Abstract: Methods, non-transitory machine readable media, and computing devices that manage data storage fabric health are disclosed. With this technology, a network model is applied to network data determined from monitored network traffic exchanged between storage nodes and via network connections over a cluster fabric to generate a health score for the cluster fabric. A cause of health degradation in the cluster fabric is determined based on an analysis of the network data, when the health score indicates that health of the cluster fabric is degrading. A corrective action is automatically initiated based on the cause of health degradation in the cluster fabric. With this technology, cluster fabrics in data storage networks are more effectively monitored for health degradation and, advantageously, corrective actions can be preemptively initiated to improve performance.

Abstract: Methods, non-transitory machine readable media, and computing devices that manage data storage fabric health are disclosed. With this technology, a network model is applied to network data determined from monitored network traffic exchanged between storage nodes and via network connections over a cluster fabric to generate a health score for the cluster fabric. A cause of health degradation in the cluster fabric is determined based on an analysis of the network data, when the health score indicates that health of the cluster fabric is degrading. A corrective action is automatically initiated based on the cause of health degradation in the cluster fabric. With this technology, cluster fabrics in data storage networks are more effectively monitored for health degradation and, advantageously, corrective actions can be preemptively initiated to improve performance.

Abstract: Embodiments are directed to selecting, by a computing device comprising a processor, the size of at least one prime mover associated with an aircraft to satisfy a baseline power requirement for operation of the aircraft during a steady state load condition, selecting at least one power source configuration to supplement power provided by the at least one prime mover during a transient load condition associated with the operation of the aircraft, and selecting, by the computing device, a parameter of the at least one power source configuration to provide a total power in an amount that is greater than a threshold during the transient condition.

Abstract: Embodiments are directed to selecting, by a computing device comprising a processor, the size of at least one prime mover associated with an aircraft to satisfy a baseline power requirement for operation of the aircraft during a steady state load condition, selecting at least one power source configuration to supplement power provided by the at least one prime mover during a transient load condition associated with the operation of the aircraft, and selecting, by the computing device, a parameter of the at least one power source configuration to provide a total power in an amount that is greater than a threshold during the transient condition.

Abstract: A solid oxide fuel cell generator (10) is made which contains bundles (14) of solid oxide fuel cells (36), a bus bar unit (128) in adjacent contact with the fuel cell bundles, where the bus bar unit (128) can pass electrical current, the bus bar unit (128) containing flat inner plate sections (130) adjacent the fuel cell bundles, outer solid nickel bar (134) and with solid, U-shaped nickel strap take-off connections (136) between the plates and bar; and a power lead (140) electrically connected to the outer solid nickel bar, where the flat inner plate sections (130) and solid U-shaped nickel strap take-off connections (136) pass electrical current generated in the fuel cell bundles through the bus bar units (128).

Abstract: A solid oxide fuel cell generator (10) is made which contains a plurality of bundles (14) of solid oxide fuel cells (36), the fuel cells, capable of generating electrical current, a bus bar unit (128) in adjacent contact with the plurality of fuel cell bundles at the sides of the generator, where the bus bar unit (128) can pass electrical current from the adjacent fuel cell bundles, the bus bar unit (128) containing inner flat plate/screen sections (130) near the fuel cell bundles, outer solid nickel bar (134) and with wide, solid, flexible, corrugated nickel strap electric current take-off connections (136) between the screens and bar; a power lead (140) electrically connected to the outer solid nickel bar, and also electrically through the bus bar unit to the fuel cell bundles through the take-off connections and inner screen sections; where the inner screen sections (130) and take-off connections (136) pass electrical current generated in the fuel cell bundles through the bus bar units (128) to an electric