Abstract: A combination comprises a cap for a container and a neck of a container. The neck is delimited by an outer surface from which a circular enlargement projects, the outer surface extending up to a rim of the neck. The cap comprises a side wall extending about an axis. A separation line is provided on the side wall for defining a retaining ring intended to engage with the circular enlargement to remain anchored to the neck of the container and a closure element removably engageable with the neck so as to be movable between a closed position and an open position. The separation line extends about the axis and is circumferentially interrupted so as to leave a joining portion between the retaining ring and the closure element.

Abstract: An avionics system comprising a central processing unit to implement one or more hard real-time safety-critical applications, the central processing unit comprises a multi-core processor with a plurality of cores, an avionics system software executable by the multi-core processor, a memory, and a common bus though which the multi-core processor can access the memory; the avionics system is characterized in that the avionics system software is designed to cause, when executed, the cores in the multi-core processor to access the memory through the common bus by sharing bus bandwidth according to assigned bus bandwidth shares.

Abstract: An avionics system comprising a central processing unit to implement one or more hard real-time safety-critical applications, the central processing unit comprises a multi-core processor with a plurality of cores, an avionics system software executable by the multi-core processor, a memory, and a common bus though which the multi-core processor can access the memory; the avionics system is characterized in that the avionics system software is designed to cause, when executed, the cores in the multi-core processor to access the memory through the common bus by sharing bus bandwidth according to assigned bus bandwidth shares.