Bolted Beam Splice
Web plates (double shear) + flange plates — shear and moment transfer per AISC 360-22 Chapter J
Beam Splice — AISC 360-22 Ch. J
kip · ft · in| Check | φRn | DCR |
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| Check | Actual | Limit | Status |
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A bolted beam splice joins two beam segments at a field location where a continuous member cannot be delivered or erected as a single piece. The splice must transfer the full factored shear Vu and moment Mu across the joint. In most cases the splice is designed as a fully restrained (FR) moment connection, meaning it is intended to transfer the same moment and shear as would occur in a continuous beam at that cross-section.
The load path is divided into two sub-systems:
| Sub-system | Force transferred | Shear plane |
|---|---|---|
| Web splice plates (2 plates) | Shear Vu + moment web component Mw | Double shear (2 planes per bolt) |
| Flange splice plates (1 per flange) | Flange force Pf = Mu / (d − tf) | Single shear |
The moment is typically assumed to be resisted entirely by the flange plates (flange-force model), while the web plates carry only the shear. This simplification is conservative and widely used in practice. Alternatively, a more refined approach distributes moment between the web plates and flange plates in proportion to the web and flange contributions to the section modulus, but DG9 and common practice favor the flange-force approach for its simplicity.
Two identical plates are placed symmetrically on opposite sides of the beam web. Each bolt passes through both plates and the web, engaging two shear planes, so the bolt shear capacity is doubled relative to single shear: φRn,bolt = 2 × φFnvAb. Plate capacities (shear yield, shear rupture, block shear, bending) are summed for both plates combined.
Eccentricity effect: the bolt group centroid is offset horizontally by the eccentricity aw from the splice centerline. This offset creates a secondary moment Me = Vu × aw that must be distributed among the bolts in addition to the direct shear. The elastic vector method (instantaneous center method, elastic assumption) resolves this: each bolt resists a direct shear component Vd = Vu/n and a torsional component proportional to its distance from the bolt group centroid. The critical bolt is the one with the largest resultant force.
rcrit = √((Vdirect + Vtorsion,x)² + Vtorsion,y²) ≤ φRn,bolt
The plate must also be checked for out-of-plane bending due to the eccentric shear (§F11 for plates in bending). The moment in each web plate is Mplate = Vu × aw / 2 (half to each plate), and the plastic section modulus Z = tphp²/4.
One plate is placed on the outside face of each beam flange and bolted through the flange. The flange force at the splice is:
Pf = Mu / (d − tf)
where d − tf is the distance between flange mid-planes (moment arm). Each plate must be adequate in both tension (top flange in negative moment, bottom flange in positive moment) and compression, since the moment direction can reverse depending on the load combination.
Design checks for the flange plate in tension (AISC 360-22 Chapter J):
| Limit state | Section | φ | Expression |
|---|---|---|---|
| Bolt shear (nf bolts) | §J3.6 | 0.75 | φFnvAb × nf |
| Plate tension yield (gross section) | §J4.1 | 0.90 | φFy bfp tfp |
| Plate net section rupture | §J4.1 | 0.75 | φFu (bfp − dh) tfp |
| Bolt bearing on plate | §J3.10 | 0.75 | Based on clear distance, Fu, db |
| Bolt bearing on beam flange | §J3.10 | 0.75 | Based on flange tf and Fu,beam |
One bolt hole is deducted from the net section for rupture because the critical cross-section (at the outermost bolt nearest the splice) has only one row of holes transverse to the force direction in a single-row configuration. For wider plates with two rows of bolts, both holes would be deducted.
Bearing strength accounts for the plate material being compressed and deformed by the bolt shank. AISC 360-22 §J3.10 gives two equations based on the clear distance lc between bolt holes (or between the hole and the plate edge):
| Condition | Nominal bearing strength Rn |
|---|---|
| Deformation at bolt hole is a design consideration | 1.2 lc t Fu ≤ 2.4 db t Fu |
| Deformation is not a design consideration | 1.5 lc t Fu ≤ 3.0 db t Fu |
The total bearing capacity of the bolt group equals the sum of individual bolt bearing capacities. End bolts (nearest the plate edge) have smaller clear distances lc = ev − dh/2 and govern when edge distances are small. Interior bolts have lc = s − dh where s is the bolt pitch. This calculator uses the deformation-controlled equation (1.2 lc cap) as the standard design approach, applied separately to the web plate, beam web, flange plate, and beam flange.
Block shear is a combined failure mode in which a block of material tears out along a shear plane through the bolt holes and a tension plane perpendicular to the load. It is often the governing limit state for web plates with short edge distances or few bolt rows. The nominal strength is:
Rn = min(0.6FuAnv + FuAnt , 0.6FyAgv + FuAnt)
where Agv = gross shear area = (n−1)s + ev) × tp; Anv = net shear area (holes deducted); and Ant = net tension area = (eh − dh/2) × tp. The φ factor for block shear is 0.75. For web splice plates, the computation is performed on one plate and doubled (both plates carry equal load). The horizontal edge distance eh from the bolt centerline to the free (non-loaded) edge of the plate defines Ant.
The nominal shear stress Fnv depends on the bolt grade and whether threads are included in the shear plane (N) or excluded (X). AISC Table J3.2 values:
| Grade | Fnv threads included (N) [ksi / MPa] | Fnv threads excluded (X) [ksi / MPa] |
|---|---|---|
| A307 / 4.6 | 27 / 160 | 27 / 180 |
| A325 / 8.8 | 48 / 320 | 54 / 360 |
| A490 / 10.9 | 60 / 400 | 68 / 450 |
Snug-tight bearing-type connections (most common for splice plates) allow threads in the shear plane (N condition). Fully pretensioned connections or slip-critical connections are required by some codes for seismic or fatigue applications but are not typically required for gravity splice plates. Threads are excluded (X condition) only when the bolt is carefully positioned so the thread run-out does not enter the shear plane — this is difficult to control in the field and the N condition is the standard assumption.
Successful beam splice design involves balancing several competing requirements. A few practical rules of thumb:
- Place the splice at a point of contraflexure (zero moment) where possible, minimizing flange plate size. In continuous beams this is roughly 20–25 % of the span from an interior support.
- Use the same bolt diameter throughout the connection — mixing sizes complicates shop fabrication and field inspection.
- Web plate height hp should be at least 0.6dbeam to provide adequate shear area and avoid large eccentricity moments in the plates.
- Minimum web plate thickness is typically 5/16 in (8 mm) for weldability and handling; maximum is limited by bearing ratio requirements.
- Flange plate width should match or exceed the beam flange width to keep the bolt edge distances manageable and to simplify the field layout.
- For seismic SMF splices, AISC 341 requires the splice to develop the full plastic moment of the beam, which typically controls over the demand-based design used here.