Aircraft door equipped with a system for adjustment in position and method for installing such a door
US12312065B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Jan 27, 2022 |
| Grant date | May 27, 2025 |
| Priority date | — |
| Expiry date | Jan 27, 2042 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C1/1461
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft door mounted in a fuselage in a reference frame X, Y, Z, having a casing, a door leaf and a support arm enabling the door leaf to be installed and the position thereof to be adjusted relative to the fuselage by a pair of fasteners. Each fastener (10, 40) includes a pivot (16, 46) rotatable about a common axis parallel to the axis Z, a base (13, 43) fastened to the casing (3), and a trolley (14, 44) movable on this base (13, 43), the base (13, 43) and the trolley (14, 44) of each fastener (10, 40) forming two translational adjustment links in directions parallel to the X and Y axes, these directions determining adjustment axes (11, 12; 41, 42) secant in a plane parallel to the plane XY.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.