Static Unbalance. Both bearing reactions occur in the same plane and in the. After balancing no bearing reaction remains theoretically.

Similar documents
ME 6505 DYNAMICS OF MACHINES Fifth Semester Mechanical Engineering (Regulations 2013)

DYNAMICS OF MACHINES By. Dr.K.SRINIVASAN, Professor, AU-FRG Inst.for CAD/CAM, Anna University BALANCING OF RECIPROCATING MASSES

ME Machine Design I

Theory and Practice of Rotor Dynamics Prof. Dr. Rajiv Tiwari Department of Mechanical Engineering Indian Institute of Technology Guwahati

Balancing of Rotating Masses

This equation of motion may be solved either by differential equation method or by graphical method as discussed below:

UNIT 4 FLYWHEEL 4.1 INTRODUCTION 4.2 DYNAMICALLY EQUIVALENT SYSTEM. Structure. Objectives. 4.1 Introduction

WORK SHEET FOR MEP311

Dynamics of Machinery

[You will experience the effect of a centrifugal force if you swing a mass on the end of a piece of string around in a circle.]

Theory & Practice of Rotor Dynamics Prof. Rajiv Tiwari Department of Mechanical Engineering Indian Institute of Technology Guwahati

Dynamics of the Swash Plate Mechanism

TOPIC : 8 : Balancing

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

DYNAMICS OF MACHINERY

WEEKS 2-3 Dynamics of Machinery

18.12 FORCED-DAMPED VIBRATIONS

UNIT-I (FORCE ANALYSIS)

of the four-bar linkage shown in Figure 1 is T 12

Structural Dynamics Lecture 2. Outline of Lecture 2. Single-Degree-of-Freedom Systems (cont.)

Dynamics of Machines Prof. Amitabha Ghosh Department of Mechanical Engineering Indian Institute of Technology, Kanpur

WEEKS 8-9 Dynamics of Machinery

SAULT COLLEGE OF APPLIED ARTS AND TECHNOLOGY SAULT STE. MARIE, ONTARIO COURSE OUTLINE CODE NO. : MCH320 SEMESTER: FIVE.

ABSTRACT I. INTRODUCTION

20k rad/s and 2 10k rad/s,

Mitigation of Diesel Generator Vibrations in Nuclear Applications Antti Kangasperko. FSD3020xxx-x_01-00

ME Machine Design I. FINAL EXAM. OPEN BOOK AND CLOSED NOTES. Friday, May 8th, 2009

Mathematical Modeling and response analysis of mechanical systems are the subjects of this chapter.

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

Name: Fall 2014 CLOSED BOOK

ENGINEERING COUNCIL DYNAMICS OF MECHANICAL SYSTEMS D225 TUTORIAL 8 BALANCING OF ROTATING BODIES

7. FORCE ANALYSIS. Fundamentals F C

This, of course, is simply a restatement of Newton's law as discussed in Section 10.1 (p. 491).

COMPUTER-AIDED ANALYSIS OF BALANCING OF MULTI-CYLINDER INLINE AND V ENGINES

Equilibrium of rigid bodies Mehrdad Negahban (1999)

ME2302 DYNAMICS OF MACHINERY

DEPARTMENT OF MECHANICAL ENGINEERING Dynamics of Machinery. Submitted

Chapter 4 Statics and dynamics of rigid bodies

Mechanical vibration Rotor balancing. Part 2: Vocabulary. Vibrations mécaniques Équilibrage des rotors Partie 2: Vocabulaire. First edition

Mechanical Vibrations Prof. Rajiv Tiwari Department of Mechanical Engineering Indian Institute of Technology, Guwahati

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

MECHANISM AND MACHINE THEORY

Unit 15: Electrical, mechanical, hydraulic and pneumatic control LO1: The mechanical elements of a control system

Department of Mechanical Engineering ME6505- DYNAMICS OF MACHINES. Two Marks Question and answer UNIT I FORCE ANALYSIS AND FLYWHEELS

Inertia Forces in Reciprocating. Parts. 514 l Theory of Machines

KNIFE EDGE FLAT ROLLER

Dept.of Mechanical Engg, Defence Institute of Advanced Technology, Pune. India

PHY 001 (Physics I) Lecture 7

MECHANICAL ENGINEERING

The basic dynamic load rating C is a statistical number and it is based on 90% of the bearings surviving 50 km of travel carrying the full load.

Theory and Practice of Rotor Dynamics Prof. Rajiv Tiwari Department of Mechanical Engineering Indian Institute of Technology Guwahati

Chapter 3 Velocity Analysis

Kinematics, Dynamics, and Vibrations FE Review Session. Dr. David Herrin March 27, 2012

STATICS. Friction VECTOR MECHANICS FOR ENGINEERS: Eighth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr.

