Aerodynamic flap support structure
US10850829B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Jun 26, 2018 |
| Grant date | Dec 1, 2020 |
| Priority date | — |
| Expiry date | May 1, 2039 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/40
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A flap deployment apparatus and system for a wing of an aircraft that includes a support structure having a first aerodynamic surface. A nose fitting secures the support structure to a forward portion of an aircraft wing and an aft fitting secures the support structure to an aft portion of the wing. A carrier beam having a second aerodynamic surface is coupled to the support structure. The carrier beam is movable between a stowed position and a deployed position. Links guide the carrier between the positions. The first and second aerodynamic surfaces are configured to define a continuous aerodynamic surface when the carrier beam is in the stowed position. The apparatus includes a nose fairing having a third aerodynamic and a mid fairing cover having a fourth aerodynamic surface. The third and fourth aerodynamic surfaces also defines the continuous aerodynamic surface when the carrier beam is in the stowed position.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.