Airbus Operations (s.a.s.)

Airbus Operations Gmbh

Vincent Delpy

Gérard Millet

Simon Foucart-Gaudy

Marc-Antoine Brocard

A tool for laying a sealing strip around a protruding part of a connecting element protruding from a bearing surface, the laying tool including an annular duct having an outer surface configured to delimit, with the bearing surface and the protruding part, a cavity when the annular duct is positioned around the protruding part and in contact with the bearing surface, the annular duct including at least one orifice for supplying pasty composition and outlet orifices for injecting the pasty composition into the cavity to form the sealing strip. A method for laying a sealing strip using the tool is disclosed and an aircraft with at least one sealing strip obtained using the method.

Tool for laying a sealing strip around a protruding part of a connecting element, method for laying a sealing strip using said tool, and aircraft comprising at least one sealing strip obtained using said laying method

An electrical connection device including a first end-fitting secured to a first part of an electrical cable, including a first cylindrical lateral surface coaxial to a first axis and a first end surface forming a first angle with the first axis, a second end-fitting secured to a second part of an electrical cable, including a second cylindrical lateral surface coaxial to a second axis and a second end surface forming a second angle with the second axis equal to the first angle, and a holding system configured to hold the first and second end surfaces pressed against one another. The first and second end-fittings are directly in contact with one another and held in contact via a holding system coaxial to the first and second end-fittings and supported by the latter, which contributes to obtaining a compact device.

Electrical connection device comprising end-fittings placed end to end

A drainage valve comprising a through hole, a seat around the through hole, a shutter comprising an end face and movable in a longitudinal direction between a first position in which the end face of the shutter is away from the seat and a second position in which the end face of the shutter is pressed against the seat and blocks the through hole, and an elastic element configured to keep the shutter in the first position. The shutter has a recess, emerging at its end face, configured to introduce therein a part of a tool in order to temporarily secure the part of the tool and the shutter in order to displace it in two directions longitudinally.

Aircraft drainage valve, tool for checking the correct operation of said drainage valve and method for checking the operation of said drainage valve using said checking tool

A seal includes a barrel extending between a base and a top, in which the barrel has a cylindrical cavity passing through it between its base and its top, and a skirt indissociable from the barrel and extending around said barrel, in which the skirt adopts the shape of a dome of which the exterior edges extend out beyond the base starting from the top. The seal is able to divert the fluid and keep the space under the skirt fluid tight.

Seal with skirt

A boom for an electrical harness, including a straight bar extending in a longitudinal direction, and several supports distributed along and attached to the bar, to which supports at least one electrical harness is connected in operation. The bar includes at least two parts configured to slide relative to one another in the longitudinal direction so that a length of the bar can be adjusted.

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Toulouse, France

Vincent Delpy