Field installable and removable helicopter rotor blade vibration and blade tracking device
US8192162B2 · kind B2 · utility
3Cited by
15References
21Claims
0Family size
Inventors
Key dates
| Filing date | Jul 29, 2008 |
| Grant date | Jun 5, 2012 |
| Priority date | — |
| Expiry date | Feb 3, 2031 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10S416/50
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
This invention provides convenient airframe vibration and tracking improvements of a helicopter rotor blade by use of an elastomer profile system that is attached through an adhesive system that allows convenient removal and relocation for use by the helicopter manufacturer or by the helicopter operator in a field environment.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.