Assignment 2: «DESIGN OF SPRINGS»staff.fit.ac.cy/eng.la/AMEM317/Assig_2 springs(Example).pdf ·...
Transcript of Assignment 2: «DESIGN OF SPRINGS»staff.fit.ac.cy/eng.la/AMEM317/Assig_2 springs(Example).pdf ·...
PROGRAMME: «BSc in MECHANICAL ENGINEERING»
COURSE: Machine Elements I I - AMEM 317
ACADEMIC YEAR: 2010-11
INSTRUCTOR: Dr. Antonios Lontos
DATE: 06/05/2011
Assignment 2:
«DESIGN OF SPRINGS»
Prepared by:
Georgiou Georgios
Reg. Num.: 1010
NICOSIA - CYPRUS
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TABLE OF CONTENTS
Contents Assignment 2: ........................................................................................................... 1
1. INTRODUCTION AND INPUT DATA .............................................................. 3
1.1 TABLES................................................................................................... 6
2. GENERAL CALCULATIONS .......................................................................... 8
2.1 USEFUL DATA ........................................................................................ 8
2.2 NUMBER OF ACTIVE COILS (Na) .......................................................... 8
2.3 ESTIMATION OF SPRING WIRE DIAMETER ......................................... 8
2.4 ACTUAL SPRING RATE (K) .................................................................... 9
2.5 ACTUAL SPRING DEFLECTION (Yi) ..................................................... 9
2.6 ACTUAL SPRING FREE LENGTH (Lf) .................................................... 9
2.7 SPRING INDEX ....................................................................................... 9
2.8 SHEAR STRESS FACTOR (KB) .............................................................. 9
2.9 SPRING PITCH DIAMETER (P) .............................................................. 9
3. LOAD AT OPERATING AND AT SOLID LENGTH POSSITION ................... 10
3.1 SPRING LOADING AT OPERATING POSSITION ................................ 10
3.2 SPRING LOADING AT SOLID POSSITION .......................................... 10
4. TENSILE AND TORTIONAL YIELD STRENGTH OF WIRE ......................... 10
4.1 ULTIMATE TENSILE STRENGTH ......................................................... 10
4.2 TENSILE YIELD STRENGTH ................................................................ 10
4.3 TORTIONAL YIELD STRENGTH .......................................................... 10
5. GENERAL CALCULATION FOR DYNAMIC LOADING ................................ 11
5.1 FORCE Fa ............................................................................................. 11
5.2 MEAN FORCE Fm .................................................................................. 11
5.3 SHEAR STRESS AMPLITUDE (τa) ........................................................ 11
5.4 MIDRANGE SHEAR STRESS (τm) ........................................................ 11
5.5 LOAD LINE SLOPE ............................................................................... 11
6. SAFETY AGAINST FATIGUE USING GERBER CRITERION ...................... 12
6.1 ENDURANCE STRENGTH (Sse) ........................................................... 12
6.2 AMPLITUDE COMPONENT OF STRENGTH ........................................ 12
6.3 SAFETY FACTOR AGAINST FATIGUE ................................................ 12
7. THE SPRING CRITICAL FREQUENCY ....................................................... 13
7.1 CRITICAL FREQUENCY ....................................................................... 13
8. REFERANCES ............................................................................................. 14
9. DRAWINGS .................................................................................................. 14
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1. INTRODUCTION AND INPUT DATA Subject: AMEM 317 (AUTO 309) - Machine Elements and Analysis II Academic Year: 2014 (Spring Semester) Lecturer: Dr. Antonios Lontos ([email protected])
Assignment No. 2: Design of springs
Figure shows an old type of internal combustion engine and a new modification. The
position of the camshaft will change as well as all the other components related to
that part. A helical compression spring made of chrome-vanadium wire A232 will be
use in the new engine valve as shown in the figure. When the valve is closed the
compression load of the spring is (a) 70 N. The ends of the spring are square with (b)
5,5 total turns. At that position the installed length is (c) Li=63 mm. The operation
length is (d) Lo=49. mm.
A. Calculations
1. Calculate the proper spring for this valve. (Diameter of the wire, pitch diameter,
spring rate k). Calculate the load when is compressed at Lo and at solid length.
Calculate the stresses of the valve (cross section of stem) when spring is
operating at Li and Lo. Specify the valve material.
2. Estimate the tensile and torsional yield strength of the wire.
3. Estimate the factor of safety guarding against fatigue using Gerber criterion.
Determine the critical frequency of the spring.
B. Drawings and Assembly
1. Design the spring with all the dimensions. Design the spring in the unloading and
loading condition (when the spring length is Li and Lo).
