Aircraft undercarriage fitted with visual warning means for signaling an angular overstroke of a steerable bottom portion of the undercarriage
US11407524B2 · kind B2 · utility
0Cited by
4References
11Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 18, 2020 |
| Grant date | Aug 9, 2022 |
| Priority date | — |
| Expiry date | Feb 4, 2041 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64F1/225
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft undercarriage comprising a top portion (2) secured to the aircraft and a steerable bottom portion (3) carrying wheels and suitable for being steered by a steering control system (4) fitted to the undercarriage or else by an external towing device, the undercarriage being fitted with visual warning means (9) for indicating an angular overstroke. The visual warning means comprising at least one visual indicator (14) mounted to move between a retracted position that is invisible and an extended position that is visible.An aircraft provided with an undercarriage.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.