(Had a connection problem, hope it won’t end as accidental double post.)
Referring to an earlier message: Cavitation as such won’t happen in the cylinder, it can especially damage pumps. If the absolute pressure of the hydraulic fluid even if only very locally and very shortly drops below some limits, small voids like vacuum bubbles can form and than implode which can cause serious damages. Due to physical laws the vacuum ist not an absolute vacuum but I leave that to the experts.
When designing hydraulic systems among the basic rules to follow is to keep all pressures and all temperatures within the applicable low and high limits and to keep the oil clean.
Sneaky can be some issues related to important temperature changes which can lead to overpressures or air entering the circuit as sealing is never perfect.
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I expect regulations to require that both the High Voltage side breaker and the Low Voltage side breaker of a transformer always trip together, regardless of the cause of the breaker opening.
I.e. if HR1 opens, LR1 will open too and vice versa (also applies by analogy to HR2 and LR2).
If HR2 or LR2 tripped to clear a detected fault, the protection function which issued the trip command should normally be displayed and possibly even be logged by the Power Management System (PMS), it depends how the protection relays are interfaced. Often critical interfacing is handled by discrete signals (e.g. 24 V DC digital I/Os) and additional non-vital communication is handled by bus communication but as said, we’d need to know further details about the exact hardware architecture of the PMS.
Among other possibilities would be human error though in my opinion not very likely but of course not fully excluded as well as a spurious trip which cause may be found… or not.
Lots of causes can initiate an unwanted (spurious) breaker trip and it’s not always possible to find out the exact cause, could for example be some shock in a specific direction with a small spring which has become too weak but still won’t cause spurious trips otherwise.
Though overall I rather suspect an issue with the protection and other digital relays as well as the PMS.
A spurious breaker trip may happen but here first the breakers protecting TR1 tripped and than there was a double generator breaker trip (DGR3 and DGR4). Also we don’t know if there are specific busbar protections which, if present, can also issue breaker trip commands.
Referring to the ICMS (PR page 10) I’m not sure at all that it’s fast enough and networked in a way that all event timestamps remain coherent for remote modules. Also we don’t know if it’s partially interfaced digitally (bus communication) or only discretely (using I/O’s, Inputs/Outputs).
When referring to the PMS and digital protections I also include genset and bay controllers.
For know I ignore if the breaker trips of the incident voyage are related to what happened the day before but I wouldn’t be surprised.
Purely intuitively I’d tend to believe that the whole suite of electrical incidents could be related to some misconfiguration of the PMS and/or other issues with devices which can issue breaker trip commands. That said, of course it’s also possible that there were real faults which had to be cleared by automatically opening the corresponding breakers.
Why TR2 was not reconnected automatically by the PMS immediately after TR1 was disconnectd is unclear, especially as TR2 was brought back online manually. Also, after DG3 and DG4 tripped (DGR3 and DGR4 tripped), once DG2 which had started automatically and got also reconnected automatically to the HV BUS as DGR2 closed automatically, it’s all but normal that neither TR1 nor TR2 was brough online automatically by the PMS.
Also the fact that DGR3 and DGR4 tripped simultaneously (or nearly?) clearly shows that two distinct trip orders have been issues, a dual purely spurious trip without any common cause would be extremely highly improbable, i.e. “close to impossible”.
It’s unclear if the engines of DG3 and DG4 were shut down at any time, if not there was probably always enough power available to run the ME (Main Engine).
It will be interesting to find out if a ME can ride through a short blackout and if so how long that grace period can be. If well designed I don’t see why a ME couldn’t ride during a couple of seconds through a blackout especially also that there’s some propeller windmilling.