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fundamentals of engineering supplied-reference handbook - Ventech!

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Only the tangential component Wt transmits torque from<br />

one gear to another. Neglecting friction, the transmitted<br />

force may be found if either the transmitted torque or<br />

power is known:<br />

2T<br />

2T<br />

Wt = = ,<br />

d mN<br />

2H<br />

2H<br />

Wt = = , where<br />

dω<br />

mNω<br />

Wt = transmitted force (newton),<br />

T = torque on the gear (newton-mm),<br />

d = pitch diameter <strong>of</strong> the gear (mm),<br />

N = number <strong>of</strong> teeth on the gear,<br />

m = gear module (mm) (same for both gears in mesh),<br />

H = power (kW), and<br />

ω = speed <strong>of</strong> gear (rad/sec).<br />

Stresses in Spur Gears: Spur gears can fail in either<br />

bending (as a cantilever beam, near the root) or by surface<br />

fatigue due to contact stresses near the pitch circle. AGMA<br />

Standard 2001 gives equations for bending stress and<br />

surface stress. They are:<br />

Wt KaKm σ b =<br />

KK s BKI, bending and<br />

FmJ K<br />

v<br />

σ c = Cp Wt CaCm CsCf , surface stress , where<br />

FId Cv<br />

σb = bending stress,<br />

σc = surface stress,<br />

Wt = transmitted load,<br />

F = face width,<br />

m = module,<br />

J = bending strength geometry factor,<br />

Ka = application factor,<br />

KB = rim thickness factor,<br />

K1 = idler factor,<br />

Km = load distribution factor,<br />

Ks = size factor,<br />

Kv = dynamic factor,<br />

Cp = elastic coefficient,<br />

I = surface geometry factor,<br />

d = pitch diameter <strong>of</strong> gear being analyzed, and<br />

Cf = surface finish factor.<br />

Ca, Cm, Cs, and Cv are the same as Ka, Km, Ks, and Kv,<br />

respectively.<br />

Rigid Body Dynamics<br />

See DYNAMICS section.<br />

208<br />

MECHANICAL ENGINEERING (continued)<br />

Natural Frequency and Resonance<br />

See DYNAMICS section.<br />

Balancing <strong>of</strong> Rotating and Reciprocating<br />

Equipment<br />

Static (Single-plane) Balance<br />

n<br />

mbRbx = −∑<br />

miRix<br />

,<br />

n<br />

mbRby<br />

= −∑<br />

i=<br />

1<br />

i=<br />

1<br />

⎛ mbR<br />

θ = ⎜<br />

b arctan<br />

⎜<br />

⎝ mbR<br />

b<br />

b<br />

by<br />

bx<br />

⎞<br />

⎟<br />

⎠<br />

( ) ( ) 2<br />

2<br />

m R m R<br />

m R = +<br />

b<br />

bx<br />

b<br />

by<br />

m R<br />

where mb = balance mass<br />

Rb = radial distance to CG <strong>of</strong> balance mass<br />

mi = ith point mass<br />

Ri = radial distance to CG <strong>of</strong> the ith point mass<br />

θb = angle <strong>of</strong> rotation <strong>of</strong> balance mass CG with<br />

respect to a <strong>reference</strong> axis<br />

x,y = subscripts that designate orthogonal<br />

components<br />

Dynamic (Two-plane) Balance<br />

A<br />

B<br />

Two balance masses are added (or subtracted), one each<br />

on planes A and B.<br />

n<br />

n<br />

1<br />

1<br />

mBRBx = − miRixli<br />

mBRBy<br />

l ∑ , = −<br />

B<br />

l ∑<br />

i=<br />

1<br />

B i=<br />

1<br />

A<br />

n<br />

Ax = −∑<br />

i=1<br />

m R m R − m<br />

n<br />

Ay = −∑<br />

i=1<br />

m R m R − m<br />

A<br />

i<br />

i<br />

ix<br />

iy<br />

B<br />

B<br />

R<br />

R<br />

Bx<br />

By<br />

i<br />

iy<br />

m R<br />

i<br />

l<br />

iy i<br />

where<br />

mA = balance mass in the A plane<br />

mB = balance mass in the B plane<br />

RA = radial distance to CG <strong>of</strong> balance mass<br />

RB = radial distance to CG <strong>of</strong> balance mass<br />

and θA, θB, RA, and RB are found using the relationships<br />

given in Static Balance above.

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