Strength considerations for Power Screws|
The following notes are provided for general guidance. In practice power
screws are provided by specialist suppliers who provide technical literature which
includes all the necessary data for selecting power screws from their range.
The notes below are general in nature and cannot provide detailed information about precise
strength levels because there are limitations on the understanding of the stress levels in screws.
Calculations assume that loading is distributed along the whole length of the engaged screw.. In practice this
is not the case and the loading is actually mainly taken by the first two threads. These
may yield a little to distribute the load along the thread.
The stress levels are also effected by thread finish, clearance, shape,lubrication etc etc.
The following factors need to be considered in calculating the strength of a power screw
- Bearing Strength
- Bending Strength
- Shear Strength
- Direct tensile/compressive strength
- Direct tensile/compressive strength
- Column strength
σ B = Bearing stress ..N/m2|
σ b = Bending stress ..N/m2
σ c = Compressive stress ..N/m2
σ t = Tensile stress ..N/m2
σ co = compressive stress on concave side of column ..N/m2
τ = Shear stress ..N/m2
A = stress area ..m2
θ = Thread angle ...(radians)
b = width of screw thread at root
d m = Mean screw dia...(m)
d mc = Mean collar dia...(m)
d r = dia at the screw root ...(m)
d p = pitch dia of screw ...(m)
d o = Outside dia of the screw ..(m)
d t = dia used calculation of stress area = (d p +d r ) /2 ..(m)
E = Modulus of Elasticity ...(N /m2)
e = Load eccentricity for column calculation ..(m)|
h = Thread depth ..(m)
k = least radius of gyration = Sqrt(I/A)..(m)
L = factor for buckling loads for end support conditions
P = Column load ..(N)
l = lead of thread = n.p...(m)
n = number of threads in engagement.
p = pitch between adjacent threads... (m)
α = Helix /lead angle (radians) = tan-1 l/(π.dm ).
rm = Mean radius of thread (m)
W = Vertical force generated by screw-(N)
TR = Torque to raise load ...(Nm)
TL = Torque to lower load ...(Nm)
To = Overhaul torque resulting from load ...(Nm)
y = distance from centroid of screw to extreme fibre ..(m)
The bearing stress results from the crushing force between the screw surface and the adjacent
nut surface developed by lifting and supporting the load W.
σ B = W / ( π . dm. h.n )
Table of Safe Bearing Pressures
| Screw Mat|| Nut Mat|| Bearing Pressure|| Notes|
|Steel|| Bronze|| 17-24 N/mm2|| Low Speed|
|Steel|| Bronze|| 11-17 N/mm2|| 3 m/min|
|Steel|| Cast Iron||13-17 N/mm2|| 2,5m /min|
|Steel|| Bronze||5-10 N/mm2|| 6-12 m/min|
|Steel|| Cast Iron||7-7 N/mm2|| 6-12 m/min|
|Steel|| Bronze|| 1- 2 N/mm2|| 15 m/min|
The maximum bending stress occurs at the root of the thread. It is calculated
by assuming the thread is a simple cantilever beam built in at the root. The load is
assumed to act at mid point on the thread.
The maximumum stress is provided by the bending moment relationship M/I = σ /(y) =e/R. that is σ = M.y/I
The section under bending has a length = π.dm.n
The width of the section at the thread root = b.
The Moment of Inertia at the root I = π.dm.n.b3 /12
The distance from the centroid the the most remote fibre ..y = b/2.
The Bending Moment M = W.h/2
The maximum bending stress is therefore..
For an ISO metric screw thread b = 3p /4 ... for a square single start thread b = p /2
Both the nut and screw threads are subject to traverse shear stress resulting from
the bending forces. For a rectangular section the maximums shear stress
occurs at the neutral axis and equals
Screw...τ = 3.W /2.A = 3.W /(2.π.d r.n.b )
Nut...τ = 3.W /2.A = 3.W /(2.π.d o.n.b )
Tensile /Compressive stresses
A loaded power screw is subject to a direct tensile or compressive load.. This is simply calculated
as the load / tensile stress area.
The tensile stress area is generally provided in screw tables and is generally larger than
that calculated by the root dia. Using a stress area based on the root diameter may
be used for conservative design studies. (A = πdr2/4)
The preferred stress area is actually based on the (pitch dia + root dia)/2.. For ISO
metric screws this is illustrated at section Stress area -ISO 898
σ t or c = W /A...
A = π d t 2 / 4
d t = (dp + dr) /2
Based on maximum shear stress theory...
The shear stress τ caused by torque on the screw =
The value of the combined stress is therefore
This equation always applies when the screw is in tension. When a screw is in compression
and the length is greater than 8 time the root diameter then the buckling stress has to be considered..
Buckling stress..ref Simple Struts
When the screw is longer than 8 times the root diameter it must be considered a column.
Long columns with are dealt with using the Euler equation.
Columns with slenderness ratios of less than 100 are considered as short columns. The slenderness
ratio is the length (between supports) / Least radius of gyration of the section.
For Machine tool design a variation on the Gordon-Rankine formula is used. This is
called the Ritter equation ..
For a column the maximum stress at the concave side of the column
σ co should not exceed the design compressive strength of
the screw material..
K = factor to allow the column end supports
- One end fixed and one end free K= 0,25
- Both ends pin-connected K= 1
- One end pin-connected and one end fixed K= 2
- Both ends fixed K= 4
The above equation applies only the screws with purely axial loads.
When the load is eccentric from the screw centre line by distance e. Then
the following variation of the Ritter equation applies.