High-lift system of an aircraft
US8960610B2 · kind B2 · utility
0Cited by
2References
27Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Sep 22, 2011 |
| Grant date | Feb 24, 2015 |
| Priority date | — |
| Expiry date | Sep 22, 2031 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10S464/902
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A high-lift system of an aircraft has at least one drive unit, at least one load station as well as one or more transmissions for transmitting the drive energy of the drive unit to the at least one load station. One or more of the transmissions are made as transmission shafts from a material containing titanium or include a material containing titanium.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.