outline the function(s) of springs · the function(s) of springs most fundamentally: ... **see...
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OutlineSpring Functions & TypesHelical Springs
CompressionExtensionTorsional
The Function(s) of Springs
Most fundamentally: to STORE ENERGY
Many springs can also: pushpulltwist
Some ReviewF
y
k
linear springs: k=F/y
nonlinear springs:dydFk =
Parallel
ktotal=k1+k2+k3
Series
321
1111kkkktotal
++=
Types of SpringsHelical:
Compression
Extension Torsion
More Springs
Washer Springs:
Beams:Power springs:
Helical Compression Springs
d diameter of wireD mean coil diameterLf free lengthp pitchNt Total coils
may also need:Do and Di
2
Length Terminology
Free Length AssembledLength
Max WorkingLoad
Bottomed Out
minimum of 10-15%clash allowance
Lf La Lm Ls
End ConditionsPlain
Square
Plain Ground
Square Ground
Na=Active Coils
F
F
F
F
Stresses in Helical SpringsSpring Index C=D/d
CCKwhere
d
FDK ss 212,8
3max+
==π
τ
FF
T
T
Curvature Stress
under static loading, local yielding eliminates stress concentration, so use Ks
under dynamic loading, failure happens below Sy: use Ks for mean, Kw for alternating
Inner part of spring is a stress concentration(see Chapter 4)
Kw includes both the direct shear factor and the stress concentration factor
CCCKwhere
d
FDK ww615.0
4414,8
3max +−−
==π
τ
Spring Deflection
Gd
NFDy a4
38≈
Spring Rate
Gd
NFDy a4
38≈
aND
Gdk 3
4
8≈
k=F/y
3
Helical SpringsCompression
NomenclatureStressDeflection and Spring ConstantStatic DesignFatigue Design
ExtensionTorsion
Static Spring DesignInherently iterative
Some values must be set to calculate stresses, deflections, etc.
Truly Designthere is not one “correct” answermust synthesize (a little bit) in addition to analyze
Material PropertiesSut ultimate tensile strength
Figure 13-3Table 13-4 with Sut=Adb
Sys torsional yield strengthTable 13-6 – a function of Sut and set
Spring/Material TreatmentsSetting
overstress material in same direction as applied load
» increase static load capacity 45-65%» increase energy storage by 100%
use Ks, not Kw (stress concentration relieved)Load Reversal with SpringsShot Peening
What type of failure would this be most effective against?
What are You Designing?Given
F, yk, y
Find
kF
Such that:Safety factor is > 1Spring will not buckleSpring will fit in hole, over pin, within vertical space
d, C, D*, Lf*, Na
*, clash allowance (α)**, material**
design variables
+
* - often can calculate from given** - often given/defined
Static Spring Flow Chart
STRESSES
Ns=Sys/τ
for shut spring if possibleif not, for max working load
if GIVEN F,y, then find k; If GIVEN k, y, then find F
D, Ks, Kw
material strengths
DEFLECTION
Lf, yshut, Fshut
Three things to know:• effect of d• shortcut to finding d• how to check buckling
ITERATE?
d, C
material
Na, α
CHECK
buckling, Nshut, Di, Do
Nshut=Sys/τshut
4
Static Design: Wire Diameter
Three things to know:• effect of d• shortcut to finding d• how to check buckling
3max8
dFDKsπ
τ =Gd
NFDy a4
38≈
**see Example 13-3A on Norton CD*maintain units (in. or mm) for A, b
use Table 13-2 to select standard d near calculated d
( ) ( ) ( )[ ] )2(115.08 b
minitialworks
AKFFCNd
+
⎭⎬⎫
⎩⎨⎧ −++
=π
αα
Based on Ns=Ssy/τ and above equation for τ:
Km=Sys/Sut
Buckling
f
workinginit
f
Lyy
y
DL
RS
+=′
=..
Three things to know:• effect of d• shortcut to finding d• how to check buckling
Helical SpringsCompression
NomenclatureStressDeflection and Spring ConstantStatic DesignFatigue Design
ExtensionTorsion
Material PropertiesSus ultimate shear strength
Sus≈0.67 Sut
Sfw´ torsional fatigue strengthTable 13-7 -- function of Sut, # of cyclesrepeated, room temp, 50% reliability, no corrosion
Sew´ torsional endurance limitfor steel, d < 10mmsee Eq. 13-12 (=45 ksi if unpeened, =67.5 ksi if peened)repeated, room temp., 50% reliability, no corrosion
Modified Goodman for SpringsSfw, Sew are for torsional strengths, so von Mises not used
0.5 Sfw
0.5 Sfw
τa
τm
Repea
ted
SfsC
B
Sus
A
( )fwus
usfwfs SS
SSS
5.05.0
−=
Fatigue Safety Factor
0.5 Sfw
0.5 Sfw
τa
τm
Sfs
Sus
load
line
Saτa
τi τm
mload
mgoodaa
fsSNτ
=
τa,load = τa,good at intersection( )
( ) ausimfs
iusfsfs SS
SSN
ττττ+−
−=
Eq. 13-17a
Fi=Fmin
Fa=(Fmax-Fmin)/2Fm=(Fmax+Fmin)/2
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What are you Designing?Given
Fmax,Fmin, ∆yk, ∆ y
Find
kF
Such that:Fatigue Safety Factor is > 1Shut Static Safety Factor is > 1Spring will not buckleSpring is well below natural frequencySpring will fit in hole, over pin, within vertical space
d, C, D*, Lf*, Na
*, clash allowance (α)**, material**
design variables
+
* - often can calculate from Given** - often given/defined
Fatigue Spring Design Strategy
d, C
if GIVEN F,y, then find k; If GIVEN k, y, then find F
Nshut=Sys/τshut
CHECKbuckling, frequency,Nshut, Di, Do
D, Ks, Kw
material strengths
DEFLECTION
Lf, yshut, Fshut
Two things to know:• shortcut to finding d• how to check frequency
ITERATE?
