Introduction
The girder is the backbone of any Electric Overhead Traveling (EOT) crane. Whether you are designing a Single Girder Cranes (using rolled sections like ISMB) or a Double Girder Crane (using Box sections), selecting the right section is not just about "guessing" the heavy metal. It is a precise science of balancing load capacity, span, and deflection.
In this post, we will break down the detailed design calculation process for a crane girder as per standard codes (such as IS 3177, IS 807, or CMAA 70).
Step 1: Define the Design Parameters
Before touching the calculator, you must have your input data locked in. If you get these wrong, the whole design fails.
Safe Working Load (SWL): The capacity (e.g., 5 Ton, 10 Ton).
Span (L): The center-to-center distance between the rails.
Class of Duty: (M1 to M8). This determines your Impact Factor. Higher duty cycles (like M8) require higher safety margins.
Material Grade: Typically E250 (Fe 410W) or E350 (Fe 510W).
Step 2: Calculate the Loads
You aren't just lifting the weight of the goods; you are lifting the hoist, the accessories, and fighting gravity and momentum.
Live Load: The SWL + Weight of the Hoist/Crab.
Dead Load: The self-weight of the girder itself (initially assumed, then verified).
Impact Factors: As per IS 807, you must multiply the live load by a "Duty Factor" (e.g., 1.1 to 1.4 depending on hoist speed and class).
Pro Tip: Don't forget the Surge Loads (Horizontal forces due to acceleration/braking) which affect the lateral stability of the girder.
Step 3: Calculate Maximum Bending Moment ($M_{max}$)
The critical part of the design is finding the point where the beam suffers the most stress. For a crane, this is a moving load problem.
The worst-case scenario usually occurs when the loaded hoist is at the center of the span (for single girder) or when the wheel loads are positioned to create maximum moment (for double girder).
The general formula for the maximum Bending Moment ($M$) is:
Where:
$W$ = Total design load (including impact factors)
$L$ = Span of the crane
Step 4: Determine Required Section Modulus ($Z_{req}$)
Now that we know the force trying to bend the beam ($M$), we need to find a section strong enough to resist it. We use the allowable bending stress ($\sigma_{b}$) of the steel.
If you are using standard steel (Fe 410), $\sigma_{b}$ is typically around 165 MPa (or $0.66 \times Yield Stress$).
The resulting $Z_{req}$ value tells you the minimum geometric strength your girder needs.
Selection:
For Single Girder: Look at a steel table and pick an ISMB (I-Beam) with a $Z$ value higher than your calculated $Z_{req}$.
For Box Girder: You must design a custom box by selecting Plate Thicknesses (Web and Flange) to achieve the required Inertia.
Step 5: The Deflection Check (The Most Critical Step)
A beam might be strong enough not to break, but if it bends (sags) too much, the trolley will roll to the center on its own! This is why deflection is often the governing factor in crane design.
Calculate the actual deflection ($\delta$) using:
Where:
$E$ = Modulus of Elasticity (typically $2 \times 10^5$ MPa for steel)
$I$ = Moment of Inertia of your selected section.
The Standard Limit:
According to IS 3177/IS 807, the allowable deflection is typically:
Span / 750 (For moderate duty)
Span / 1000 (For heavy duty/precision cranes)
If your calculated $\delta$ is higher than the limit, you must increase the section size, regardless of what the Bending Moment calculation said.
Step 6: Shear and Stability Checks
Finally, ensure the web of your girder is thick enough so it doesn't buckle under the weight of the wheel loads (Shear Check).
Shear Stress ($\tau$): Force / Area of the Web.
Buckling: If using a tall Plate Girder, you may need vertical stiffeners to prevent the web from crumpling.
Conclusion
Designing a girder is an iterative process. You assume a section, check the Bending Moment, and then check the Deflection. If it fails deflection, you go bigger.

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