Chapter 5 Design and Analysis of a Laminate The Drive Shaft Problem Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa,

Slides:



Advertisements
Similar presentations
Chapter 4 Macromechanical Analysis of a Laminate Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa, FL Courtesy.
Advertisements

FRC Robot Mechanical Principles
PROBLEM-1 The pipe shown in the figure has an inner diameter of 80 mm and an outer diameter of 100 mm. If its end is tightened against the support at A.
Chp12- Footings.
Principle Stresses Under a Given Loading
PACE Collaborative Project: Emerging Market Vehicle Transmission Design Team member: Anthony Smith Kevin Scott Decorian Harris Jacque Thornton Advisor:
Power Transmission Shaft Irmydel Lugo Victor Molina Eladio Pereira.
Torsion: Shear Stress & Twist ( )
Methods of Attaching Components to a Shaft
Chapter 5 – Torsion Figure: 05-00CO.
Chapter 18 Shafts and Axles Dr. A. Aziz Bazoune
Strength of Material-5 Torsion Dr. Attaullah Shah.
CTC / MTC 222 Strength of Materials Chapter 5 Torsional Shear Stress and Torsional Deformation.
Power Transmission Fundamentals Terminology. Gear System Characteristics Gears are used to reduce the speed by a known ratio. Reducing the speed increases.
CTC / MTC 222 Strength of Materials
Resistance Forces on A Vehicle P M V Subbarao Professor Mechanical Engineering Department Estimation of Vehicle Demands ….
Flywheel Selection Need flywheel to simulate inertia of bus to model exactly how bus will react Option to manufacture our own flywheel or use existing.
L ESSON 5: M ECHANICS FOR M OTORS AND G ENERATORS ET 332a Dc Motors, Generators and Energy Conversion Devices 1.
CLARKSON UNIVERSITY Department of Mechanical and Aeronautical Engineering Introduction to AIRCRAFT STRUCTURES Ratan Jha (CAMP 364, ,
Chapter 4 Macromechanical Analysis of a Laminate Hygrothermal Loads Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa,
Chapter 4 Macromechanical Analysis of a Laminate Laminate Analysis: Example Dr. Autar Kaw Department of Mechanical Engineering University of South Florida,
Chapter 4 Macromechanical Analysis of a Laminate Objectives and Laminate Code Dr. Autar Kaw Department of Mechanical Engineering University of South Florida,
EML 4230 Introduction to Composite Materials
Engineering Analysis Presentation ME 4182 Team: 5 Guys Engineering + 1 Nathan Bessette, Rahul Bhatia, Andrew Cass, Zeeshan Saiyed, Glen Stewart YJ Chok.
 If you don't let a teacher know at what level you are - by asking a question, or revealing your ignorance - you will not learn or grow. You can't pretend.
Section 6 Newton’s 2nd Law:
Chapter 3 Micromechanical Analysis of a Lamina Ultimate Strengths of a Unidirectional Lamina Dr. Autar Kaw Department of Mechanical Engineering University.
Vehicle Dynamics Example Problems
Chapter 3 Micromechanical Analysis of a Lamina Elastic Moduli Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa, FL.
CoG and Speeding Building SPEED July 28, July-2011 Center of Gravity The Center of Gravity is the point where the object/figure balances Geometry.
Chapter 3 Micromechanical Analysis of a Lamina Coefficients of Thermal Expansion Dr. Autar Kaw Department of Mechanical Engineering University of South.
Problem Statement A drive shaft for a Chevy Pickup truck is made of steel. Check whether replacing it with a drive shaft made of composite materials will.
Problem Statement An automobile drive shaft is made of steel. Check whether replacing it with a drive shaft made of composite materials will save weight?
Chapter 5 Design and Analysis of a Laminate The Drive Shaft Problem Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa,
UNIT-05. Torsion And Buckling of columns
EML 4230 Introduction to Composite Materials
EML 4230 Introduction to Composite Materials
PROBLEM-1 The pipe shown in the figure has an inner diameter of 80 mm and an outer diameter of 100 mm. If its end is tightened against the support at A.
Chapter 2 Macromechanical Analysis of a Lamina 2D Stiffness and Compliance Matrix for Unidirectional Lamina Dr. Autar Kaw Department of Mechanical Engineering.
Machine Design - II ME 441 Lecture 6-2: Flexible Mechanical Elements Belts, Ropes and Chains Chapter 17 Dr. Mohammad A. Irfan Oct 12, Zul Hajj.
Chapter 3 Micromechanical Analysis of a Lamina Volume Fractions, Weight Fractions, Density, and Void Content Dr. Autar Kaw Department of Mechanical Engineering.
Innovative Rocking Chair Design with Electro-Magnetically Induced Rocking Motion Jorge Alvarado-Colón Yocli Comas-Torres Andrés Cruz-Vélez Tamarys Heredia-Arroyo.
Sci 701 Unit 5 Speed is a measure of how fast an object is moving, that is, how much distance it will travel over a given time. This measure is given.
EML 4230 Introduction to Composite Materials
EML 4230 Introduction to Composite Materials
Chapter 2 Macromechanical Analysis of a Lamina Tsai-Hill Failure Theory Dr. Autar Kaw Department of Mechanical Engineering University of South Florida,
1 - An AISI 1020 cold- rolled steel tube has an OD of 3.0 inch. The internal pressure in the tube is 6,840 psi. Determine the thickness of the tube using.
Chapter 2 Macromechanical Analysis of a Lamina Review of Definitions Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa,
Chapter 2 Macromechanical Analysis of a Lamina Maximum Stress Failure Theory Dr. Autar Kaw Department of Mechanical Engineering University of South Florida,
Chapter 3.
Power Transmission Shaft
EML 4230 Introduction to Composite Materials
Design of a Transmission Shaft
EML 4230 Introduction to Composite Materials
SAE Mini Baja: Powertrain
EML 4230 Introduction to Composite Materials
Mechanical Properties of Materials
design and optimization of a composite drive shaft for an automobile
Gears and Transmissions
Pulleys, Sprockets, and Gears
Pulleys, Sprockets & Gears
Powertrains Erin Choi Ffff.
SAE Mini Baja: Powertrain
EML 4230 Introduction to Composite Materials
Chapter 2 BELTING SYSTEM.
EML 4230 Introduction to Composite Materials
EML 4230 Introduction to Composite Materials
EML 4230 Introduction to Composite Materials
EML 4230 Introduction to Composite Materials
EML 4230 Introduction to Composite Materials
Presentation transcript:

