 6. Physics, 4 th Edition James S. Walker. Copyright 2010 Pearson Education, Inc.

CEE 271: Applied Mechanics II, Dynamics Lecture 25: Ch.17, Sec.4-5

Deriving 1 DOF Equations of Motion Worked-Out Examples. MCE371: Vibrations. Prof. Richter. Department of Mechanical Engineering. Handout 3 Fall 2017

SCHEME OF BE 100 ENGINEERING MECHANICS DEC 2015

Statics deal with the condition of equilibrium of bodies acted upon by forces.

PROBLEM 16.4 SOLUTION

Rotational Motion About a Fixed Axis

Physics 8 Wednesday, October 25, 2017

Chapter 8 Lecture. Pearson Physics. Rotational Motion and Equilibrium. Prepared by Chris Chiaverina Pearson Education, Inc.

Chapter 8. Rotational Equilibrium and Rotational Dynamics

Chapter 9. Rotational Dynamics

KINGS COLLEGE OF ENGINEERING ENGINEERING MECHANICS QUESTION BANK UNIT I - PART-A

General Physics (PHY 2130)

Circular Motion, Pt 2: Angular Dynamics. Mr. Velazquez AP/Honors Physics

CHAPTER 1 INTRODUCTION

Torque and Rotation Lecture 7

Torques and Static Equilibrium

Transcription:

WEEK 1 Dynamics of Machinery References Theory of Machines and Mechanisms, J.J. Uicker, G.R.Pennock ve J.E. Shigley, 2003 Makine Dinamiği, Prof. Dr. Eres SÖYLEMEZ, 2013 Uygulamalı Makine Dinamiği, Jeremy Hirschhorn, Çeviri: Prof.Dr. Mustafa SABUNCU, 2014 1

Course Policy Two Midterms (20%) +Homework (10%) + 1 Final (50%) 2

A mechanism is a device which transforms motion to some desirable pattern and typically develops very low forces and transmits little power. A machine typically contains mechanisms which are designed to provide significant forces and transmit significant power Some examples of common mechanisms are a pencil sharpener, a camera shutter, an analog clock, a folding chair, an adjustable desk lamp, and an umbrella. Some examples of machines which possess motions similar to the mechanisms listed above are a food blender, a bank vault door, an automobile transmission, a bulldozer, and a robot. 3

Degree of freedom of a rigid body: The degree of freedom (DOF) of a rigid body is the number of independent parameters that define its configuration Six independent parameters are required to define the motion of the ship. An unrestrained rigid body in space has six degrees of freedom: three translating motions along the x, y and z axes and three rotary motions around the x, y and z axes respectively. Degree of freedom a kinematic pair: The degrees of freedom (DOF) of a kinemtaic pairs defined as the number of independent movements it has. 4

Theory of machines is separated into two section Dynamics is also separated into two section Statics: is that branch of theory of machines which deals with the forces and their effects, while the machine parts are rest. Dynamics: is that branch of theory of machines which deals with the forces and their effects, while acting upon the machine parts in motion. Kinematics: Kinematic analysis involves determination of position, displacement, rotation, speed, velocity, and acceleration of a mechanism. Kinetics: It is that branch of theory of machines which deals with the inertia forces which arise from the combined effect of the mass and motion of the machine parts. Kinetics analysis will be used for this lecture. 5

Newton's Three Laws of Motion: 6

F = ma m F = ma F + F = ma a = 1 2 F net m 7

Law 3: Reaction is always equal and opposite to action; that is to say, the actions of two bodies upon each other are always equal and directly opposite. 8

Rigid Body: is that body whose changes in shape are negligible compared with its overall dimensions or with the changes in position of the body as a whole, such as rigid link, rigid disc..etc. Links: are rigid bodies each having hinged holes or slot to be connected together by some means to constitute a mechanism which able to transmit motion or forces to some another locations. 9

FORCE AND MOMENT VECTORS A force is characterized by its magnitude and direction, and thus is a vector. In an (x, y)-plane the force vector, F, can be represented in different forms The characteristics of a force are its magnitude, its direction, and its point of application. The direction of a force includes the concept of a line along which the force is acting, and a sense. Thus a force may be directed either positively or negatively along its line of action. 10

Two equal and opposite forces along two parallel but noncollinear straight lines in a body cannot be combined to obtain a single resultant force on the body. Any two such forces acting on the body constitute a couple. The arm of the couple is the perpendicular distance between their lines of action, shown as h in the Figure, and the plane of the couple is the plane containing the two lines of action. M = R F =. A BA or M h F A or M = R F A BA M = R sin θ F= hf. A ( ) BA 11

FORCES IN MACHINE SYSTEMS A machine system is considered to be a system of an arbitrary group of bodies (links), which will be considered rigid. We are involved with different types of forces in such systems. a) Reaction Forces: are commonly called the joint forces in machine systems since the action and reaction between the bodies involved will be through the contacting kinematic elements of the links that form a joint. The joint forces are along the direction for which the degree-of-freedom is restricted. e.g. in constrained motion direction All lower pairs and their constraint forces: (a) revolute or turning pair with pair variable θ 12

(b) prismatic or sliding pair with pair variable z (c) cylindric pair with pair variables θ and z (d) screw or helical pair with pair variables θ and z 13

