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Aircraft with means for a premature breakdown of the wing vortex pair

机译:具有使机翼涡流对过早损坏的装置的飞机

摘要

For a premature breakdown of a wing vortex pair +/-M behind an aircraft in flight (1) comprising a symmetry plane (7), two wings (3), a fuselage (2) and a horizontal tail plane (HTP) (4), the wing vortex pair +/-M being generated in the area of the tips of the wings (3), having a first spin direction and descending behind the aircraft, an interfering vortex pair -/+P, which is generated between the fuselage (2) and the tips of the wings (3) without merging already in the near field behind the wing (3) with the wing vortex pair +/-M and which has a second spin direction that is opposed to the first spin direction, is retained behind the aircraft (1) in an altitude range of the wing vortices of the wing vortex pair +/-M by adjusting to suitable values the relative circulation and the relative span of the interfering vortex pairs -/+P, each related to the wing vortex pair +/-M. The interfering vortex pair -/+P includes portions of a fuselage vortex pair -/+F, which is generated in the junction area of the wings (3) to the fuselage (2), and a tail plane vortex pair -/+H, which is generated in the area of the wing tips (5) of the horizontal tail plane (4).
机译:为了使飞行中的飞机(1)后面的+/- M机翼涡流对过早损坏,该机翼包括对称平面(7),两个机翼(3),机身(2)和水平尾翼(HTP)(4 ),在机翼(3)的尖端区域产生机翼涡流对+/- M,该涡流对具有一个第一旋转方向并下降到飞机后方,在飞机之间产生干扰涡流对-/ + P。机身(2)和机翼(3)的尖端未在机翼(3)后面的近场中与机翼涡流对+/- M合并并且具有与第一旋转方向相反的第二旋转方向通过将干扰涡流对-/ + P的相对环流和相对跨度调整到适当的值,将它们保持在飞机涡旋对+/- M的涡流高度范围内的飞机(1)的后面。到翼涡对+/- M。干扰涡流对-/ + P包括机身涡流对-/ + F的一部分,该部分在机翼(3)与机身(2)的交界处产生,尾翼涡流对-/ + H在水平尾翼(4)的翼尖(5)的区域中生成。

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