Aircraft rudder with articulated support structure of pedal
US12409927B2 · kind B2 · utility
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20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Mar 6, 2023 |
| Grant date | Sep 9, 2025 |
| Priority date | — |
| Expiry date | Nov 16, 2043 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C25/44
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft rudder pedal comprising a frame and at least one pedal side system. The or each pedal side system includes a pedal and an articulated support structure of the pedal connecting the pedal to the frame. The articulated support structure of said pedal comprises a crank, a lever and a support link. The crank presents a first pivotal articulation connection to the frame and a second pivotal articulation connection with the support link. The lever presents a first pivotal articulation connection with the frame and a second pivotal articulation connection with the support link.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.