Optimized method of controlling yaw for rotary-wing aircraft, and a system for implementing it
US7427046B2 · kind B2 · utility
4Cited by
4References
20Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jun 15, 2005 |
| Grant date | Sep 23, 2008 |
| Priority date | — |
| Expiry date | Nov 25, 2026 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C27/78
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
A method of the invention for controlling the pitch of the blades of a tail rotor of a rotary-wing aircraft includes the following operations:
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.