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Critical load of a tower – a buckling problem<br />

Slender structural elements under pressure can fail due to<br />

buckling. This means the system is not able to undo<br />

unintentional deflections from a certain pressure load, but<br />

the deflection is continuously increasing which means that<br />

the system is failing. The load because of which this critical<br />

state can occur is called critical load or limit load.<br />

The load state of a tower under critical load can be<br />

visualized by the following analogy:<br />

If the existing load is lower than the critical load<br />

the tower behaves like a ball in a bowl. If the ball<br />

is moved it always rolls back to the middle of the<br />

bowl by itself. This is called a stable system.<br />

If the existing load is higher than the critical load<br />

the tower behaves like a ball on a bowl that is turned<br />

upside down. As soon as it is moved only<br />

some millimeters the ball drops. This is called an<br />

instable system.<br />

In this context the tower can be regarded as free standing<br />

column with bending resistant connection to the basement<br />

(exception: inclined or braced towers) and the critical load<br />

can be determined with Euler’s formula:<br />

Fk = π x EI / (2 x H)²<br />

Decisive for the size of the critical load are the stiffness of<br />

the trusses (EI) and the height of tower (H). The stiffer and<br />

lower the tower is the higher is the critical load and thus the<br />

higher the tower can be loaded. Referring to 4-point-trusses<br />

it can be said further:<br />

The permissible pay load declines quadratically with the<br />

height (twice the height => 1/4 pay load)<br />

The pay load rises quadratically with the axial distance of<br />

the mainchords (twice the axial distance => quadrupled<br />

pay load)<br />

The pay load rises linearly with the cross section area of the<br />

mainchords (twice the area => twice the pay load)<br />

The following chart shows the critical loads for different<br />

tower heights for some common trusses (calculation see<br />

example): the critical load applies to towers with central loading<br />

without horizontal loads; for the calculations a safety<br />

of 2.5 is taken into account. Eccentric loads and wind loads<br />

lead to further reduction of the permissible load.<br />

Please note again, this is a simplified calculation.<br />

For a more precise verification further points need to be<br />

taken into account:<br />

- Bending resistant connection to a weak basement<br />

(in this case the critical load declines even more, which<br />

means the permissible pay load also declines)<br />

- If the load is not suspended directly at the tower but<br />

lifted with a pulley the pressure load on the tower is<br />

doubled which means the permissible pay load is halved.<br />

- A dynamic increase of lifting or lowering the pay load<br />

should be taken into account by a load increase of<br />

20 – 40%.<br />

- For inclined towers or towers with cantilevered loads the<br />

critical load is diminished due to the additional bending<br />

stress. In this case a more detailed calculation is<br />

necessary.<br />

Example: Determination of the critical<br />

load according to Euler<br />

Tower H = 10 m of square aluminium trusses<br />

with main chords 50 x 4 center distance 47 cm<br />

critical load according<br />

to Euler:<br />

Fk = \pi x E x I / (2 x H)²<br />

with \pi = circuit number = 3,14<br />

E = E = E modulus of aluminium = 7.000 kN/cm²<br />

I = A chord x e² = 5,78 cm² x 47² = 12768 cm 4<br />

H= height tower = 10 m = 1000 cm<br />

permissible load F with safety = 2,5<br />

I = area moment of inertia 2. degree<br />

for square trusses:<br />

I = cross section area main chord<br />

multiplied by the square of center distance<br />

F < Fk / 2,5 = 3,14 x 7.000 x 12768 / (2,5 x 2000²)<br />

= 28,1kN = 2,81 t<br />

PA-TOWER<br />

main chords center distance I buckling load in [kN] bucklingd with safety of 2.5<br />

main chords<br />

at H in [m]<br />

[cm] [cm 2 ] 5,0 7,5 10,0 12,5<br />

50 x 2,0 24 1737 15,3 6,8 3,8 2,4<br />

48 x 4,5 30 5535 48,7 21,6 12,2 7,8<br />

50 x 4,0 47 12769 112,3 49,9 28,1 18,0<br />

48 x 4,5 57 19980 175,8 78,1 43,9 28,1<br />

Further informationen of the autors:<br />

www.krasenbrink-bastians.de, www.vom-felde.de<br />

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