3.1 CONDITIONS FOR RIGID-BODY EQUILIBRIUM

E 490 FE Exam Prep. Engineering Mechanics

DESIGN & STATIC STRUCTURAL ANALYSIS OF CRANKSHAFT FOR HIGH PRESSURE PLUNGER PUMP

Misalignment Fault Detection in Dual-rotor System Based on Time Frequency Techniques

Dynamics of Machinery

Anna University May/June 2013 Exams ME2151 Engineering Mechanics Important Questions.

PROJECT 2 DYNAMICS OF MACHINES 41514

6. 3D Kinematics DE2-EA 2.1: M4DE. Dr Connor Myant

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

Use of Full Spectrum Cascade for Rotor Rub Identification

ME 301 THEORY OFD MACHİNES I SOLVED PROBLEM SET 2

Fig.1 Partially compliant eccentric slider crank linkage

The principle of the flywheel is found before the many centuries ago in spindle and the potter's wheel.

DYNAMIC ANALYSIS OF ROTOR-BEARING SYSTEM FOR FLEXIBLE BEARING SUPPORT CONDITION

Contact problems in rotor systems

Varuvan Vadivelan. Institute of Technology LAB MANUAL. : 2013 : B.E. MECHANICAL ENGINEERING : III Year / V Semester. Regulation Branch Year & Semester

DYNAMIC BALANCING OF ROTATING MACHINERY EXPERIMENT

Theory and Practice of Rotor Dynamics Prof. Rajiv Tiwari Department of Mechanical Engineering Indian Institute of Technology Guwahati

Computerized Analysis of Automobile Crankshaft with novel aspects of Inertial analysis

Modelling of lateral-torsional vibrations of the crank system with a damper of vibrations

RIGID BODY MOTION (Section 16.1)

Theory of Vibrations in Stewart Platforms

The University of Melbourne Engineering Mechanics

T1 T e c h n i c a l S e c t i o n

Inertia Forces in a Reciprocating Engine, Considering the Weight of Connecting Rod.

PLANAR KINETIC EQUATIONS OF MOTION (Section 17.2)

Towards Rotordynamic Analysis with COMSOL Multiphysics

Nonlinear effects on the rotor driven by a motor with limited power

C7047. PART A Answer all questions, each carries 5 marks.

Dynamics Qualifying Exam Sample

CHAPTER 6. Quality Assurance of Axial Mis-alignment (Bend and Twist) of Connecting Rod

UNIT 4 Balancing of Rotating Masses

Quiz No. 1: Tuesday Jan. 31. Assignment No. 2, due Thursday Feb 2: Problems 8.4, 8.13, 3.10, 3.28 Conceptual questions: 8.1, 3.6, 3.12, 3.

MOMENT OF A FORCE ABOUT A POINT

ENGINEERING MECHANICS: STATICS AND DYNAMICS

UNIT 2 KINEMATICS OF LINKAGE MECHANISMS

Precision Ball Screw/Spline

DYNAMICS VECTOR MECHANICS FOR ENGINEERS: Plane Motion of Rigid Bodies: Energy and Momentum Methods. Seventh Edition CHAPTER

Textbook Reference: Wilson, Buffa, Lou: Chapter 8 Glencoe Physics: Chapter 8

Chapter 8 Acceleration in Mechanisms

CHAPTER 6 FAULT DIAGNOSIS OF UNBALANCED CNC MACHINE SPINDLE USING VIBRATION SIGNATURES-A CASE STUDY

Robust shaft design to compensate deformation in the hub press fitting and disk clamping process of 2.5 HDDs

ME Machine Design I

Tuesday, February 11, Chapter 3. Load and Stress Analysis. Dr. Mohammad Suliman Abuhaiba, PE

Engineering Mechanics Statics

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

Transcription:

BALANCING

Static Unbalance A disk-shaft system on rigid rails An unbalanced disk-shaft system mounted on bearings and rotated For the unbalanced rotating system: Dynamic Bearing Reactions + Inertia Forces =0 -(F A + F B )i + mr G 2 i = 0 same direction. Balancing is performed on Both bearing reactions occur in the same plane and in the same direction. Balancing is performed on the plane of unbalance. After balancing no bearing reaction remains theoretically.

Dynamic Unbalance A long rotor mounted in bearings at A and B If m1=m2 and r1=r2 the rotor is statically balanced but dynamically unbalanced. Both bearing reactions occur in the same plane but in opposite directions. Balancing may be performed on the planes of unbalances or any other two convenient planes. After balancing, no bearing reactions remain theoretically.

