Aircraft structural assembly and associated assembling method
US8844869B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Jun 3, 2011 |
| Grant date | Sep 30, 2014 |
| Priority date | — |
| Expiry date | Dec 25, 2032 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF16B37/047
- WIPO fieldMechanical elements
- WIPO sectorMechanical engineering
Abstract
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.