Abstract:
An aircraft assembly including a wing element and an attachment pylon of a turboengine, including a rigid structure forming a caisson defined externally by a first longeron, a second longeron, and two lateral panels. The assembly also includes an attachment mechanism of the structure on the wing element, fitted with two front attachments, each including two first fittings solid with the associated lateral panel. For each front attachment, the two first fittings are arranged respectively on either side of their associated lateral panel.
Abstract:
The manufacturing of electronic components on individual substrates made of an insulating material includes molding, in a silicon wafer, an insulating material with a thickness corresponding to the final thickness desired for the substrates, manufacturing the electronic components, and removing the silicon from the rear surface of the wafer after manufacturing of the components.
Abstract:
A method for manufacturing an inductance in a monolithic circuit including a substrate of planar upper surface, including the steps of forming in the substrate a cavity substantially following the contour of the inductance to be formed, the cross-section of the cavity being deep with respect to its width; and filling the cavity with a conductive material.
Abstract:
A method for forming a component in a portion of a semiconductor substrate on insulator delimited by a lateral wall separated by an insulating layer from a peripheral region internal to the portion and heavily doped of a same first conductivity type as the substrate. A conductive plate is formed at the same time as the wall, on a layer of protection of the substrate surface, in electric contact with the peripheral region, the plate extending above said peripheral region towards the inside of the portion with respect to the wall, beyond the location above the limit between the peripheral region and the substrate.