This is a CO gas expander turbine for cat cracker regenerator flue gas. The turbine drives the air blower for the regenerator, which has a helper steam turbine. The CO gas expander exhaust includes a rupture disc upstream of the first block valve. However, for some undiscovered, undocumented reason, it is sized for only ~15% of the normal operating flow, and I am trying to recreate the original designer's relief evaluation. I know by today's standards, we would assume the exhaust valve can be inadvertently closed at any time, not just a turndown condition.
If this were a relief valve for a centrifugal pump to protect piping and downstream equipment from a high deadhead pressure, I'd look at the pump curve to find the flow at the point where the valve is relieving. This could reduce the required capacity below normal operating flow. However, in the case of a gas turbine expander, I have no knowledge/experience of whether a similar evaluation can be made, nor have I ever seen a "turbine curve," nor do I have strong hopes that it would reduce the required flow capacity as far as 15% of normal. But, we tend to assume our predecessors from several decades ago made reasonable design choices, and would like to have strong argument that they were unreasonable, at least by today's standards, before installing a much larger relief device.
What are your thoughts?