rather_be_riding
Mechanical
- Sep 21, 2021
- 57
Someone floated a project the other day which involved refurbishing a used item of plant for a customer who has no loading history for it. The plant structure can be considered to be fatigue sensitive and some anecdotal evidence suggests that maybe at some point someone was actually concerned about this but there's really nothing to work with.
For the purposes of debate, lets say that the structure all checks out and welds are subjected to NDT and turn out to be in good condition. How do you go about determining the remaining fatigue life? It could be 90% of its way through its design life or 10%; at either point, the structure should still be in good condition. I recognise this is probably a somewhat unusual case and maybe no one has a great answer but even a good text reference would be appreciated.
Side note: I was unsure if this was better here or in structural but figured that maybe the aero engineers might have valuable input and they'd be more likely to monitor this forum.
For the purposes of debate, lets say that the structure all checks out and welds are subjected to NDT and turn out to be in good condition. How do you go about determining the remaining fatigue life? It could be 90% of its way through its design life or 10%; at either point, the structure should still be in good condition. I recognise this is probably a somewhat unusual case and maybe no one has a great answer but even a good text reference would be appreciated.
Side note: I was unsure if this was better here or in structural but figured that maybe the aero engineers might have valuable input and they'd be more likely to monitor this forum.