Aerodynamically shaped, active dragging body

摘要

Aerodynamically shaped, active dragging body (01), by means of a parachute (31) of a driven aircraft schleppbar by the air is at least with a in its vertical and horizontal longitudinal plane curved fuselage (02) with a unit chamber (09), in the at least one power supply (29) and a control device (28) are arranged, and a load chamber (10) as well as with two in the rear part of the hull (02) arranged bearing surfaces (03) and a tail fin (04) with in each case by the control device (28) adjustable rudders (05, 06) and with a coupling (30) for the towing cable (31), characterised in that the fuselage (02) in its transverse plane (15) as triangular, wherein two upper corners (16) on the upper side (18) of the hull (02) and a lower corner (17) on the underside (19) of the hull (02), and wherein the hull (02) in its vertical longitudinal plane only on the upper side (18) is curved and on the underside (19) is straight, and each of the two bearing surfaces (03) into a small and a large segment (07, 08) is divided, wherein the small segment (07), pointing downwards in the region of the lower corner (17) on the fuselage (02) and the large (08) segment facing upwardly to the first segment (07) is connected and each of said small segment (07) a further load chamber (11) comprises.