2. Design the cross section of the engine in 2D
3. Design the spring with the valve in 3D and explain how they will assemble.
VERY IMPORTANT NOTES
* Estimate all dimensions that are not given.
* Useful documents: Cover for Assignment, Drawing template example
* You must submit one hard copy and one pdf file with all calculations and
drawings
* Example for the pdf file “Georgiou Georgios 6820 (Assignment 2)”
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Fig. 1: New configuration of the machine (Cross-section)
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Fig. 2: Old engine with components (Cross-section)
Fig. 3: valves and springs
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Fig. 4: Engine cross section
1.1 TABLES
7
8
2. GENERAL CALCULATIONS
2.1 USEFUL DATA Material: Chrome –Vanadium A232
Modulus of rigidity: G=77200 MPa
Constant A from table 10-4: A=2005 MPa.mmm
Exponent m from table 10-4: m=0.168 m
Ssa’= 241 MPa
Ssm= 379 MPa
Ssu= 0.67 sut
Spring End Type: Square
Total turns: Nt= 5.5
Compression load: F= 70 N
Installed length: Lf= 63 mm
Operating length: Lo= 49 mm
2.2 NUMBER OF ACTIVE COILS (Na)
Na = Nt – 2 = 5.5-2 = 3.5 turns
2.3 ESTIMATION OF SPRING WIRE DIAMETER We assume that the deflection during the installation is Yi=5mm. K = Fi / Yi = 70 / 5 = 14 N/mm The required diameter is given by :
√
√
d= 3.59mm from tables the nearest available wire diameter is 3.5mm
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2.4 ACTUAL SPRING RATE (K)
K = 12.6264 N/mm
2.5 ACTUAL SPRING DEFLECTION (Yi) K=Fi / Yi => Yi = Fi / K = 70 / 12.6264 Yi = 5.5 mm
2.6 ACTUAL SPRING FREE LENGTH (Lf) Lf = Li + Yi = 63+5.55 Lf = 68.55 mm
2.7 SPRING INDEX C = D / d = 32 / 3.5 = 9.14
2.8 SHEAR STRESS FACTOR (KB)
2.9 SPRING PITCH DIAMETER (P)
Due to the approximations and decimal places during the calculations we have error in P value. The real value due to design program SolidWork 2013 P = 11.82 mm
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3. LOAD AT OPERATING AND AT SOLID LENGTH POSSITION
3.1 SPRING LOADING AT OPERATING POSSITION YO = Lf – LO = 68.5 - 49 = 19.5 mm FMAX = K * YO = 12.6*19.5 = 245.7 N
3.2 SPRING LOADING AT SOLID POSSITION LS = d * (NT+1) = 3.5*(5.5+1) = 22.75 mm YS = LF – LC = 68.5 – 22.75 = 45.75 mm FSOLID = K*YS = 12.6 * 45.75 = 576.45 N
4. TENSILE AND TORTIONAL YIELD STRENGTH OF WIRE
4.1 ULTIMATE TENSILE STRENGTH SUT = A / dm = 2005 / 3.50.168 = 1624.5 MPa
4.2 TENSILE YIELD STRENGTH SSU = 0.67 * SUT = 0.67 * 1624.5 = 1088.4 MPa
4.3 TORTIONAL YIELD STRENGTH SSY = 0.45 * SUT = 0.45* 1624.5 = 731 MPa
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5. GENERAL CALCULATION FOR DYNAMIC LOADING
5.1 FORCE Fa Fa = FMAX – FMIN / 2 = 245.7-70 / 2 = 87.85 N
5.2 MEAN FORCE Fm Fm = FMAX + FMIN / 2 = 245.7 + 70 / 2 = 157.85 N
5.3 SHEAR STRESS AMPLITUDE (τa)
5.4 MIDRANGE SHEAR STRESS (τm)
5.5 LOAD LINE SLOPE
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6. SAFETY AGAINST FATIGUE USING GERBER CRITERION
6.1 ENDURANCE STRENGTH (Sse)
( )
( )
6.2 AMPLITUDE COMPONENT OF STRENGTH
[ √ (
)
]
[ √ (
)
]
Ssa = 233.47 MPa
6.3 SAFETY FACTOR AGAINST FATIGUE nf = Ssa / τa = 233.47 / 192 = 1.216
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7. THE SPRING CRITICAL FREQUENCY
7.1 CRITICAL FREQUENCY
CHANGES PER SECOND
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8. REFERANCES
[1] Mechanical Engineering Design, Ch. R. Mischke, J. Edward Shigley, McGraw-Hill, 7th edition, 2004.
