Abstract: A pouch fitment (10) is provided and comprises a base (12) which is attachable to a pouch and includes a dispensing spout (20). The fitment further comprises a closure (14) for closing the spout. The closure is non-releasably associated with the base.

Abstract: An electrical power supply module intended to supply power to an on-board DC electrical network of an aircraft comprising a battery (12) including a primary line (16), a secondary line (18) and a switching member between said primary and secondary lines; and an electrical distribution box (24) separate from the battery (12) including at least one electrical power supply busbar (26) and a plurality of electrical distribution lines (28) each bearing a circuit breaker (30). The power supply module comprises a connection pad (32) positioned on the secondary power supply line (18) allowing a voltage connection between the battery (12) and the electrical distribution box (24).

Abstract: The invention relates to a cap for the neck of a container and to a method for producing one such cap. According to the invention, the skirt (12) of the cap (1) is provided with frangible bridge elements (44A, 44B) which break when the cap is first opened. In addition, on either side of the aforementioned frangible bridge elements, the skirt includes a non-removable part and a removable part provided with an outer biasing tab (24) that only extends along a peripheral portion (12A) of the skirt. In order to limit the biasing force of the tab, so as to release the removable skirt part, the radial dimension (e44A) of the bridges (44A) located in the skirt portion (12) associated with the tab is smaller than the radial dimension (e44B) of the bridges (44B) located outside said portion.

Abstract: The invention relates to a cap for the neck of a container and to a method for producing one such cap. According to the invention, the skirt (12) of the cap (1) is provided with frangible bridge elements (44A, 44B) which break when the cap is first opened. In addition, on either side of the aforementioned frangible bridge elements, the skirt includes a non-removable part and a removable part provided with an outer biasing tab (24) that only extends along a peripheral portion (12A) of the skirt. In order to limit the biasing force of the tab, so as to release the removable skirt part, the radial dimension (e44A) of the bridges (44A) located in the skirt portion (12) associated with the tab is smaller than the radial dimension (e44B) of the bridges (44B) located outside said portion.

Abstract: The invention concerns a method for defining scaled stresses indicating an estimation of the product reliability with maximum accuracy. It comprises a phase which consists in inputting characteristic parameters (1), defining a sequence of stresses and simulating occurrences of failure time (2), estimating the characteristic parameters with indication of trust intervals (3), estimating proportions of faulty parts (4), a phase of testing the accuracy of the estimation (5), a feedback on phase (2) defining the cycle of stresses in case of insufficient accuracy. That set of operations (6) is only simulated, but when the estimation of proportion is determined to be sufficiently accurate, the cycle of stresses is implemented on a real test. The inventive method can also be used to test electronic products sensitive to thermal or vibratory stresses as well as mechanical products sensitive to fatigue stresses.