Segmentized flap system
US4892274A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Aug 26, 1986 |
| Grant date | Jan 9, 1990 |
| Priority date | — |
| Expiry date | Aug 26, 2006 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C9/16
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A flap system along the trailing edge of a transonic aircraft wing which system includes segments arranged in span direction, a driving system for protraction and retraction of the segments includes a plurality of spindle drives connected to the segments such that each segment is connected to at least two spindle drives; are controlled the spindle drives in such a manner that at least some of the drives are independently controlled from each other so that the segments can pivot on vertical axes, in addition to a regular pivoting about respective horizontal axes.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.