Unbalance Types STATIC (Misalignment of axes) DYNAMIC (Tilt of axes) STATIC and DYNAMIC (GENERAL) (Called as DYNAMIC, in industry) (Both misalignment and tilt of axes)

Analysis of Static Unbalance F=0 m 1 R 1 2 + m 2 R 2 2 + m 3 R 3 2 + m c R c 2 =0 m c R c is the correction quantity. It is added to the plane of unbalances.

Analysis of Dynamic Unbalance Graphical Vectorial Scalar True moment polygon is 90 cw away

Industrial Balancing Machines

Balance Quality Grade Maximum Permissible Spesific Unbalance G M RA G. m. mr 2 r G Mr G 2 Mr G 2 =mr 2 Mr G =mr=u (Amont of Unbalance) r e=r G =mr/m=u/m (Spesific Unbalance) Empirically, e =constant G (Balance quality grade) (0.4-4000) For example: N=3000 rpm, G=6.3 give e=20 m as max permissible eccentiricity. Maximum Speed Permissible spesific unbalance (u/m) OR Mass center s eccentricity (e) 1) As the rotor mass increases permissible unbalance also increases (u=mr G ) 2) As the rotor speed increases permissible unbalance decreases (e =constant ) For small masses and high speeds, higher quality balance grade is required.

Balancing A Single-Cylinder Engine m A F C F = F A,B + F C Secondary component does not changed Primary component reduced 50% (Altough a new vertical component added) Eliminated

Polar Diagram of Inertia Forces Before adding m C : After adding m C :

Imaginary-Mass Approach 1) Two imaginary rotary masses are used for each reciprocating mass. 2) Each mass is equal to half the equivalent reciprocating mass. 3) These imaginary masses rotate about the crank center in opposite directions and with equal angular velocities. A simple model to analyse and recover the unbalance of reciprocating piston mass. 4) The total inertia force in y-direction is zero. 5) The inertia force in x-direction is equal to the inertia force due to reciprocating pisto mass.

Balance of Multicylinder Engines 2-Cylinder 2-Stroke Engine First Harmonics: Angles between imaginary masses : 360 /2 = 180 S 1 = 0 M 1 0

2-Cylinder 2-Stroke Engine Second Harmonics: Angles between imaginary masses: 720 /2 = 360 S 2 0 M 2 0

4-Cylinder 4-Stroke Engine Firing Order: 1-2-4-3 First Harmonics: Angles between imaginary masses : 720 /4 = 180 S 1 = 0 M 1 = 0

4-Cylinder 4-Stroke Engine Firing Order: 1-2-4-3 Second Harmonics: Angles between imaginary masses : 1440 /4 = 360 S 2 0 M 2 0

4-Cylinder 4-Stroke Engine Firing Order: 1-2-3-4 First Harmonics: Angles between imaginary masses : 720 /4 = 180 S 1 = 0 M 1 0

4-Cylinder 4-Stroke Engine Firing Order: 1-2-3-4 Second Harmonics: Angles between imaginary masses : 1440 /4 = 360 S 2 0 M 2 0

Balancing Linkages The position of the mass center of whole linkage, is tried to remain stationary.

Balancing Linkages (cont d) rs3 rs4 rs2 Vector loop-closure eq n: One of the vectors, for example may be drawn from this eq n: e.g.

Balancing Linkages (cont d) This eq n shows that the center of mass may be made stationary at the position, ( 1 and 3) if the following coefficients of the time-dependent terms vanish: r j 3 j r 4 4 j 3 0 m4a4e m3a3 e 0 r r j 2 2 m a e m r m a e 2 2 3 2 3 3 Simplification a e r a e 3 j 3 j 3 3 3 3 j 2 2 j 3 m2a2e m3a 3 e r3 3 r 0 These two equations must be satisfied for total force balance

Balancing Linkages (cont d) These equations yield the two sets of conditions: r4 and 3 r2 m and 2a2 m3a 3 2 r 3 3 A study of these conditions show that the mass and its location can be specified in advance for any single link (3); and then full balance can be obtained by rearranging the masses of the other two links (2 and 4). Without disturbing 3rd link, counterweights are added to rotating links 2 and 4. In this procedure, m a m a r 4 4 3 3 4 3 m a m a m a 0 0 0 * * * i i i i i i i i i relations must be satisfied. Unbalanced linkage Counterweight

Balancing Linkages (cont d) Therefore gives, * * 2 0 0 2 0 0 0 mi ai ( miai ) ( mi ai ) 2( miai )( mi ai ) cos( i i and tan * 1 i m a sin m a sin 0 0 0 i i i i i i 0 0 0 i i cos i mi ai cos i m a * m i If it is required to find, m m m * 0 i i i condition must be satisfied.