reinforcement for plates

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Reinforcement for Plates Course CT4150 Lecture12 5 Jan. 2010

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Reinforcement for Plates . Course CT4150 Lecture12 5 Jan. 2010. Normal forces in concrete plates. Only rebars in the x and y directions Equilibrium of a plate part. Equations Design Choose q such that n s x + n sy is minimal (lower bound theorem). Solution. Example 1. - PowerPoint PPT Presentation

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Page 1: Reinforcement for Plates

Reinforcement for Plates

Course CT4150Lecture12

5 Jan. 2010

Page 2: Reinforcement for Plates

Normal forces in concrete plates

• Only rebars in the x and y directions• Equilibrium of a plate part

Page 3: Reinforcement for Plates

• Equations

• DesignChoose such that nsx+nsy is minimal

(lower bound theorem)

2cos

sin cos

xx sx c

yy sy c

xy c

n n n

n n n

n n

Page 4: Reinforcement for Plates

• Solution

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Example 1• Situationnxx=1200, nyy=-200, nxy=-400 kN/mfy = 500 N/mm², f’c= 30 N/mm²Thickness = 100 mm• Reinforcementnsx= 1200+400 = 1600 kN/mnsy= -200+400 = 200• Concretenc= -2x400 = -800 kN/m

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Asx=1600/500 = 3.20 mm = 3200 mm²/m

212–280 = 2/4x12²x1000/280 = 3231 OK

Asy=200/500 = 0.40 mm = 400 mm²/m

26–500 = 2/4x6²x1000/500 = 452 OK

c = 800/100 = 8 N/mm² < f’c OK

(safety factors omitted)

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Example 2• Deep beam 4.7x7.5 m, 2 supports, opening 1.5x1.5 m,

point load 3000 kN, fcd = 16.67 N/mm², fyd = 435 N/mm²

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• Forces nxx, nyy, nxy (linear elastic analysis)• Principal stresses

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• Reinforcement requirements (software)

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• Reinforcement (engineer)

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Moments in concrete plates• Only rebars in the x and y directions• Equilibrium of a plate part

• Result (Yield contour)2 min{( )( ), ( )( )}xy px xx py yy px xx py yym m m m m m m m m

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Example 3• Moments in a pointmxx = 13, myy = -8, mxy = 5 kNm/m• Moment capacitiesmpx = 17, mpy = 0, m’px =0, m’py = 10• Is the capacity sufficient?

• Yes

25 ?min{(17 13)(0 8), (0 13)(10 8)}25 ?min{32,26}

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Design of moment reinforcement

• Carry the moments with the least amount of reinforcement.

• So, minimize mpx+ mpy+ m’px+ m’py

• 5 constraints• mpx, mpy, m’px, m’py ≥ 0•

Solution 1 (Wood-Armer moments)•

• Crack direction 45º to the reinforcing bars

px xx xy px xx xy

py yy xy py yy xy

m m m m m m

m m m m m m

2 min{( )( ), ( )( )}xy px xx py yy px xx py yym m m m m m m m m

Page 16: Reinforcement for Plates

Solution 2 (when mpx would be < 0)

Solution 3 (when mpy would be < 0)2

0

xypx xx

yy

py

mm m

n

m

2

0px

xypy yy

xx

m

mm m

m

Page 17: Reinforcement for Plates

Solution 4 (when m’px would be < 0)

Solution 5 (when m’py would be < 0)

2

0px

xypy yy

xx

m

mm m

m

2

0

xypx xx

yy

py

mm m

m

m

Page 18: Reinforcement for Plates

Solution 6 (when mpx and mpy would be < 0)

Solution 7 (when m’px and m’py would be < 0)

0

0px

py

m

m

0

0px

py

m

m

Page 19: Reinforcement for Plates

Example 4• Moments in a point (as in example 1)mxx = 13, myy = -8, mxy = 5 kNm/m• Moment capacitiesmpx = 13+5²/8 = 16.13 m’px = 0mpy = 0 m’py = 8+5²/13 = 9.92• Amount of reinforcement is proportional to16.13+0+0+9.92 = 26• Amount of reinforcement in example 317+0+0+10 = 27 (larger, so not optimal)

Page 20: Reinforcement for Plates

Example 5

• Plate bridge, simply supported• 4 x 8 m, point load 80 kN, thick 0.25 m

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Example 5 continued

• Decomposition of the load

Page 22: Reinforcement for Plates

Example 5 Torsion moment

12

18 10 kNm/m

xy

xy

m a Va T

m F

xyV mxyV m

12T

12T

12

T Fa

x

Page 23: Reinforcement for Plates

Example 5 All moments

• Moments in the bridge middle

• Moments at the bridge support

14 1

2

18

240 kNm/m

0

10 kNm/m

xx

yy

xy

F am F

am

m F

18

00

10 kNm/m

xx

yy

xy

mm

m F

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Example 5 FEM moments

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Example 5 Reinforcement

Middle Support Designed

2

40 10 50 kNm/m 0 10 10 50

0 10 10 0 10 10 10

40 10 0 0 10 10 10

100 2.5 0 10 10 1040

px px px

py py py

px px px

py py py

m m m

m m m

m m m

m m m

Page 28: Reinforcement for Plates

Example 5 Upper bound check

Result> 1

OK

4 4 506 6 1.225 5 80pxF m

Page 29: Reinforcement for Plates

Computed requirements

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ConclusionsThe design procedure used is1 Compute the force flow linear elastically2 Choose the dimensions plastically

The reason for the linear elastic analysis in the firststep is that it shows us how an as yet imperfectdesign can be improved. A plastic (or nonlinear)analysis in step 1 would shows us how thestructure would collapse; but that is not what wewant to know in design.

This procedure is applied to design many types ofstructure for the ULS.