Challenge

Roof Design

Objective:

To design a roof for an automobile with given master sections and satisfy the roof curvature analysis for Heat distortion and Snow Load criteria.

Design Considerations:

  • Headroom clearance
  • Bow roof position
  • Heat distortion and Snow load criteria
  • Draft analysis

Input:

Styling:

Final Design:

Roof Outer Panel with Ditch:

Front Roof Rail: Added Embosses for improved material properties.

Rear Roof Rail: Added Embossing and Darts (Stiffener) fro improved material properties.

Bow Roofs on either side of the Center roof rail:

The bow roofs and the center roof rail will be spot-welded onto the side flanges and/or the pillars from the BiW, while they will be attached to the roof outer using mastics. The front and rear roof rails will also be attached to the outer roof with mastics (sealant).

Curvature Analysis:

Heat Distortion:

This analysis aims to study the deflection of roofs in high-temperature conditions. This is predicted by calculating:

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

Where,

L = Roof Length in X-Direction[mm](Roof dimension in 0-Y)

R = Roof curvature

R = 2(Rx*Ry)/(Rx+Ry)

Rx = X curvature

Ry = Y curvature

t = Roof plate thickness [mm]

l = Bow Roof Span [mm];

The acceptable maximum value for W is 2.7.

Results:

HEAT DISTORTION
Roof Section Rx Ry Rx*Ry Rx+Ry R L t I W Status
Front - Bow 1 5726 2738 15677788 8464 3704.581 2029 0.75 462 1.676893 OK
Bow 1 - Center 4837 6742 32611054 11579 5632.793 2029 0.75 390 2.041803 OK
Center - Bow 2 3960 10672 42261120 14632 5776.534 2029 0.75 370 2.060256 OK
Bow 2 - Rear 3260 14719 47983940 17979 5337.776 2029 0.75 391 1.963069 OK

Snow Load:

This analysis aims to understand the deflection of the roof when a load is applied on top of it. This is predicted by calculating:

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

Note: The Qr value given over here is correct. There was a typo error in the formula given in the video.

Where,

α = My x Lx2 x 10-12 , My = Y(Ly-Y)

t = Roof plate thickness [mm]

Ly = Distance between the front and rear roof Rails on the Vehicle along with 0Y[mm]

Length of Roof panel with the center point between Roof rail Front /Rear as the front and rear reference point.

Lx = Distance between the Left and Right end of the roof on the Roof BOW [mm]

The width of the roof panel is exposed on the surface.

Y = Distance front Front Roof Rail to Roof BOW[mm]

s = Distance for which Roof BOW bears divided load [mm]

s = L1/2 + L2/2

Iy = Geometrical moment of inertia of Roof BOW (Y cross-section )[mm4]

Rx = Lateral direction curvature radius of roof panel Y cross-section on Roof BOW [mm]

Roof panel curvature Radius of the Length Lx in Front view

Ry = Longitudinal Direction curvature radius of the Roof panel X cross-section on Roof BOW [mm]

Roof panel X curvature radius of length s in Side view;

The minimum acceptable Qr value is 3.1 when the value of 's' ranges between 20 and 380.

Results:

SNOW LOAD
Roof Section Iy Lx Ly L1 L2 Rx Ry t Y S My α Qr Status
Front - Bow 1 2215.9 1134 2029 462 390 4415 2776 0.75 545 426 808780 1.040055 19.92599 OK
Bow 1 - Center 2243.6 1082 2029 390 370 3780 6677 0.75 470 380 732730 0.857825 12.80761 OK
Center - Bow 2 2228.7 1058 2029 370 390.5 4284 11193 0.75 450 380.25 710550 0.795364 6.301672 OK

Draft Analysis:

The minimum draft angle for sheet metal manufacturing is 7 degrees.

Roof :

Front roof rail:

Rear roof rail:

Bow Roof 1:

Bow Roof 2:

Center roof rail:

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