[2] Fundamentals of Machine Elements, B. J. Hamrock, B. Jacobson, S. R. Scmid, Mcgraw-Hill, 1999
[3] Design of Machine Elements and Machines by Jack A. Collins, George H. Staab, Henry R. Busby, John Wiley & Sons, 2002
[4] Machine Design: An Integrated Approach by Robert L. Norton, Robert L Norton, Prentice Hall, 2nd edition, 2000
[5] Machine Elements in Mechanical Design by Robert L. Mott, Prentice Hall, 3rd edition, 1998
9. DRAWINGS
68,
50
35,50
28,50
3,50
FREE LENGTH
SPRING'S FREE LENGTHLf
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MATERIAL:
DATESIGNATURENAME
DEBUR AND BREAK SHARP EDGES
FINISH:UNLESS OTHERWISE SPECIFIED:DIMENSIONS ARE IN MILLIMETERSSURFACE FINISH:TOLERANCES: LINEAR: ANGULAR:
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35,50
28,50
3,50
INSTALLED LENGTH
SPRING'S INSTALLED LENGTH Li
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A3
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DATESIGNATURENAME
DEBUR AND BREAK SHARP EDGES
FINISH:UNLESS OTHERWISE SPECIFIED:DIMENSIONS ARE IN MILLIMETERSSURFACE FINISH:TOLERANCES: LINEAR: ANGULAR:
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49
28,50
35,50
3,50
OPERATING LENGTH
SPRING'S OPERATING LENGTH Lo
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A3
SHEET 1 OF 1SCALE:1: 2
DWG NO. 3
TITLE:
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MATERIAL:
DATESIGNATURENAME
DEBUR AND BREAK SHARP EDGES
FINISH:UNLESS OTHERWISE SPECIFIED:DIMENSIONS ARE IN MILLIMETERSSURFACE FINISH:TOLERANCES: LINEAR: ANGULAR:
58A/A
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40
15
2
2
CAP 45
5
R2
38
,50
16
20 20
10
GUIDE
R3
R9
6
18
12
5,83
6
5
SAFE 1,2
36
28
,50
11
5
4,50
10,82
15,86
RETAINER
36
28,50
11 130
5
10
104
,61
5
6
2,2
7
R1
R11,16
15,
39
6,67
VALVE
34
20
,79
10
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COMPONENTS3/5/14
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A3
SHEET 1 OF 1SCALE:1: 2
DWG NO. 4
TITLE:
REVISIONDO NOT SCALE DRAWING
MATERIAL:
DATESIGNATURENAME
DEBUR AND BREAK SHARP EDGES
FINISH:UNLESS OTHERWISE SPECIFIED:DIMENSIONS ARE IN MILLIMETERSSURFACE FINISH:TOLERANCES: LINEAR: ANGULAR:
58A/A
R.No. 8650Manolas George
40
15
2
2
CAP 45
5
R2
38
,50
16
20 20
10
GUIDE
R3
R9
6
18
12
5,83
6
5
SAFE 1,2
36
28
,50
11
5
4,50
10,82
15,86
RETAINER
36
28,50
11 130
5
10
104
,61
5
6
2,2
7
R1
R11,16
15,
39
6,67
VALVE
34
20
,79
10
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COMPONENTS 3D3/5/14
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A3
SHEET 1 OF 1SCALE:1: 2
DWG NO. 4.1
TITLE:
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MATERIAL:
DATESIGNATURENAME
DEBUR AND BREAK SHARP EDGES
FINISH:UNLESS OTHERWISE SPECIFIED:DIMENSIONS ARE IN MILLIMETERSSURFACE FINISH:TOLERANCES: LINEAR: ANGULAR:
58A/A
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ASSEMBLY 1 3/5/14
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A3
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MATERIAL:
DATESIGNATURENAME
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58A/A
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1435
6
8 7
ITEM NO. PART NUMBER DESCRIPTION QTY.1 body half hole2 1
2 valve 13 spring Li 1
4 guide 1
5 keeper 1 1
6 keeper 2 1
7 retainer cap 1
8 cap 1
ASSEMBLY 1 EXPOADED VIEW
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DATESIGNATURENAME
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FINISH:UNLESS OTHERWISE SPECIFIED:DIMENSIONS ARE IN MILLIMETERSSURFACE FINISH:TOLERANCES: LINEAR: ANGULAR:
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ASSEMBLY1 CROSS SECTION
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DATESIGNATURENAME
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engine cross section2D
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A3
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DWG NO. 8
TITLE:
REVISIONDO NOT SCALE DRAWING
MATERIAL:
DATESIGNATURENAME
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FINISH:UNLESS OTHERWISE SPECIFIED:DIMENSIONS ARE IN MILLIMETERSSURFACE FINISH:TOLERANCES: LINEAR: ANGULAR:
58A/A
R.No. 8650Manolas George