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Design procedure of steel purlin

Short answer

Steel purlin design as simply supported beam under biaxial bending from dead, live, and wind loads resolved normal and parallel to roof. Compute bending moments Mz and My, select trial section, check Mz/Mdz + My/Mdy ≤ 1, shear capacity, deflection limits, and uplift case with sag rods. Use IS 800:2007 load combinations.

Describe the design procedure of steel purlins in roof truss.

A purlin is a beam spanning between roof trusses that carries the roof sheeting and transfers the loads to the truss panel points. Its design is done as a beam under bi-axial bending (IS 800:2007).

Procedure

  1. Spacing and span. Span LL = truss spacing (usually 4 to 6 m). Purlin spacing ss along the rafter is fixed by the roofing sheet (e.g. 1.2 to 1.8 m for GI/AC sheets) so that purlins sit at the truss panel points.
  2. Loads per metre of purlin.
    • Dead load: weight of sheeting ×s\times s + self-weight of the purlin (assumed, then revised).
    • Live load (IS 875 Part 2): 0.75−0.02(α−10)0.75 - 0.02(\alpha - 10) kN/m² on plan for roof slopes above 10° (minimum 0.4 kN/m²), applied on the plan projection scos⁡αs\cos\alpha.
    • Wind load (IS 875 Part 3): pd=(Cpe−Cpi)pzp_d = (C_{pe} - C_{pi})p_z acting normal to the roof, ×s\times s.
  3. Resolve vertical loads into components normal to the roof (wcos⁡αw\cos\alpha) and parallel to the roof (wsin⁡αw\sin\alpha). Wind acts normal to the roof.
  4. Load combinations (IS 800 Table 4): 1.5(DL+LL)1.5(DL + LL), 1.2(DL+LL+WL)1.2(DL + LL + WL), 1.5(DL+WL)1.5(DL + WL), and uplift 0.9DL+1.5WL0.9DL + 1.5WL (check the reversal of stress).
  5. Bending moments. Mz=wnL2/8M_z = w_nL^2/8 (simply supported; wL2/10wL^2/10 if continuous). My=wt (L′)2/8M_y = w_t\,(L')^2/8 about the minor axis, where L′L' is the span between sag rods (a sag rod at mid-span gives L′=L/2L' = L/2).
  6. Select a trial section (ISMB, ISLB, channel or angle) from Zpz,req=Mzγm0/fyZ_{pz,req} = M_z\gamma_{m0}/f_y (add about 20 to 30% for the minor-axis moment).
  7. Classification and capacity. Mdz=Zpzfy/γm0M_{dz} = Z_{pz}f_y/\gamma_{m0} and Mdy=Zpyfy/γm0M_{dy} = Z_{py}f_y/\gamma_{m0} (each not more than 1.2Zefy/γm01.2Z_ef_y/\gamma_{m0}); check lateral-torsional buckling for the uplift case when the bottom flange is in compression.
  8. Interaction (biaxial bending). MzMdz+MyMdy≤1\dfrac{M_z}{M_{dz}} + \dfrac{M_y}{M_{dy}} \le 1 (cl. 9.3.1, simplified).
  9. Shear V≤Vd=Avfy/(3γm0)V \le V_d = A_vf_y/(\sqrt3\gamma_{m0}).
  10. Deflection under unfactored loads, limit span/150 for elastic (GI) sheeting and span/180 for brittle (AC) sheeting (Table 6).
  11. Sag rods and connections. Provide sag rods (12 to 16 mm) at mid-span or third points to carry the tangential component, and cleat angles (with two bolts) to connect the purlin to the rafter; check the bolts for shear.
   truss           truss
    |<----- L ----->|
    |==== purlin ====|   sag rod at mid-span

✓ Answer checked by Claude Opus 5.5 (high effort)

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