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Bridge Bearing Pad Calculation: A Worked Elastomeric Bearing

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  • Bridge Bearing Pad Calculation: A Worked Elastomeric Bearing Case Study
Steel-reinforced laminated elastomeric bridge bearing between a concrete girder and pier cap, with a blurred calculation sheet in the foreground.

Bridge Bearing Pad Calculation: A Worked Elastomeric Bearing Case Study

A bridge bearing has a demanding job. It must transfer vertical reaction while accommodating the movements and rotations that occur in a bridge superstructure. For a steel-reinforced elastomeric bearing, the engineering problem is a balance of compressive, shear and rotational stiffness; it is not a simple choice of pad length, width and thickness.3

 

This article is an educational adaptation of a published Federal Highway Administration example for an interior-girder bearing at an intermediate pier. It illustrates the sequence of checks used in that example. It is not a design for a live project and must not be substituted for the governing code, the current project documents or the responsible engineer’s calculations.3

 

The illustrative inputs

The FHWA example considers a rectangular bearing with a 24 in transverse width and a 7.5 in longitudinal length. It assumes a 60 Shore A elastomer with a shear modulus, G, of 0.150 ksi. The cited maximum Service I reaction is 290.5 kips and the cited maximum live-load reaction is 129.9 kips.3

 

Input from the published example

Symbol

Value

Bearing length

L

7.5 in

Bearing width

W

24 in

Service reaction

P

290.5 kips

Live-load reaction

PLL

129.9 kips

Assumed shear modulus

G

0.150 ksi

Chosen internal elastomer layer

hri

0.5 in

Step 1: Establish a preliminary plan area

The published example uses a 1.75 ksi limit to establish a preliminary minimum plan area:

 

Arequired = 290.5 / 1.75 = 166.0 in²

 

A 24 in × 7.5 in plan gives:

 

Aprovided = 24 × 7.5 = 180.0 in²

 

The selected preliminary plan area exceeds the cited minimum. This does not complete the bearing design; it simply establishes a reasonable starting geometry for the further checks.3

 

Step 2: Check average compressive stress

Using the service reaction and the 180 in² plan area:

 

σ<sub>service</sub> = 290.5 / 180 = 1.614 ksi

 

For the live-load reaction:

 

σ<sub>live</sub> = 129.9 / 180 = 0.722 ksi

 

The values above reproduce the rounded results presented in the published example. They become inputs to the shape-factor check, which relates the geometry of the elastomer layer to the permitted stress behaviour.3

 

Step 3: Calculate the shape factor

For a rectangular elastomeric layer without holes, the FHWA example defines the shape factor as:

 

S = LW / [2hri(L + W)]

 

The example derives minimum shape-factor demands of 5.38 under total load and 4.81 under live load. Using the 0.5 in internal layer selected in the example:

 

S = 7.5 × 24 / [2 × 0.5 × (7.5 + 24)] = 5.71

 

That value exceeds the governing 5.38 value for this worked example. Rearranging the same equation gives limiting internal-layer thicknesses of approximately 0.531 in for the total-load check and 0.594 in for the live-load check; the selected 0.5 in layer therefore meets both stated conditions.3

 

What the preliminary calculation does—and does not—say

The calculation demonstrates why the internal elastomer-layer thickness cannot be selected by appearance alone. It affects the shape factor, and the shape factor in turn influences compressive and rotational stiffness. But a bearing whose area and shape factor look acceptable has not yet completed the necessary review.

 

The same FHWA design path goes on to address the following items:3

 

Further check

Why it matters

Compressive deflection

Helps assess vertical movement and joint-related implications where relevant.

Shear deformation

For movable bearings, total elastomer thickness must accommodate the design translation.

Combined compression and rotation

Helps prevent uplift and excessive edge stress under applicable service combinations.

Stability

Assesses whether geometry and load lead to an instability concern.

Reinforcement and fatigue

Confirms that steel shims/reinforcement are adequate for induced tensile stresses and fatigue considerations.

Temperature and compound grade

Elastomer selection must suit the service temperature conditions specified for the bridge.

The FHWA example notes that elastomeric materials are stiff in compression but flexible in shear, enabling a bearing to support gravity load while allowing controlled deformation. It also explains that the selected elastomer compound should suit the climatic conditions because elastomers stiffen at low temperatures.3

 

A disciplined way to start a project enquiry

A project discussion should include the governing standard, dead/live/seismic/wind or other actions as applicable, movement at each support, design rotations, bearing layout, available support dimensions, temperature range, corrosion environment, fixed or guided/free intent, installation geometry and required test or inspection documentation.

 

Berzelius Performance Materials can discuss neoprene and elastomeric bearing-pad product requirements. The final calculation, detailing, specification, acceptance criteria and project approval must remain with the responsible engineer and the governing design standard.

 

For a technical discussion, visit www.bpmaterials.uk or email sales@berzelius.uk.

 

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Recent Posts

  • Silicone Gaskets for Aviation and Marine Service: A Material-Selection Framework
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  • Neoprene Pads with Cemented Bases and Clamps: Designing the Whole Support Interface
  • Neoprene Pads: A Practical Guide to Material Versatility and Application Selection
  • Silicone Rubber vs. EPDM Rubber for Acoustic and Fire-Rated Door Seals: A Global Engineering Study

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Berzelius ® is a UK-based company with a state-of-the-art manufacturing facility in the UAE. Specializing in performance materials, Berzelius manufactures UL-compliant Fire Retardant Silicone Rubber Profiles for Fire Dampers, EPDM Rubber Sealing Systems, Neoprene Rubber Pads, Rubber Sheeting, Vibration Isolation Pads, Fluorosilicone Rubber, Aircraft Trim Seals for Aerospace Solutions, and EPDM Rubber Extrusion Profiles.
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