| 摘要 |
<p>1. Aircraft which are launched from containers assembled in batteries, containing propulsion units with fuel tanks (14) forming structual parts which can be assembled with the wing unit (4) and which support the wings as well as fuel feeding devices (34) and in particular aircraft, the wing units of which are swept back in a pronounced manner in the form of delta wings, characterised in that - the wing unit (4) is provided between the front spar (8) and ribs (9, 9') which adjoin each other in the area of the wing root (6) with receiving spaces (12) which are accessible from the wing nose (10) for accommodating prefilled fuel tanks (14), in that - interacting guide components (16; 17) are provided at the ribs (9, 9') which are adjacent to each other and the front spar (8) of the wing (4) and the fuel tanks (14) and - for the automatic locking of the tanks (14) in their final slide-in position or for releasing the tanks from the wing nose (10) by releasable locking devices (29, 30, 32) via operating devices (38).</p> |
