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SAE J987 provides a systematic, nondestructive procedure for evaluating the structural integrity of pendant-supported and luffing jib type lattice boom cranes using resistance strain gages. By simulating maximum service loading conditions under static loads, engineers can measure actual stresses, classify stress areas, and validate boom ratings against acceptance criteria based on material yield and buckling strength. This article outlines the core methodology, stress classification system, and key considerations for applying the standard.
The testing procedure involves three primary load conditions: an initial no-stress reference (N1), a dead load condition (N2) with the assembled structure ready to lift, and a working load condition (N3) supporting the specified rated load. Strain readings from these conditions yield the dead load stress S1 and working load stress S2. The maximum resultant stress Sr is then compared to established limits for four stress area types:
| Stress Area Type | Description | Acceptance Criteria (based on) |
|---|---|---|
| Type I | Areas where stresses are calculated analytically | Yield point (Sy) |
| Type II | Areas rarely calculated but evaluated by test | Yield point with safety margins |
| Type III | Areas correlated with SAE J1093 analytical procedure | Correlation with calculated stresses |
| Type IV | High stress concentration areas requiring further analysis | Special calculation methods |
Understanding these classifications helps engineers focus their analysis on the most critical regions and properly validate design calculations.
Proper instrumentation and adherence to the standard’s procedures are essential for reliable data. Key steps include:
The test results are intended to supplement, not replace, analytical methods such as SAE J1093. For production boom systems, a prototype should undergo these tests to document capability. The stress data from Type III areas in particular should be used to correlate and refine boom calculation results. The standard also allows for a tested design to be applied to a new machine without retesting if the analytical procedure shows lower stress levels and supporting structure rigidity is comparable.
From an engineering design perspective, the stress area classification provides a structured approach: Type I areas verify calculations, Type II areas catch unanalyzed details, Type III areas anchor the analytical model, and Type IV areas highlight where stress concentrations need special attention.
The standard defines two methods: supporting the structure on blocking to minimize gravity effects, or using an unassembled state. Any method that establishes a true no-stress condition is acceptable, as long as a consistent initial reference reading N1 is obtained.
Section 4.1 explicitly states that if analysis reveals a more severe loading condition than those specified in Tables 1 and 2, that condition should be added or substituted. The testing must always represent the maximum anticipated service loading.
Yes, under certain conditions: the same analytical procedure must show stress levels lower than the original application, and the supporting structure must be at least as rigid. Rigidity is assessed by measuring the change in slope of the boom foot axis during testing (per section 8.5).
The standard defines column average stress (Sra) and column maximum stress (Srm) based on multiple gages at the section. The critical buckling stress (Scr) is then compared to these values to evaluate stability. Detailed procedures are provided in Appendix C.