Aircraft structural assembly and associated assembling method

摘要

An assembly includes a structural wall and a composite wall extending in the extension of the structural wall and defining a second section positioned facing a first section of the wall. The assembly includes an 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. The composite wall defines a second passage opening out into the second section and receiving the elongated element. The assembly includes a locking member added onto the elongated element. The composite wall delimits an access cavity connecting an outer surface of the composite wall to the second passage. The locking member is received into the access cavity.

主权项

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.