Apparatus for connecting a rotor blade to a rotor hub
US4086024A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Sep 15, 1976 |
| Grant date | Apr 25, 1978 |
| Priority date | — |
| Expiry date | Sep 15, 1996 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C27/51
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A rotor blade is connected to a rotor hub, for example, in a helicopter, by t least one pair of damping elements and by a blade connector bolt. The damping elements comprise metal discs and layers of elastomeric material arranged in sandwich fashion. The damping elements are arranged symmetrically relative to the rotor blade, as well as to the blade connector bolt. Furthermore, the damping elements are connected in a force transmitting manner to the rotor blade on the one hand and to the rotor hub on the other hand.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.