(e) planar or flat pair with pair variables x, z, and θ. (f) spheric pair with pair variables θ, φ and ψ 14

Reaction Forces 15

b) Physical Forces : As the physical forces acting on a rigid body we shall include external forces applied on the rigid body, the weight of the rigid body, driving force, or forces that are transmitted by bodies that are not rigid such as springs or strings attached to the rigid body. weight external forces Spring force 16

c) Friction or Resisting Force: The friction force is the force exerted by a surface as an object moves across it or makes an effort to move across it. F = R = ( ) µ F friction 32 32 F tan φ = µ = friction F µ: coefficient of friction 23 d) Inertia Forces are the forces due to the inertia of the rigid bodies involved. F i a F i F = ( ) i ma = ma m: mass, Kg a=acceleration, m/s 2 F=force, N 17

Inertia Torque i F = ma G T i = I α G m: mass, Kg a=acceleration, m/s 2 F=force, N T=Torque, Nm I= Moment of Inertia, kgm 2 18

We shall be using SI systems of units. A list of units relevant to the course is given below SI System of units 19

Moment of Inertia of a Mass For a body of mass m the resistance to rotation about the axis AA is I = = 2 2 2 1 m + r2 m + r3 m + 2 r r dm = mass moment of inertia The radius of gyration for a concentrated mass with equivalent mass moment of inertia is I k m k = = 2 Moment of inertia with respect to the y coordinate axis is 2 2 I y ( 2 ) z x = r dm = + dm Similarly, for the moment of inertia with respect to the x and z axes, ( 2 2 ) I = y + z dm In SI units, x 2 2 2 I = kg m I = x + y dm r dm = z ( ) I m ( 2 ) 20

Moments of Inertia of Common Geometric Shapes 21

FREE-BODY DIAGRAMS A free-body diagram is a sketch or drawing of the body, isolated from the rest of the machine and its surroundings, upon which the forces and moments are shown in action. A free body diagram shows all forces of all types acting on this body 22

Slider Crank Mechanism external force and torque, F 4 and T 2 All frictions are neglected except for the friction at joint 14 23

STATIC EQUILIBRIUM: A body is said to be in static equilibrium if under a set of applied forces and torques its translational (linear) and rotational accelerations are zeros (a body could be stationary or in motion with a constant linear velocity). Planar static equilibrium equations for a single body that is acted upon by forces and torques are expressed as F F = = 0 x Fy = 0 0 M z = M = 0 24

Two-force member: If only two forces act on a body that is in static equilibrium, the two forces are along the axis of the link, equal in magnitude, and opposite in direction.. If an element has pins or hinge supports at both ends and carries no load in-between, it is called a two-force member Two force and one moment member: A rigid body acted on by two forces and a moment is in static equilibrium only when the two forces form a couple whose moment is equal in magnitude but in opposite sense to the applied moment 25

Three-force member: If only three forces act on a body that is in static equilibrium, their axes intersect at a single point. A special case of the three-force member is when three forces meet at a pin joint that is connected between three links. When the system is in static equilibrium, the sum of the three forces must be equal to zero. For example, if the axes of two of the forces are known, the intersection of those two axes can assist us in determining the axis of the third force. 26

Let the force F A be completely specified. And the line of action of F B and the point of application of F C be known. When the moment equilibrium equation is written for the sum of moments about the point of intersection of the line of action of F A and F B (point O), since M O =0, the moment of F C about O must be zero, or the line of action of the force F C must pass through point O. The magnitudes of the forces can then be determined from the force and moment equilibrium equations. O their axes intersect at a single point. F = 0 27

Example: Find all the pin (joint) forces and the external torque M 12, that must be applied to link 2 of the mechanism (static). AO 2 =6 m, AB=18 m, BO 4 =12 m ve BQ=5 m GRAPHIC SOLUTION =120 N M 12 28

F 34 =33.1 N F 14 =89 N M 12 =183 N.m 29

ANALYTIC SOLUTION we sum moments about point O 4. Thus m m m m N N m m N N N N N 30

from the free-body diagram of link 2 m.n 31

Example: For the mechanism shown A 0 A= a 2 = 80, AB= a 3 =100, B 0 B= a 4 =120, A 0 B 0 = a 1 = 140, AC= b 3 = 70, BC=80 and B 0 D= b4=90 mm. When θ 12 =60 0, from kinematic analysis θ 13 =29,98 0, θ 14 = 96.40 0. Two forces F 13 =50 N < 230 0 and F 14 = 100 N < 200 0 are acting on links 3 and 4 respectively 32

The free-body diagrams of the moving links are shown (STATIC). 33

The three equilibrium equations for link 4 are: 34

There are four unknowns in three equations, therefore the equations obtained from one free-body diagram is not enough to solve for the unknowns. Equations 1 and 2 can be used to solve for G 14x and G 14y, only when F 34xy and F 34y are determined. The three equilibrium equations for link 3 must also be written (note that F 34 and F 43 are of equal magnitude). Where a= 52.62 0 (using the cosine theorem for the triangle ABC). 35

Equations 4 and 5 can be used to determine F 23x and F 23y Equations 3 and 6 must be used simultaneously to solve for F 34x and F 34y. Substituting the known values into equations 3 and 6 results: 36

37

38

39