Chapter 5 Design and Analysis of a Laminate The Drive Shaft Problem Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa, FL Courtesy of the Textbook Mechanics of Composite Materials by Kaw

A drive shaft for a Chevy Pickup truck is made of steel. Check whether replacing it with a drive shaft made of composite materials will save weight?

 Light weight ___ reduces energy consumption; increases amount of power transmitted to the wheels. About 17-22% of engine power is lost to rotating the mass of the drive train.  Fatigue resistant ___ durable life.  Non-corrosive ___ reduced maintenance cost and increased life.  Single piece ___ reduces manufacturing cost.

 Prevent injuries – the composite drive shaft “broom” on failure

Design Constraints 1. Maximum horsepower= 175 rpm 2. Maximum torque = 265 rpm 3. Factor of safety = 3 3. Outside radius = 1.75 in 4. Length = 43.5 in

In first gear - the speed is 2800 rpm (46.67 rev/s) - assume ground speed of 23 mph (405 in/sec) Diameter of tire = 27 in Revolutions of tire =405/[π(27)] = 4.78 rev/s Differential ratio = 3.42 Drive shaft speed = 4.78 x 3.42 = rev/s Torque in drive shaft = (265x46.7)/16.35 = 755 lb-ft

Maximum Speed = 100 mph (1760 in/sec) Diameter of tire = 27 in Revolutions of tire =1760/[π(27)] = rev/s Differential ratio = 3.42 Drive shaft speed = 20.74x3.42 = 71Hz

 Torque Resistance.  Should carry load without failure  Not rotate close to natural frequency.  Need high natural frequency otherwise whirling may take place  Buckling Resistance.  May buckle before failing

Shear Strength,  max = 25 Ksi Torque, T = 755 lb-ft Factor of Safety, FS = 3 Outer Radius, c = 1.75 in Polar moment of area, J = c in = 1.69 in t = = 0.06 in = 1/16 in

f n = Acceleration due to gravity, g= 32.2 ft/s 2 Young’s modulus, E = 30 Msi Weight per unit length, W = lbf/in Length, L = 43.5 in Second Moment of Area, I = f n = 204 Hz Meets minimum of 71.1Hz

T= Mean radius, r m = in Thickness, t = 1/16 in Young’s modulus, E = 30 Msi Critical Buckling Load, T = 5519 lb-ft Meets minimum of 755 lb-ft

N xy = (Why) T = 755 lb-ft r = 1.75 in N xy = lb / in Neglecting centrifugal force contribution

Inputs to PROMAL: Glass/Epoxy from Table 2.1 Lamina Thickness = in Stacking Sequence: (45/-45/45/-45/45) s Load N xy = lb / in Outputs of PROMAL: Smallest Strength Ratio = 1.52 (not safe) Thickness of Laminate: h = *10 = in

f n = g = 32.2 ft/s 2 E x = Msi I = in 4 W = lbf/in L = 43.5 in Hence f n = Hz (meets minimum 71.1 Hz)

T = r m = /2= in t = in E x = Msi E y = Msi T = 183 lb-ft (does not meet 755 lb-ft torque)