Aircraft rudder pedal frame
US12214861B2 · kind B2 · utility
0Cited by
5References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Mar 6, 2023 |
| Grant date | Feb 4, 2025 |
| Priority date | — |
| Expiry date | Mar 23, 2043 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C13/50
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft rudder pedal frame includes a base, a support framework and connection interfaces. Each connection interface is able to connect another part of the rudder pedal to the frame. The support framework connects each connection interface to the base. The support framework includes framework elements arranged in a lattice, at least one of the framework elements extending from each connection interface.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.