Fastening system for fastening a component on a fuselage structure
US11136124B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Dec 17, 2018 |
| Grant date | Oct 5, 2021 |
| Priority date | — |
| Expiry date | Apr 17, 2040 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF16B19/02
- WIPO fieldMechanical elements
- WIPO sectorMechanical engineering
Abstract
A system has a frame with first and second spaced apart edges, a first holder couplable to the fuselage structure and embodied for articulated connection to a first region of the frame that is close to the first edge, a second holder couplable to the fuselage structure, and a strut. A first end of the strut is connectable in an articulated manner to the second holder. A second end of the strut is connectable in an articulated manner to a second region of the frame near the second edge and remote from the first edge. The frame and the strut form a triangular structure with the first and second holders. The strut and the frame form two sides of the triangular structure. A length of the first and/or second side is variable to adjust the position of the frame.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.