fundamentals of engineering supplied-reference handbook - Ventech!
fundamentals of engineering supplied-reference handbook - Ventech!
fundamentals of engineering supplied-reference handbook - Ventech!
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
The deflection θ and moment Fr are related by<br />
Fr = kθ<br />
where the spring rate k is given by<br />
4<br />
d E<br />
k =<br />
64DN<br />
where k has units <strong>of</strong> N·m/rad and θ is in radians.<br />
Spring Material: The strength <strong>of</strong> the spring wire may be<br />
found as shown in the section on linear springs. The<br />
allowable stress σ is then given by<br />
Sy = σ = 0.78Sut cold-drawn carbon steel (A227,<br />
A228, A229)<br />
Sy = σ = 0.87Sut hardened and tempered carbon<br />
and low-alloy steel (A232, A401)<br />
Ball/Roller Bearing Selection<br />
The minimum required basic load rating (load for which<br />
90% <strong>of</strong> the bearings from a given population will survive 1<br />
million revolutions) is given by<br />
1<br />
a<br />
C = PL , where<br />
C = minimum required basic load rating,<br />
P = design radial load,<br />
L = design life (in millions <strong>of</strong> revolutions), and<br />
a = 3 for ball bearings, 10/3 for roller bearings.<br />
When a ball bearing is subjected to both radial and axial<br />
loads, an equivalent radial load must be used in the<br />
equation above. The equivalent radial load is<br />
Peq = XVFr + YFa, where<br />
Peq = equivalent radial load,<br />
Fr = applied constant radial load, and<br />
Fa = applied constant axial (thrust) load.<br />
For radial contact, deep-groove ball bearings:<br />
V = 1 if inner ring rotating, 1.2 if outer ring rotating,<br />
If Fa /(VFr) > e,<br />
X = 0.<br />
56,<br />
where<br />
and<br />
⎛ Fa<br />
⎞<br />
e = 0.<br />
513⎜<br />
⎟<br />
⎜ C ⎟<br />
⎝ o ⎠<br />
⎛ Fa<br />
⎞<br />
Y = 0.<br />
840⎜<br />
⎟<br />
⎜ C ⎟<br />
⎝ o ⎠<br />
0.<br />
236<br />
,<br />
and<br />
−0.<br />
247<br />
Co = basic static load rating, from bearing catalog.<br />
If Fa /(VFr) ≤ e, X = 1 and Y = 0.<br />
204<br />
MECHANICAL ENGINEERING (continued)<br />
Intermediate- and Long-Length Columns<br />
The slenderness ratio <strong>of</strong> a column is Sr = l/k, where l is the<br />
length <strong>of</strong> the column and k is the radius <strong>of</strong> gyration. The<br />
radius <strong>of</strong> gyration <strong>of</strong> a column cross-section is, k = I A<br />
where I is the area moment <strong>of</strong> inertia and A is the crosssectional<br />
area <strong>of</strong> the column. A column is considered to be<br />
intermediate if its slenderness ratio is less than or equal to<br />
(Sr)D, where<br />
2E<br />
S<br />
( S ) = π , and<br />
r<br />
D<br />
y<br />
E = Young's modulus <strong>of</strong> respective member, and<br />
Sy = yield strength <strong>of</strong> the column material.<br />
For intermediate columns, the critical load is<br />
⎡<br />
2<br />
1 ⎛ S ⎤<br />
yS<br />
r ⎞<br />
P ⎢ ⎜ ⎟ ⎥<br />
cr = A S y −<br />
⎢<br />
⎜ ⎟<br />
, where<br />
E ⎥<br />
⎣ ⎝ 2π<br />
⎠ ⎦<br />
Pcr = critical buckling load,<br />
A = cross-sectional area <strong>of</strong> the column,<br />
Sy = yield strength <strong>of</strong> the column material,<br />
E = Young's modulus <strong>of</strong> respective member, and<br />
Sr = slenderness ratio.<br />
For long columns, the critical load is<br />
P<br />
cr<br />
2<br />
π EA<br />
=<br />
S<br />
2<br />
r<br />
where the variables are as defined above.<br />
For both intermediate and long columns, the effective<br />
column length depends on the end conditions. The AISC<br />
recommended values for the effective lengths <strong>of</strong> columns<br />
are, for: rounded-rounded or pinned-pinned ends, leff = l;<br />
fixed-free, leff = 2.1l; fixed-pinned, leff = 0.80l; fixed-fixed,<br />
leff = 0.65l. The effective column length should be used<br />
when calculating the slenderness ratio.<br />
Power Transmission<br />
Shafts and Axles<br />
Static Loading: The maximum shear stress and the von<br />
Mises stress may be calculated in terms <strong>of</strong> the loads from<br />
2<br />
2 2 1 2<br />
τ max = [ ( 8M<br />
+ Fd ) + ( 8T<br />
) ] ,<br />
3<br />
πd<br />
[ ( ) ] 2 1<br />
4<br />
2 2<br />
σ′ = 8M<br />
+ Fd + 48T<br />
, where<br />
3<br />
πd<br />
M = the bending moment,<br />
F = the axial load,<br />
T = the torque, and<br />
d = the diameter.