Fast hybrid helicopter with long range and proportional drive to the rotor and the propeller
US8181901B2 · kind B2 · utility
38Cited by
10References
26Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | May 22, 2008 |
| Grant date | May 22, 2012 |
| Priority date | — |
| Expiry date | Nov 22, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2027/8281
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A hybrid helicopter (1) includes firstly an airframe provided with a fuselage (2) and a lift-producing surface (3), together with stabilizer surfaces (30, 35, 40), and secondly with a drive system constituted by:
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.