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Take-off and landing method of floating type air mobile airport platform carrying fixed-wing aircraft

A fixed-wing and platform technology, applied in the direction of remote control aircraft, aircraft parts, rotorcraft, etc., can solve the problems of increased air resistance, reduced load weight, increased take-off weight of the rotor group, etc., to achieve the effect of flexible deployment and convenient maintenance

Pending Publication Date: 2021-11-30
BEIHANG UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the disadvantage of this method is also very obvious. The addition of the rotor group greatly increases the take-off weight, resulting in a sharp decrease in the load weight of the aircraft in this configuration, which also leads to the fact that the aircraft in this configuration cannot be made very large, and the aircraft switches After entering the fixed-wing mode, the rotor group becomes a serious burden, which will also lead to a sharp increase in air resistance

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  • Take-off and landing method of floating type air mobile airport platform carrying fixed-wing aircraft
  • Take-off and landing method of floating type air mobile airport platform carrying fixed-wing aircraft
  • Take-off and landing method of floating type air mobile airport platform carrying fixed-wing aircraft

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Embodiment Construction

[0046] The present invention will be further described in detail below with reference to the accompanying drawings and embodiments.

[0047] The invention provides a take-off and landing method for a fixed-wing aircraft mounted on a floating air mobile airport platform, which enables the fixed-wing aircraft to take off and land without using the airport runway and without the need for a rotor group installed by itself. The present invention can not only assist in take-off and landing for manned fixed-wing unmanned aerial vehicles, but also can assist in take-off and landing for fixed-wing aircraft by enlarging the floating aerial mobile airport platform, and the docking device can also be updated and iterated at a later stage.

[0048] The take-off and landing method described, such as figure 1 shown, the specific steps are as follows:

[0049] Step 1. Mount the fixed-wing aircraft on the floating air mobile airport platform;

[0050] like figure 2 As shown in the figure, ...

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Abstract

The invention discloses a take-off and landing method of a floating type air mobile airport platform carrying a fixed-wing aircraft, and belongs to the field of aircraft design and control. Particularly, to a floating type air mobile airport platform adopting a four-rotor aircraft, and a large-area magnetic type docking device and a GD30 differential satellite navigation module used for guiding following are carried on the platform; the magnetic type docking device is used for attracting an iron sheet below the fixed-wing aircraft; the fixed-wing aircraft is carried on a ground section platform, and normally takes off in a transition period, and the platform is separated from the fixed-wing aircraft and returns to the ground; then, when the fixed-wing aircraft executes the task and returns, the platform takes off and follows the fixed-wing aircraft; and finally, the fixed-wing aircraft gradually slows down and is in butt joint with the platform, and the platform carries the shut-down fixed-wing aircraft to land to a designated place. The docking process is positioned through the GD30 differential satellite navigation module, the fixed-wing aircraft can take off and land at any place, and deployment is more flexible and maneuvering.

Description

technical field [0001] The invention belongs to the field of aircraft design and control, in particular to a take-off and landing method for a floating-type air mobile airport platform carrying a fixed-wing aircraft. Background technique [0002] Fixed-wing aircraft, referred to as aircraft, generally refers to a heavier-than-air aircraft that is driven by a power device to generate thrust or pull when moving forward, and lift is generated by fixed wings on the fuselage, flying in the atmosphere. Unmanned aerial vehicle is referred to as unmanned aerial vehicle, English full name is Unmanned Aerial Vehicle, abbreviated as UAV. manned aircraft. The drone industry has developed rapidly since the beginning of the 21st century. Various types of drones emerge in an endless stream and are widely used in various scenarios. Among them, consumer-grade UAVs are mainly quad-rotor UAVs, while fixed-wing UAVs are still dominated by fixed-wing because of their significant advantages of ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D5/00B64D47/00B64C27/08B64C39/02B64F1/02
CPCB64D5/00B64D47/00B64C27/08B64C39/024B64F1/0297B64U10/10B64U10/13B64U2101/00
Inventor 王松骈学超付仁皓毛浩谢嘉轩赵亦涵张楠
Owner BEIHANG UNIV