| 摘要 |
The device (10) has an aerodynamic support (14) for positioning and maintaining front and rear sections (Tav, Tar) and an intermediate section of a fuselage of an aircraft on a carrier aircraft (12) with longitudinal axes (Lav, Lar) and a longitudinal axis of the respective sections parallel to a plane axis (A) of the carrier aircraft. The support includes support elements (16, 18, 20, 22) fixed on an upper part (24) of the fuselage of the carrier aircraft. The support elements are aligned behind each other along the plane axis. |
