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Crack control concrete

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 Cracking must be controlled and deflections must not be excessive  Cracks should not be unsightly or wide enough to lead to durability problems  Design for the serviceability limit

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Design Procedures

In order to satisfy the serviceability

limit states, a concrete structure must

be serviceable and perform to its

intended function throughout its

working life

Cracking must be controlled and

deflections must not be excessive

Cracks should not be unsightly or wide

enough to lead to durability problems

Design for the serviceability limit states

involves making reliable predictions of

the time dependent deformation and

cracking of the concrete structure

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The non-linear behaviour that complicates

serviceability calculations is due to

cracking, tension stiffening, creep and

shrinkage

Of these, Shrinkage is the most problematic

Shrinkage causes curvature on

non-symmetrically reinforced sections

Shrinkage causes time dependent

cracking; and

Shrinkage causes a reduction in tension

stiffening with time

All of these contribute to the long term

deflection and cracking of a RC member

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The width of a crack depends on:

The quantity, orientation and distribution of the reinforcing steel

crossing the crack

Concrete cover and member size

The bond between the concrete and reinforcement

The deformation properties of the concrete

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Crack Control

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Simplified Approach

For reinforced concrete beams and slabs, cracking is deemed to be

controlled (crack widths will be less than 0.3mm) if each of the

following is satisfied:

The quantity of the tensile reinforcement in a beam of slab

provides an ultimate limit strength at least 20% higher than the

cracking moment (with cs taken as 0)

The distance from the side of soffit of the member to the centre of the nearest longitudinal bar doesn’t exceed 100mm

The centre to centre spacing of bars near a tension face of a beam

or slab shall not exceed 300mm for a beam and the lesser of two

times the slab thickness and 300mm for a slab

The stress in the tensile steel is less than a limiting value

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Simplified Approach

For members subject primarily to flexure, the calculated steel stress

caused by the serviceability design moment shall not exceed the larger

of the maximum steel stresses given in Tables 8.6.2.2 & 9.5.2.1

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Simplified Approach

For members subject primarily to flexure, the calculated steel stress

caused by the serviceability design moment shall not exceed the larger

of the maximum steel stresses given in Tables 8.6.2.2 & 9.5.2.1

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AS3600 Refined Approach

The final crack width is the elongation of the tensile steel over the final crack spacing minus the extension of the concrete caused by the

induced load plus the shortening of the concrete between the cracks

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AS3600 Comparison to Experiments

Crack widths predictions at

~50-80% of ultimate load

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Tension Chord Model

13

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Tension Stiffening in SFRC/RC

Consider the response of 2 tension ties:

Cracking load remains about the same

Visibly reduced crack spacings and crack widths

Fibres can still be effective after yielding – but this

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Tension Chord Model - RC

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Tension Chord Model for SFRC

Tension carried across the cracks through the fibres

Consequently the strain in steel bars

is reduced

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Instantaneous Crack Widths

s c i

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Proposed SFRC Crack Width Model Results

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Time Dependent Crack Widths

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Time Dependent Crack Widths

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Time Dependent Crack Widths

st s

3 13 48

 =2fct for short term calcs

=1fct for long term calcs

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Design Example

Determine the maximum flexural crack width of a FRC member

subjected to a moment of 25.2kNm at t = 250 days The member has the following properties

cc

2 sc

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tc ct tc b

9.56 0.009 9.56 1 0.006 66.6 mm

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tc ct tc b

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250 66.6

9.56 462 205 66.6 9.56 1 307 66.6 45 3

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250 66.6

9.56 462 205 66.6 9.56 1 307 66.6 45 3

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Design Example

Step 6: Due to reduction in Tension Stiffening

Step 7: Combined Curvature

Step 8: Calculate crack width

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Concluding Remarks

Provisions for the calculation of flexural crack widths are available in

AS3600

Available models are typically built off the tension chord model

These models can be readily extended to account for the presence of

fibre reinforcement – ongoing research at USYD

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