Morphing aircraft with variable swept wings and head deflection

A variant aircraft and aircraft technology, applied in the field of variant aircraft, can solve the problems of uneven streamline of the fuselage and complex configuration of the variant aircraft, and achieve smooth streamline, increase lift, and increase force area. Effect

Pending Publication Date: 2021-12-10
NANJING UNIV OF SCI & TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] This application provides a variant aircraft with variable swept wings and head deflection, which can be used to solve the technical problems that the configuration of the variant aircraft is relatively complex and the streamline of the fuselage is not smooth

Method used

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  • Morphing aircraft with variable swept wings and head deflection
  • Morphing aircraft with variable swept wings and head deflection
  • Morphing aircraft with variable swept wings and head deflection

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Embodiment Construction

[0034] In order to make the purpose, technical solution and advantages of the present application clearer, the implementation manners of the present application will be further described in detail below in conjunction with the accompanying drawings.

[0035] First combine the following figure 1 A possible system architecture applicable to the embodiments of the present application is introduced.

[0036] Please refer to figure 1 , which exemplarily shows a schematic structural diagram of a low-sonic time-axis view of a variant aircraft with variable-sweep wings and head deflection applicable to the embodiment of the present application.

[0037] Such as figure 2 As shown, it is a schematic diagram of the front view structure of a variant aircraft with variable sweep and head deflection provided by the embodiment of the present application at low supersonic speed.

[0038] The variant aircraft with variable swept wing and head deflection provided by the present application ...

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Abstract

The invention provides a morphing aircraft with variable swept wings and head deflection. The morphing aircraft comprises an aircraft head, an aircraft fuselage, a left swept wing, a right swept wing, a head deflection device and a swept wing deflection device. Wherein the head deflection device is arranged between the head of the aircraft and the fuselage of the aircraft; the sweeping wing deflection device is arranged between the left sweeping wing and the right sweeping wing; the head deflection device is used for controlling the aircraft head to deflect; and the sweeping wing deflection device is used for controlling the left sweeping wing and the right sweeping wing to sweep. According to the morphing aircraft, the streamline of the aircraft body is smooth, the deformation mechanism principle is simple and easy to achieve, and the aerodynamic performance of the aircraft in subsonic velocity and low supersonic velocity flight is improved by means of aerodynamic shape changes of the aircraft head and the swept wings.

Description

technical field [0001] The application relates to the technical field of variant flying chess design, in particular to a variant aircraft with variable-sweep wings and head deflection. Background technique [0002] The task required by the aircraft is more complex, and the design is only for a fixed-shaped aircraft. The result of the design must be a trade-off under various working conditions, sacrificing the drag of subsonic flight in order to meet the lift of subsonic flight. That is to say, the aerodynamic characteristics of fixed-wing aircraft with multi-working conditions are not optimal in each speed range. [0003] In order to solve the above problems, the researchers proposed a variant aircraft, which can change the aerodynamic layout of the aircraft according to the changes of the flight environment and flight tasks, and maintain the optimal flight performance, so that the aircraft can perform various tasks at different altitudes and different flight speeds. requir...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/00
CPCB64C39/005B64C39/00
Inventor 吴威涛王明亮梅宇飞郑纯封锋
Owner NANJING UNIV OF SCI & TECH
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