PRATT TRUSS AND EXAMPLE SOLUTION
A Pratt
truss includes vertical members and diagonals that slope down towards the
center, Pratt Truss similar to the Howe Truss just the opposite of the
Howe. The interior diagonals are under tension under balanced loading and
vertical elements under compression. If pure tension elements are used in the
diagonals then crossing elements may be needed near the center to accept
concentrated live loads as they traverse the span. It can be subdivided,
creating Y- and K-shaped patterns. The Pratt truss was invented in 1844 by
Thomas and Caleb Pratt. This truss is practical for use with spans up to
250 feet (76 m) and was a common configuration for railroad bridges as
truss bridges moved from wood to metal. They are statically
determinate bridges, which lend themselves well to long spans. They were
common in the United States between 1844 and the early 20th century.
This model is inspired by a classic bridge
type called a Pratt truss bridge. You can identify a Pratt truss by its
diagonal members, which (except for the very end ones) all slant down and in
toward the center of the span. All the diagonal members are subject to tension
forces only, while the shorter vertical members handle the compressive forces.
Since the tension removes the buckling risk, this allows for thinner diagonal
members resulting in a more economic design.
A truss structure supports only tension and
compression forces in its members and you would normally model it using bars,
but as this model uses 3D beams it also includes bending moments to some extent
in a frame structure. In the model, shell elements represent the roadway and
both the Shell and Beam interfaces are used.
Fundamentals
Write the equilibrium of forces along the x -axis.
∑Fx=0
Write the equilibrium of forces along
the y -axis.
∑Fy=0
Write the equilibrium of moments about
point A.
∑MA=0
Sign Convention for force: Upward and
right forces are positive.
Sign convention for moment: Anti clockwise
moment is positive and clockwise moment is negative.
Take moment about point E:
∑ME=0:
(Ey×0.60) − (5kNx0.30) =0
0.6Ey− 1.5kN=0
0.6Ey=1.5kN
Ey=1.5/0.6=2.5kN
Apply force equilibrium in x and y directions.
Ay+Ey− 5kN=0
Ay+2.5kN − 5kN=0
Ay=2.5kN
From the free body diagram of the entire
truss:
θ=tan -1(20/15)=53.13∘
FAH x sin53.13=2.5kN
FAH = 2.5kN / sin53.13
FAH = 3.125kN (COMPRESSION)
From simetric condition:
FFE x sin53.13=2.5kN
FFE = 2.5kN / sin53.13
FFE = 3.125kN (COMPRESSION)
To calculate FAB
FAB = FAH x cos53.13
FAB = 3.125 x cos53.13 (TENSION)
FAB = 1.875kN
From the simetric condition
FDE = FBC = FDC
= FHG = FGF = FAB
FDE = FBC = FDC
= FHG = FGF = 1.875kN
FDE , FBC , FDC ,FAB
(TENSION)
FHG , FGF (COMPRESSION)
From equilibrium conditions:
Ay− FHC x sin53.13=0
2.5kN− FHC x sin53.13=0
FHC x sin53.13=2.5kN
FHC = 2.5kN / sin53.13 =
3.125kN (TENSION)
from the simetric condition:
FFC = 3.125kN (TENSION)
FGC, FHB and FFD
= 0 (ZERO FORCE MEMBER)


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