Device for linking a stringer and a frame of an aircraft structure
AssigneeAirbus Operations GmbH
InventorThierry Loupias
Life of this patent
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Abstract
A device for linking a frame and a stringer of an aircraft structure, including a first portion connected to a support surface of a frame, a second portion connected to a support surface of a stringer and a third portion referred to as intermediary portion connecting the first portion to the second portion. The second portion is connected to the intermediary portion by means of an articulation allowing for a relative movement between the two portions along a rotation axis perpendicular to the support surface of the stringer. The first portion is connected to the intermediary portion by means of an articulation allowing for a relative movement between the two portions along a rotation axis parallel to the support surface of the frame and to the support surface of the stringer.
Claims7
A device for linking a stringer and a frame of an aircraft structure, comprising:
- a first portion configured to be connected to a frame of an aircraft structure,
- a second portion configured to be connected to a stringer of the aircraft structure, and
- a third portion connected to the first portion and connected to the second portion,
- wherein the first portion and the third portion are movable relative to each other about a first rotation axis when the first portion is connected to the frame, and
- wherein the second portion and the third portion are movable relative to each other about a second rotation axis being perpendicular to the first rotation axis when the second portion is connected to the stringer.
Dependencies are inferred from the claim text.