material
Na, α
STRESSES( )
( ) ausimfs
iusfsfs SS
SSN
ττττ+−
−=
Fatigue Design:Wire Diameteras before, you can iterate to find d, or you can use an equation
derived from relationships that we already know:
)2(1
min 134.11
67.08
b
awfw
bs
fs
fsms
fs FKSAdFK
NN
FKA
CNd
+
⎪⎭
⎪⎬⎫
⎪⎩
⎪⎨⎧
⎥⎥⎦
⎤
⎢⎢⎣
⎡⎟⎟⎠
⎞⎜⎜⎝
⎛−+
−−=
π
use Table 13-2 to select standard d near calculated d
Two things to know:• shortcut to finding d• how to check frequency
**see Example 13-4A on Norton CD*maintain units (in. or mm) for A, b
Natural Frequency: Surge
Two things to know:• shortcut to finding d• how to check frequency
Surge == longitudinal resonance
for fixed/fixed end conditions:
an W
kgf21
= (Hz)
ideally, fn will be at least 13x more than fforcing… it should definitely be multiple times bigger
Review of Design Strategy
Find LoadingSelect C, d
Find stressesDetermine material propertiesFind safety factor
Solve for d, pick standard dFind stressesDetermine material propertiesCheck safety factor
Find LoadingSelect C, safety factor
ITERATIVE USING d EQUATION
Strategy Review ContinuedFind spring constant, Na, Nt
Find FSHUT (must find lengths and y’s to do this)Find static shut shear stress and safety factor
Check Buckling
Check Surge
Check Di, Do if pin to fit over, hole to fit in
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Consider the Following: Helical SpringsCompression
NomenclatureStressDeflection and Spring ConstantStatic DesignFatigue Design
ExtensionTorsion
Extension SpringsAs before, 4 < C < 12
However, no peening, no setting,no concern about buckling
aws forKusedFDK τπ
τ ,83max =
surge check is same as before
Lb=d(Na+1)
Difference 1: Initial Force
deflection y
force F
Fi
“preloading”
F=Fi+kya
iND
Gdy
FFk 3
4
8=
−=
Difference 1a: Deflection
Gd
NDFFy ai4
3)(8 −≈
Difference 2: Initial Stress
take initial stress as the average stress between these lines, then find Fi
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Difference 3: Ends!: Bending
23416dF
dDFKba
ππσ +=
CdD
dRC
CCCC
Kb
===
−
−−=
222
)1(414
11
11
121
67.0
)()(
minmin
ese
altutmeaneute
fb
SS
SSSSN
=
+−−
=σσσ
σ
standardend
Difference 3a: Ends: Torsion
4414,8
22
3max 22 −−
==CCK
dFDK wwπ
τ
C2=2R2/d
pick a value >4
Materials
Sut – SameSys, Sfw, Sew – same for bodySys, Sfw, Sew – see Tables 13-10 and 13-11 for ends
Strategysimilar to compression + end stresses - buckling
Helical SpringsCompression
NomenclatureStressDeflection and Spring ConstantStatic DesignFatigue Design
ExtensionTorsion
Torsion Springs
• close-wound, always load to close
Deflection & Spring Rate
Ed
MDN
DNwireoflengthLEI
ML
aroundwirerev
aww
rev
4, 8.10
,21
=
===
θ
ππ
θ
rev
Mkθ
=
8
Stresses
Compressive is Max – Use for Static – Inside of Coil
3maxmax 32
max d
MKI
cMKii bbi
πσ ==
)1(414 2
−−−
=CC
CCKib
For Fatigue – Slightly lower Outside Tensile Stress – Outside of Coil
)1(414 2
+−+
=CC
CCKob
3max32
max d
MKobo
πσ =
3min32
min d
MKobo
πσ =
Materialssee Tables 13-13 and 13-14
follow book on Sewb=Sew/0.577
Strategy
M K
θ
• fit over pin (if there is one)• don’t exceed stresses
Select C, dHelical Springs
CompressionNomenclatureStressDeflection and Spring ConstantStatic DesignFatigue Design
ExtensionTorsion