发明名称 |
Connection arrangement, aircraft or spacecraft, method for dropping load and method for landing |
摘要 |
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. |
申请公布号 |
US9248902(B2) |
申请公布日期 |
2016.02.02 |
申请号 |
US201113885597 |
申请日期 |
2011.11.16 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
Benthien Hermann;Poppe Andreas |
分类号 |
B64C3/38;B64C1/26;B64D1/08 |
主分类号 |
B64C3/38 |
代理机构 |
Greer, Burns & Crain, Ltd. |
代理人 |
Greer, Burns & Crain, Ltd. |
主权项 |
1. A connection arrangement, having:
a fuselage portion; a wing portion which is mounted on the fuselage portion in an upper region of the fuselage portion; a first Z-coupling element which couples the wing portion to the fuselage portion in the vertical direction of the fuselage portion; and two XZ-coupling elements which couple the wing portion to the fuselage portion in the vertical direction and the longitudinal direction of the fuselage portion; wherein the first Z-coupling element is longitudinally adjustable in the vertical direction, in order to thus adjust an angle of attack of the wing portion, wherein a second Z-coupling element is provided, which is provided so as to be longitudinally adjustable in a direction parallel to the first Z-coupling element, wherein the connection arrangement further comprises Y-coupling elements which couple the fuselage portion in the transverse direction of the fuselage portion to the wing portion, and wherein the Z-coupling elements, XZ-coupling elements and Y-coupling elements are matched to one another in such a way that in the case of a fault of one of the coupling elements, the other elements ensure a load-bearing capacity which is sufficient to enable safe normal flight operation. |
地址 |
Hamburg DE |