compuerta radial

γ 15 Ubicación de BrazosB 2.45 ht 0.7H 1.7 hf 1.7h 1

ht/hf 0.4118 Ordenando

Wh 44.1Interpolacion para la ubicación de brazos (tabla 5,10)

α β γNMA 100.1 x1 0.4 0.4 0.4C 99.4 x0 0.4118 0.4118 0.4118V 99.4 x2 0.5 0.5 0.5 M´B =S 98.4 y1 0.179 0.5596 0.2614

y2 0.1858 0.5656 0.2486 Dividiendo entre 2,1568 y derivandoDm 0.7 x2 +2,2253x-1,862 = 0Ds 0 y0 0.1798 0.5603 0.2599 resolviendo la ecuacionDi 1 En radianes 0.16672768 0.51956897 0.24099857 X = 0,648 m

θ 0.92729522 M´B =R 1.25 θº 53.1299781Ds/R 0.00 1.159 mDi/R 0.80αs 0.0000 S1 0.208 m 9.55277006αi 0.9273 S2 0.649 m 29.7690393αsº 0.00 S3 0.301 m 13.8081688 SECCION DE LA VIGA VERTICAL

αiº 53.13 1.1591.5202 a 0.65

D(c -c) 0.28 0.95989412 b 0.650.58 γ 15 b/a 1.00

Rsencos/2 -0.30 B 2.45 a/2 0.320.5343 KN.m/m

Wv 25.70 0.5354 KN.m/m b1 100.00

h1 6.50Wtotal 51.04 A1 650.00

I1 2288.54Ω 0.5277 b2 6.50

Ωº 30.24 h2 200.00A2 1300.00I2 4333333.33

b3 130.00h3 6.50A3 845.00I3 2975.10

hDx2

hDS2x

(hA-hD)x3/(3S2)

(hA-hD)S2 x/3

(M´Á+ M´D)/2

S = θ * R MA

MD

MB

hA

hD

R(αi-αs)/2

M´Á

M´D

Esfuerzos en la bocina de articulacionA 0.0030190776

W 51044.54 t 0.11 τ 1538445.04925α 0.34906667 d 0.062 1.54Fn 9289.36997 L 0.012Fr 25522.2694 E 1.10E+11σ 3742268.24 δ 4.08E-07

3.74226824

μ 0.12 db 0.091Mm 145.662802 NmX 1.05W 6867Mp 7210.35Mv 85.64Mr 7672.9556R 1.25T 6138.36448Tc 3069.18224en kg 312.862614

CALCULO DE CARGAS EN VIGAS HORIZONTALES0.9598940.623414 x β1 16.43 0.290.287575 β2 12.94 0.230.121299 x

entre 2,15 23.31 KN2.15681 1.0000 29.44 KN

7.199206 3.3379 52.74 20º5.585347 x 2.5896 9.51 KN / m0.534835 KN.m/m 0.2480

12.02 KN / m2,1568 X3 +7,1992X2- 5,5860X +0,53484 12015.3728

a 0.575Dividiendo entre 2,1568 y derivando b 1.3x2 +2,2253x-1,862 = 0resolviendo la ecuacion -1.98629132 -1986.29132

0.6480.525369 KN.m/m 0.55195619 551.956189 N.m

525.369 N.m/m0.654477 KN.m 654.4768587 N.m -1.12E+07 -11.22 Mpa

0.65587 KN.m 655.8697205 N.m 0.000.643577 KN.m 643.5770338 N.m 3.12E+06 3.12 MPa

SECCION DE LA VIGA VERTICAL

CALCULO DE LA DEFORMACIONγ 0.2

Au 0.1298 E 2.00E+11f 6.76E-06 m

f 0.01 mm

A1+A2+A3 2795 B/750 3.27

Y1 3.25 f< B/750 0,07 < 3,67 CORRECTOY2 106.5Y3 209.75

Y 113.7034884 0.11370349

d1 110.4534884 σB 3.64E+06 Pad2 7.203488372 σB 3.64 Mpad3 96.04651163 σD 3.70E+06 Pa

I 2.01E+07 mm4 3.70 MPa

2.01E-05 m4

x2

x3

Ws Ws/2

x3 Wi Wi/2

x2

qs Rs

Ri

qi NS

Ni

MA = MB

MC

σA

σc

PaMpa

SELECCIÓN DEL PERFIL DE LOS BRAZOS

r1 1.03R 1.10M =L* Ni 5868.09

11.65 ω 1.1614.72 3.12E-02

0.35 A 2.47E-0312.4015.66 σ 7.53E+06

4.245.36

ESFUERZOS EN PANELESinf medio sup

Hm 1.426 1.095 0.642p 0.02139 0.016 0.010a 202 641.00 316b 800 800.00 800t 6.5 6.50 6.5c 0.206579 1.60 MPa 0.23b/a 3.960396 1.25 2.531646

Modulo inferior

c 0.207 0.207 0.207 0.207 0.207 0.207k 25 7.5 50 15 10.26 34.2

5.16 1.55 10.33 3.10 2.12 7.07

Mpa 5.46 10.78 7.38

Modulo central

c 1.60 1.60 1.60 1.60 1.60 1.60k 18.8 13.5 40.3 12.09 10.17 33.9

30.03 21.56 64.37 19.31 16.24 54.15

Mpa 30.74 67.21 56.53

Modulo superior

c 0.23 0.23 0.23 0.23 0.23 0.23k 25 8 50 15 10.29 34.3

5.69 1.82 11.38 3.41 2.34 7.81

Mpa 6.00 11.88 8.15

ωc

< 117,72 Mpa Correcto

σ1x σ1y σ3x σ3y σ4x σ4y

σ Mpa

σ1 σ3 σ4

σ1x σ1y σ3x σ3y σ4x σ4y

σ Mpa

σ1 σ3 σ4

σ1x σ1y σ3x σ3y σ4x σ4y

σ Mpa

σ1 σ3 σ4

6.6758 2.225266675.586 1.862

x2 4.951811747.448

12.39981173.52133664

raiz 0.64803499