Airbus Operations (s.a.s.)

Cedric Sable

Alexis Courpet

Olivier Bourbon

Matthieu Biteau

Thomas Barre

Jean-Marc Roques

A device to attach an aircraft's piping that includes a clamping ring made up of two jaws shaped into a gliding arc breaker separator and including at least one transverse support cut-out for at least one tube.

Fixture device for an aircraft tubing

A coupling device for piping including a duct; a coupling with a hermetic longitudinal sliding connection with an extremity of the duct along a total distance parallel to a longitudinal axis of the duct; a device to stop the translational movement of a first extremity of the duct in the coupling for a travel distance less than the total distance. The device being withdrawable for a defined compression condition of the duct.

Anti-buckling coupling device for piping

Aircraft including a fuel pump fastened to a tank panel

The aircraft comprises: It is arranged in such a manner that the bearing point(s) between the panel and a first one of the members selected from the valve and the actuator, and preferably the actuator, is/are provided by means of the second one of these members.

Aircraft including a fuel valve and a control actuator fastened to the valve

A fuel piping connection device for aircraft includes a male end fitting and a female end fitting that are configured to engage one another. The male and female end fittings are made of a resistive material that is an insulating material loaded with conducting fibers. Each of the male and female end fittings is configured to be bonded to a radial outer wall at an extremity of a respective tube in the fuel piping or to a radial outer wall at an extremity of a respective piping connector. Each of the male and female end fittings includes an inwardly projecting shoulder configured to engage with an axial end surface of the respective tube in the fuel piping or with an axial end surface of the respective piping connector.

Growing community of inventors

Toulouse, France

Cedric Sable