dc.contributor | Asia Turbomachinery & Pump Symposium (2nd : 2018) | |
dc.creator | Schwarz, Marco | |
dc.date.accessioned | 2018-10-12T15:24:43Z | |
dc.date.available | 2018-10-12T15:24:43Z | |
dc.date.issued | 2018 | |
dc.identifier.uri | https://hdl.handle.net/1969.1/172465 | |
dc.description | Case Studies | en |
dc.description.abstract | A fifteen stage axial compressor including a bleed extraction was subject to a major overhaul after nearly 20 years of trouble free operation. Shortly after recommissioning and resumption of the production the compressor faced three major failures within two weeks.
A root cause failure analysis was conducted and revealed that the process plant start-up procedures caused gas compositions which deviated strongly from the design conditions. The valve designs as well as the available control parameters were not able to protect the compressor from off-design operating conditions. For future compressor failure prevention, the process start-up procedures were adapted and the existing control parameters/logic was upgraded. The new control logic reacts to the transient process behaviours during start-up by continuous harmonization of the safety valves. | en |
dc.format.medium | Electronic | en |
dc.format.mimetype | application/pdf | |
dc.language.iso | en | |
dc.publisher | Turbomachinery Laboratory, Texas A&M Engineering Experiment Station | |
dc.relation.ispartof | Asia Turbomachinery & Pump Symposium. 2018 Proceedings. | en |
dc.subject.lcsh | Turbomachines | en |
dc.subject.lcsh | Pumping machinery | en |
dc.title | Blade Failures on an Axial Compressor by Unexpected Gas Compositions | en |
dc.type.genre | conference publication | en |
dc.type.material | Text | en |
dc.format.digitalOrigin | born digital | en |