Patent · US Active

Connection arrangement, aircraft or spacecraft, method for dropping load and method for landing

US9248902B2 · kind B2 · utility

4Cited by
31References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 16, 2011
Grant dateFeb 2, 2016
Priority date
Expiry dateSep 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.