Aerodynamic layout of a high-altitude long-endurance aircraft with twin fuselages, high rear wings and three surfaces

A technology of aerodynamic layout and long endurance, applied in aircraft, motor vehicles, transportation and packaging, etc., can solve problems such as adverse interference of rear wings, and achieve the effect of improving overall aerodynamic characteristics, increasing flight height, and improving aerodynamic characteristics.

Active Publication Date: 2020-02-07
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The layout consists of two wings, the rear wing favorably interferes with the front wing, whereas the front wing interferes negatively with the rear wing

Method used

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  • Aerodynamic layout of a high-altitude long-endurance aircraft with twin fuselages, high rear wings and three surfaces
  • Aerodynamic layout of a high-altitude long-endurance aircraft with twin fuselages, high rear wings and three surfaces
  • Aerodynamic layout of a high-altitude long-endurance aircraft with twin fuselages, high rear wings and three surfaces

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Embodiment Construction

[0028] The present invention will be further described below in conjunction with the accompanying drawings.

[0029] In the aerodynamic layout of the aircraft of the present invention, the aircraft adopts a cylindrical cross-section double fuselage 1, a front wing 2 and a rear wing 3 of a larger aspect ratio, a V-shaped support tail 4, a horizontal tail 5 and a turbofan engine 6, such as figure 1 shown.

[0030] Such as figure 2 , image 3 As shown, the axes of the cylindrical cross-section twin fuselages 1 are parallel, including a left and right fuselage 101 and a right fuselage 102 that are left and right symmetrical; Between the quarter point and the third point of the long wingspan, preferably close to the third point. The aspect ratio of the front wing 2 and the rear wing 3 is greater than 7, depending on the specific situation, the larger the aspect ratio, the better.

[0031] Installed in the front half of the double fuselage 1, it is composed of the left end 201 ...

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Abstract

The invention discloses a high-altitude long-endurance aircraft aerodynamic layout using twin fuselages, a high rear wing and three surfaces. The high-altitude long-endurance aircraft aerodynamic layout using the twin fuselages, the high rear wing and the three surfaces adopts the twin fuselages, a front wing, a rear wing, a double-support tail, a horizontal tail and a turbofan engine; the front wing and the rear wing have a difference between the dihedral angle and the cathedral angle so that an adverse inductive effect of a front wing tip vortex on the aerodynamic performance of the rear wing is effectively improved. The rear wing is supported by the double-support tail to be beneficial for improving the integral aerodynamic performance of a twin-surface layout; and the rear wing adopts larger span so that the adverse downwash induction effect of the front wing on the rear wing can be weakened. Meanwhile, a layout in which an the front wing and the rear wing layout have unequal spans is adopted; and as the span of the front wing is short and the span of the rear wing is long, the aerodynamic characteristic of the rear wing is improved. As the horizontal tail and the engine are mounted at the rear edges of the twin fuselages, the aerodynamic characteristic of the rear wing is further improved by using favorable interference of the horizontal tail to the rear wing.

Description

technical field [0001] The invention belongs to the field of aircraft aerodynamic layout design, in particular to an aerodynamic layout of a high-altitude long-endurance aircraft that adopts twin fuselages, high rear wings and three airfoils. Background technique [0002] High-altitude and long-endurance aircraft are generally used to perform strategic / campaign reconnaissance missions. They have persistent intelligence collection and reconnaissance and surveillance capabilities, and can be used as unmanned combat platforms. Therefore, they have become the focus of weapons and equipment development in various countries today. In order to make better use of the platform advantages of high-altitude and long-endurance aircraft in terms of strategic reconnaissance and intelligence collection, the flying height and flight time of such aircraft are constantly increasing, which requires such aircraft to be capable of carrying large loads to achieve high-altitude High-speed, long-las...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/04B64C39/08
CPCB64C39/04B64C39/08
Inventor 蒋崇文林宏渊高振勋李椿萱
Owner BEIHANG UNIV
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