Connection arrangement, aircraft or spacecraft, method for dropping load and method for landing
US9248902B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Nov 16, 2011 |
| Grant date | Feb 2, 2016 |
| Priority date | — |
| Expiry date | Sep 5, 2032 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D1/08
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A connection arrangement having: a fuselage portion; a wing portion which is mounted on the fuselage portion in an upper region thereof; a first Z-coupling element which couples the wing portion to the fuselage portion in the vertical direction thereof; and two XZ-coupling elements which couple the wing portion to the fuselage portion in the vertical direction and longitudinal direction thereof; the first Z-coupling element being longitudinally adjustable in the vertical direction in order to thus adjust an angle of attack of the wing portion.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.