Patent ID: 8844869
Filing Date: 2014-09-30
Classification: B64C,F16B

Abstract:
1. An aircraft structural assembly, comprising: an aircraft structural supporting wall having a first section along a first edge; an aircraft composite wall assembled on the structural wall, the composite wall extending in an extension of the structural wall beyond the first edge and defining a second section positioned facing the first section; an attachment device attaching the structural wall to the composite wall including at least one elongated traction element received in a first passage made in the structural wall, the first passage opening out into the first section and into a cell made in the structural wall, wherein the composite wall defines a second passage opening out into the second section and receiving the elongated element, wherein the attachment device comprises a locking member added onto the elongated element, the composite wall delimiting an access cavity connecting a surface of the composite wall to the second passage, the locking member being received into the access cavity, and in that the composite wall extends in a mean plane tilted at an angle greater than 5° relative to a mean plane of the structural wall.