Challenge

Roof Design

  • linken the class A surface using wave geometry linker .
  • offset the class A surface for 32 mm using offset surface.

  • extend the offset surface for 13mm using extend sheet.

  • law extend at the edges of the offset suface and class A surface by using law extension.

  • create datum plane at the edge of the class A surface at the distance of 80mm.
  • By using intersection curve create curve at the datum plane.

  • offset the surface for 6.5mm using offset in surface.

  • offset the intersection curve for 10mm using offset curve in face.

  • trim the surface with respect to offset curve in face.

  • then offset the surface for 4.5 mm using offset surface.

  • create the studio surface in between trimed surface  as shown in fig.

  • create the datum plane on surface and trim the surface with respect to datum plane as shown in fig.

  • create a sketch on law extenction os shown in fig .

  • provide the emboss to the sketch which is drawn on the above sketch as shown.
  • after emboss is created ,then blend the edges of emboss and edges of the surface.

  • extend the surface by the using extend sheet as shown in above fig.

  • then mirror the surface using mirror geometory.

  • first offset the class A surface for 6.5 mm,12mm,20mm using offset surface.

  • create the intersection curve on the class A surface and offset the curve 15mm,30mm,40mm,55mm,70mm by using offset in face.

  • trim the surface by using curves which as been created from offset in face and intersecting curve.

  • law extend the surface by using law extension .

  • trim the law extended surface and the timed surface using trim and extend.
  • face blend trimed surface using face blend.

  • offset the surface for 0.75+0.2mm using offset surface.

  • create the planes at the ends of the surface datum plane.
  • trim the offset surface which respect to datum plane using trim sheet.

  • offset the curve by using offset curve in face.

  • create the bridge curve from the lower surface to the upper surface.
  • create the surface between lower surface to upper surface by using studio surface.

  • mirror the final surface using mirror geometry and thicken the mirror surface using thicken .

          BOW - ROOF PREDUCTION FORMULA :-

W = [1.73 x 10^(-3) x L] + [1.85 x 10^(-8)  x (R^2)/t] + [ 1.10x10^(-3) x l] - 2.68   

L = 2033.9065mm

Rx = 200.2917mm

Ry = 201.7366mm

   R = 2(Rx*Ry)/(Rx+Ry)

R =2(200.2917* 201.7366)/(200.2917+201.7366)

R = 201.01155

t = 0.75 mm

I = 438.2321mm  FRONT ROOF RAIL TO BOW RAIL 1.

I = 352.2896mm BOW RAIL 1 TO CENTER RAIL.

I = 457.2952mm CENTR RAIL TO BOW RAIL 2.

I = 353.7589mm BOW RAIL 2 TO REAR ROOF RAIL.

W = [1.73 x 10^(-3) x L] + [1.85 x 10^(-8) x (R^2)/t] + [ 1.10x10^(-3) x l] - 2.68 FRONT ROOF RAIL TO BOW RAIL 1

W = (1.73 10^(-3)*2033.9065)+(1.8510^(-8) *(201.01155^2)/0.75)+(1.10*10^(-3)*438.2321)-2.68

W = 1.3217

 BOW RAIL 1 TO CENTER RAIL

W =1.2271

CENTER RAIL TO BOW RAIL 2

W = 1.3429

BOW RAIL 2 TO REAR ROOF RAIL

W = 1.2287

            SNOW LOAD PREDUCTION FORMULA :-

Qr =  [Iy x t2] / [α x s x [(Rx + Ry)/2]2 x 10-8]

t =0.75mm

LY = 1969.8472 mm

LX1 = 1137.802 mm BETWEEN FRONT ROOF RAIL AND BOW 1.

LX2 = 1089.3106 mm BETWEEN BOW 1 AND CENTER ROOF RAIL.

LX3 = 1062.3723 mm  BETWEEN CENTER ROOF RAIL AND BOW 2.

LX4 = 1047.7186 mm BETWEEN BOW 2 AND REAR ROOF RAIL .

Y1= 531.3619mm

Y2 = 961.094mm

Y3 = 1494.3579mm

Y4 = 1969.8479mm

CASE 1

L1 = 531.3619 mm 

L2 = 429.7327mm

CASE 2

L1 = 429.7327 mm

L2 =533.2632 mm

CASE 3

L1 =533.2632 mm

L2 =475.4893mm

RY1 = 2761.5317 mm      RX1 = 4423.4465 mm

RY2 = 6291.2933 mm      RX2 = 3773.6283 mm

RY3 = 11043.5828 mm    RX3 = 4272.8359mm

RY4 = 16489.2567mm     RX4 = 3989.9338mm

   s = L1/2 + L2/2

S1 = 531.3619/2+429.7327/2 =480.5473

S2 = 481.49795

S3 = 504.37625

My = Y(Ly-Y)

MY1 = 531.3619(1969.8472-531.3619)

MY1 = 764356.2821

MY2 = 969506.6480

MY3 = 710551.19182

MY4 = 0

α = My x Lx2 x 10-12

α1 = 764356.2821* 1137.802*1O-12

α1 = 0.0008696861

α2 = 0.0010560939

α3 = 0.0007548699

IY1 = 4.3064

Qr =  [Iy x t2] / [α x s x [(Rx + Ry)/2]2 x 10-8]

 Qr = [4.3064*0.752] /[0.0008696861*480.5473*[(4423.4465+2761.5317)/2]2 x 10-8]

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