mathcad - armare fundatie pe piloti franki
DESCRIPTION
Fundatie piloti - calcul armare pilotiTRANSCRIPT
n 8:=
Incarcari :
P 3500 150 n+( )kN:=
M 700 70 n+( )kN m:=
T 200 6 n+( )kN:=
P 4700kN=
M 1260kN m=
T 248kN=
Pilot cu sectiune rotunda:
ϕp_o 52cm:=
Stratificatia terenului de fundare:
Ic 0.28 0.01 n+:=
Ic 0.36=
Limita γ(kN/mc) E Ic1 1
02 -1
-33 -3
-94 -9
-50
0.36
Strat
200
40
300
Praf argilos
Nisip mediu indesat
17Umplutura
Argila Lc-0.7
Piloti Franki:
Riz Pv P1+= m1 1:= m2 m1:=
k 0.7:= m2 1=
Sfi..li 584.4166kNm
:=Aϕp_o
2 π
4:= U 2 π ϕp_o:=
pv 4000kN
m2:=
A 0.212 m2= U 3.267 m=
Riz k m1 pv A m2 U Sfi..li+( ):=
li_max 2m:=
Lp 15m:=
Strat Strat elementar Adancime Ic f.i fi*li PvII 1 2.5 0.7 32.5 16.25III 2 4 0.36 7.4 14.8III 3 6 0.36 8.9 17.8III 4 8 0.36 9.733 19.466IV 5 10 65 130IV 6 12 67.8 135.6IV 7 14 70.6 141.2IV 8 15.5 72.7 109.05
584.166 4000
Riz 1931.248 kN=σaδμ 100
daN
cm2:=Rb A σaδμ:=
Rb 2123.717 kN=
Riz Rb<
Calculul numarului de piloti si stabilirea dimensiunilor radierului:
np 4>
npc1.3PRiz
1pilot+:=
npc 4.164=
np 6piloti:=
tm 1.5 ϕp_o:=
tm 0.78 m=
tix. 4.5 ϕp_o:= tiy. 3 ϕp_o:=
tix. 2.34 m= tiy. 1.56 m=
x1 2.34- m:= x2 x1:=
x4 0:= x3 0:=
x6 2.32m:=
x5 x6:=
x1 2.34- m= x4 0=
x2 2.34- m= x5 2.32 m=
x3 0= x6 2.32 m=
L. 2 tm 2 tix.+:= B. 2 tm tiy.+:= L 6.3m:=
L. 6.24 m= B. 3.12 m= B 3.2m:=
H1. 0.35 L:= H2.H1.2
:=
H1. 2.205 m= H2. 1.102 m= H1 2.2m:= H2 1.1m:=
Stalpul are dimensiunile:
ϕp_o 0.52 m=
Calculul grupei de piloti:
Df 2.5m:= γµ 20kN
m3:=N P B L Df γµ+:=
N 5708 kN=
M0 M T Df+:= Sxi x12 x2
2+ x5
2+ x6
2+:=
np 6=M0 1880 kN m=
Sxi 21.716 m2=S1
N
np
M0 x1
Sxi+:=
S1 748.755 kN= S3N
np:= S4
N
np:=
S2N
np
M0 x2
Sxi+:= S3 951.333 kN=
S4 951.333 kN=
S2 748.755 kN=S6
N
np
M0 x6
Sxi+:=
S5N
np
M0 x5
Sxi+:=
S6 1152.181 kN=
S5 1152.181 kN=
S1 Smin> Smin 0:= mu 1:=
S6 Rg< Rg mu Riz:=Sor
T
np:= Sor 41.333 kN=
Rg 1931.248 kN=
Capacitatea portanta a pilotului izolat la solicitari orizoontale:
m 0.7:=
ϕ 16mm:=lo 4 ϕp_o:= lo 2.08 m=
Ra 300N
mm2:= A7ϕ16
7ϕ2 π4
:=
a 35mm:= A7ϕ16 1407.434 mm2=
Roriz m K Pu= A 0.212 m2=
Mcap 203kN m:=
Ro 0.7 0.7Mcap
lo:=
Ro 47.822 kN=
Sor Ro< aleg 7f16
Verificarea la solicitari axiale:
Ro 47.822 kN=
Sor 41.333 kN=
Sor Ro<
Verificarea la strapungere:
L 6.3 m= B 3.2 m=
H1 2.2 m= H2 1.1 m=
tm 0.78 m=
tix. 2.34 m=
tiy. 1.56 m=
U 3.267 m=Rt 0.9N
mm2:=
Hx 176.7cm:=
Si_cr Rt U Hx:=
ls 50cm:=Si_cr 5195.918 kN=
h0 210cm:= Pcr 2 h0 4 ls+:=
Sext S1 S2+ S5+ S6+:= Pcr 6.2 m=
Sext 3801.87 kN=
Siex Pcr Hx Rt 0.75:=
Siex 7394.895 kN=
Sext Siex< Sext Si.cr<
210
171,
7
171.5 171.5
630
320
Armarea radierului:
630
320
2
1
1Y
2
X
SECTIUNEA 1-1:
ϕ 22mm:=lx 237cm:=Mx 2 S6 lx:=ly 82cm:=My ly S1 S3+ S6+( ):= Aϕ22
ϕ2 π4
:=
Mx 5461.336 kN m=Aϕ22 380.133 mm2
=My 2338.86 kN m=
h0 2.1 m=
Aa_nec_xMx
0.85 h0 Ra:=
Aa_nec_x 10198.574 mm2=
Aaef 32 Aϕ22:=nr_bareϕ22 3bare:=
Aaef 12164.247 mm2=
Aleg 5f20/ml
ϕ 14mm:=
Aa_nec_yMy
0.85 h0 Ra:=
Aϕ14ϕ2 π
4:=
Aa_nec_y 4367.619 mm2= Aϕ14 153.938 mm2
=
Aa_nec_y 4367.619 mm2=
Aaef 32Aϕ14:=
Aaef 4926.017 mm2=nr_bareϕ14 32bare:=