oyvey
New member
- May 11, 2013
- 3
Hello All,
I have been tasked with doing structural analyses of overhead lifting slings. They are for lifting ~10,000 Lbs in a factory setting.
I've been "told" that the requirement is SF = 5.0 for the entire assembly: I-beams, lugs, bolts, bearings, wires, welds... every little detail. However, in all my web searches I can only find sf=5 for wires, ropes, etc. For example MIL-S-8512D specifies designing the main structure for SF=3 against yield allowables. I found another document (from NASA) specifying main structure using the lesser of sf=3 against yield or sf=5 against ultimate, plus sf=5 for wires, etc. others yet have different sf's per failure mode (compression, tension, shear).
Can anyone please point me to an authoritative source (preferably readily available in the public domain) that specifies sf's for structural steel used in overhead lifting?
Thanks very much,
oyvey
I have been tasked with doing structural analyses of overhead lifting slings. They are for lifting ~10,000 Lbs in a factory setting.
I've been "told" that the requirement is SF = 5.0 for the entire assembly: I-beams, lugs, bolts, bearings, wires, welds... every little detail. However, in all my web searches I can only find sf=5 for wires, ropes, etc. For example MIL-S-8512D specifies designing the main structure for SF=3 against yield allowables. I found another document (from NASA) specifying main structure using the lesser of sf=3 against yield or sf=5 against ultimate, plus sf=5 for wires, etc. others yet have different sf's per failure mode (compression, tension, shear).
Can anyone please point me to an authoritative source (preferably readily available in the public domain) that specifies sf's for structural steel used in overhead lifting?
Thanks very much,
oyvey