Steel Lattice Column Design — Built-Up Members, Lacing, and Batten Plates

Built-up (lattice) columns consist of two or more main components (typically channels, angles, or W-shapes) connected by lacing bars, batten plates, or perforated cover plates. They are used when a single rolled section cannot provide the required radius of gyration, or when architectural/functional considerations demand an open cross-section (such as columns supporting crane runways). AISC 360-22 Section E6 provides the modified slenderness ratio approach for their design.

Modified slenderness ratio per AISC 360-22 Section E6

The key principle: a built-up column is weaker than a solid column of the same overall slenderness because the lacing or battens introduce shear flexibility. AISC accounts for this through a modified slenderness ratio:

(KL/r)_m = sqrt[(KL/r)_o^2 + (a/r_i)^2]

where:

This formula penalizes wide connector spacing. The term (a/r_i) represents the local slenderness of each component between lacing points. AISC requires a/r_i <= 3/4 * (KL/r)_o to prevent local buckling of individual components from governing before global buckling of the built-up member.

Worked example — double-channel lattice column

Given: Built-up column made from two C12x20.7 channels, back-to-back with 12 in. separation (face-to-face). Lacing bars at 45 degrees, single-lacing system. Column length = 24 ft, pinned-pinned (K = 1.0). A36 steel (Fy = 36 ksi).

Step 1 — Individual channel properties: A = 6.09 in.^2 per channel, I_x = 129 in.^4, I_y = 3.88 in.^4, r_y = 0.799 in. x-bar (distance from web back to centroid) = 0.698 in.

Step 2 — Built-up section properties about the lacing axis (y-y, the built-up axis):

Separation center-to-center = 12 + 2 * 0.698 = 13.40 in. (distance between channel centroids in the y-direction, assuming back-to-back with 12 in. gap)

Wait — for back-to-back channels with a 12 in. face-to-face gap:

Centroid distance = 12 + 2 _ x-bar = 12 + 2 _ 0.698 = 13.40 in. (from centroid of left channel to centroid of right channel, measured perpendicular to webs).

I*y,built-up = 2 * [I_y + A _ (13.40/2)^2] = 2 _ [3.88 + 6.09 _ 6.70^2] = 2 * [3.88 + 273.4] = 554.6 in.^4

A_total = 2 * 6.09 = 12.18 in.^2 r_y,built-up = sqrt(554.6 / 12.18) = sqrt(45.5) = 6.75 in.

Step 3 — Overall slenderness about built-up axis: (KL/r)_o = 1.0 _ 24 _ 12 / 6.75 = 288 / 6.75 = 42.7

Step 4 — Lacing spacing and local slenderness: For single lacing at 45 degrees: lacing bar spacing along the column = separation _ tan(45) = 13.40 _ 1.0 = 13.40 in. Use a = 13.5 in. (practical rounding).

r_i = r_y of individual channel = 0.799 in. a/r_i = 13.5 / 0.799 = 16.9

Check: a/r*i <= 3/4 * (KL/r)_o = 0.75 _ 42.7 = 32.0. Since 16.9 < 32.0, OK.

Step 5 — Modified slenderness ratio: (KL/r)_m = sqrt(42.7^2 + 16.9^2) = sqrt(1,823 + 286) = sqrt(2,109) = 45.9

Step 6 — Column capacity using AISC Chapter E: F_e = pi^2 * 29,000 / 45.9^2 = 286,200 / 2,107 = 135.8 ksi

Since Fy/Fe = 36/135.8 = 0.265 < 2.25: F*cr = 0.658^(Fy/Fe) * Fy = 0.658^0.265 _ 36 = 0.896 * 36 = 32.3 ksi

phi _ P_n = 0.90 _ 32.3 * 12.18 = 354 kips

Without the modification: Fcr at KL/r = 42.7 would give phi * Pn = 0.90 * 33.0 * 12.18 = 362 kips. The modification reduces capacity by about 2% in this case because the lacing spacing is well-controlled.

Lacing bar design (the "2% rule")

Lacing bars must resist a shear force equal to at least 2% of the axial compression in the column (AISC 360 Section E6.2). For the example above:

V_lacing = 0.02 * P_u

If P_u = 300 kips: V_lacing = 0.02 * 300 = 6 kips

For single lacing at 45 degrees, the force in each lacing bar = V*lacing / (2 * cos(45)) = 6 / (2 _ 0.707) = 4.24 kips (two lacing planes, one on each side).

The lacing bar must be checked as a compression member with KL/r_lacing <= 140 (AISC Section E6.2). For a flat bar 2 in. x 3/8 in., L_lacing = 13.4 / sin(45) = 18.95 in.:

r_bar = t / sqrt(12) = 0.375 / 3.464 = 0.108 in. KL/r = 18.95 / 0.108 = 175 >> 140 (NOT OK)

Need a larger bar. Try 2.5 in. x 1/2 in.: r = 0.5/3.464 = 0.144 in., KL/r = 18.95/0.144 = 131.6 < 140 (OK).

Batten plates as an alternative

Batten plates (flat plates welded or bolted perpendicular to the column axis) can replace lacing. They create a Vierendeel (moment frame) action between the main components. AISC Section E6.2 requires:

Code comparison

Aspect AISC 360-22 AS 4100:2020 EN 1993-1-1 CSA S16-19
Modified slenderness formula Sect. E6, sqrt method Clause 6.5 (similar) Sect. 6.4, lambda_eff Clause 13.3.4
Minimum shear force 2% of axial load 2.5% of axial load 2.5% + initial imperfection 2% of axial load
a/r_i limit <= 0.75 * (KL/r)_o <= 0.5 * lambda_n <= 70 or 0.75 * lambda <= 0.75 * (KL/r)
Lacing bar KL/r limit 140 140 150 (tension) / 70 (compression) 140
Batten plate provision Sect. E6.2 Clause 6.5.3 Sect. 6.4.3 Clause 19

EN 1993-1-1 uses a more refined approach, modeling the built-up member with initial bow imperfections and calculating the shear force from the imperfection. The 2% rule in AISC is a simplification of this concept.

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