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:
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:
The invention relates to a connection assembly of an engine pylori underneath an aircraft wing, the wing being provided with a fitting (6), the engine pylori being provided with a fork joint (5) nested in the fitting and fixed to the said fitting by means of a traversing pin system (10), provided with: an external primary pin (11), a secondary pin (12) mounted inside the primary pin, a primary shoulder (13) mounted directly around the primary pin, at a blind end of the pin system, to block the said pin in translation, a secondary shoulder (14) mounted around one end of the secondary pin, at a blind end of the pin system, to block the system in rotation, an interlocking assembly (15, 16) mounted around the primary pin and the secondary pin, at a free end of the pin system, to block the pin system in translation.
Abstract:
A method for manufacturing, in a monolithic circuit including a substrate, an inductance and a through via, including the step of forming, from a first surface of the substrate, at least one trench according to the contour of the inductance to be formed; forming by laser in the substrate a through hole at the location desired for the via; simultaneously insulating the surface of the trench and of the hole; and depositing a conductive material in the trench and at least on the hole walls.
Abstract:
An aircraft engine attachment device including a rigid structure and a mechanism attaching the engine on the rigid structure, the attachment mechanism including a rear engine attachment and a device for taking-up thrust forces generated by the engine. The rear engine attachment is attached to the rigid structure by two lateral fittings attached to the rigid structure. The force take-up device includes two connecting rods mechanically connected to a spreader beam by a mechanical connection, a connection fitting attached to the rear engine attachment and mechanically connected to the rigid structure by a thrust pin, the lateral fittings including a stop mechanism to limit pivoting of the spreader beam if a connecting rod breaks and ensuring transmission of thrust forces to the rigid structure.
Abstract:
An aircraft engine attachment configured to be inserted between an engine and an EMS, the attachment including a clevis connected to a first fixing device including an end fitting with two arms and a pin passing through the clevis and the two arms, in each of which an orifice is formed including a first ring and a second ring respectively holding the pin. The first ring includes a bottom acting as a stop for a first end of the pin, and the first attachment device includes a mechanism to stop the pin in translation cooperating with a second end of the pin.
Abstract:
An aircraft engine attachment configured to be inserted between an engine and an EMS, the attachment including a plate assembly connected to a first fixing device including an end fitting with two arms and a pin passing through the plate assembly and the two arms, in each of which an orifice is formed including a first ring and a second ring respectively holding the pin. The first ring includes a bottom acting as a stop for a first end of the pin, and the first attachment device includes a mechanism to stop the pin in translation cooperating with a second end of the pin.
Abstract:
An aircraft assembly including a wing element and an attachment pylori 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:
A connection assembly of an engine pylon underneath an aircraft wing, the wing being provided with a fitting, the engine pylon being provided with a fork joint nested in the fitting and fixed to the said fitting by means of a traversing pin system, including: an external primary pin, a secondary pin mounted inside the primary pin, a primary shoulder mounted directly around the primary pin, at a blind end of the pin system, to block the said pin in translation, a secondary shoulder mounted around one end of the secondary pin, at a blind end of the pin system, to block the system in rotation, and an interlocking assembly mounted around the primary pin and the secondary pin, at a free end of the pin system, to block the pin system in translation.
Abstract:
A method for handling a thin silicon wafer including the steps of successively forming on a surface of the wafer a first protection layer, a first etch stop layer, and an external layer; forming on a surface of a support wafer a gluing layer of the same material as the external layer of the wafer, the surface of the support wafer including a plurality of pads, the respective upper portions of which are substantially planar and coplanar; fastening, by direct gluing, the external layer of the wafer and the gluing layer of the support wafer; processing the wafer to form circuits therein; depositing a second protection layer on the wafer surface which is not glued to the support wafer; and removing by an etch process the material forming the external layer of the wafer and the gluing layer of the support wafer.