Device and method for fitting two connections at the end of two conduits, in particular in an aircraft
AssigneeAirbus Operations GmbH
InventorsDamien Fraysse, Thierry Gagnaire, Benoït Thomas
Life of this patent
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AssigneeAirbus Operations GmbH
InventorsDamien Fraysse, Thierry Gagnaire, Benoït Thomas
Estimating the term…
Device for fitting two connectors at the end of two conduits, particularly in an aircraft, with a view to subsequent mutual connection of the connectors by a connecting pipe, including a body; a first support including temporary connector retainers that define an associated connector axis; an opposite second support including temporary connector retainers that define an associated connector axis; structure for moving the first support in translation relative to the body parallel to the associated connector axis, between a retracted position and a deployed position. A method of establishing fluidic communication between two conduits in an aircraft, including fitting two connectors at the end of the two conduits by such a device.
A method of fitting two connectors to the end of two respective conduits in an aircraft, in a manner enabling subsequent mutual connection of the connectors by a connecting pipe, wherein the method includes:
A method of establishing fluidic communication between two conduits in an aircraft, including:
A device for fitting two connectors to the end of two respective conduits in an aircraft, in a manner enabling subsequent mutual connection of the connectors by a connecting pipe, comprising:
Dependencies are inferred from the claim text.