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Novel wing

A new type of wing technology, applied in the aviation field, can solve problems such as long distances, achieve the effects of large lift, shorten the take-off distance of the aircraft, and reduce the footprint

Inactive Publication Date: 2019-01-25
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

But this kind of wing structure has a defect, that is, it needs a long distance when starting, because it takes a process to increase the speed of the aircraft from zero to take-off speed, and this process depends on the lift generated by the wing from zero to take-off The time required for the desired magnitude of lift

Method used

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Embodiment Construction

[0010] The present invention is described in detail in conjunction with accompanying drawing now, a kind of novel wing, comprises wing body 1, supporting plate 2, motor 3 and propeller 4.

[0011] The wing body 1 is the same as a conventional wing; the supporting plate 2 is placed behind the wing body 1 and connected to the wing body 1, and the plane where the supporting plate 2 is located is lower than the lowest point on the upper surface of the wing; After the motor 3 and the propeller 4 are installed on the supporting plate 2, the plane where the propeller 4 is located is equal to the lowest point on the upper surface of the wing. There are multiple motors 3, all of the same type, placed side by side on the supporting plate 2; the number of the propellers 4 is corresponding to the number of the motors 3, connected to the motors 3 respectively, placed behind the wing body 1, and attached The upper surface of the wing body 1 and the propeller 4 are flat with the lowest point...

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Abstract

The invention relates to a novel wing, belonging to the aeronautical field, comprising a wing body, a support plate, an electric motor and a propeller. The wing body is identical to a conventional wing. The support plate is arranged behind the wing body and connected with the wing body, and the plane of the support plate is lower than the lowest point of the upper surface of the wing; after mounting the motor and propeller on the pallet, the plane of the propeller is flat with the lowest point of the upper surface of the wing. The motors have a plurality of identical models and are arranged side by side on a support plate. The number of the propellers corresponds to the number of the motors, is respectively connected with the motors, is arranged behind the wing body, is close to the wing body, and the upper surface of the propellers is flat with the lowest point of the upper surface of the wing. The novel wing of the invention is improved on the conventional wing structure, so that theairflow speed flowing through the upper surface of the wing is faster, and the wing can generate greater lift force, thereby greatly shortening the takeoff distance of the aircraft and reducing the area occupied by the airport.

Description

technical field [0001] A novel wing belongs to the field of aviation, and in particular relates to a wing. Background technique [0002] The reason why a traditional wing can generate lift is that the paths on the upper and lower surfaces of the wing are different. The airflow velocity flowing through the upper surface is faster, while the airflow velocity on the lower surface is slower than that on the upper surface, thereby generating lift and making the aircraft Able to soar high into the sky. But this kind of wing structure has a defect, that is, it needs a long distance when starting, because it takes a process to increase the speed of the aircraft from zero to take-off speed, and this process depends on the lift generated by the wing from zero to take-off The time required for the desired magnitude of lift. If the lift of the wing can be greatly improved, the starting distance of the aircraft will be greatly shortened. Contents of the invention [0003] The soluti...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/10B64C3/36
CPCB64C3/10B64C3/36
Inventor 王志成党先红李玉龙
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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