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High-lift trailing edge flap system for an aircraft wing unit
| Content Provider | Semantic Scholar |
|---|---|
| Copyright Year | 2014 |
| Abstract | A high-lift trailing edge flap system for an aircraft wing unit is provided. In the high-lift trailing edge flap system, the backward movement and the inclination of the trailing edge flap (2) in the extended position are dissociated in order to allow for the incorporation of an actuating mechanism (11, 12, 14, 15) into a wing (1) in the stowed position. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | https://patentimages.storage.googleapis.com/b0/2c/eb/4a118825dfd8a6/US9545992.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |