Aircraft provided with low-resistance hanging wall

A low-resistance, aircraft technology, applied in the field of aircraft, can solve the problems of unable to increase flight speed, unable to reduce air resistance, unable to effectively ensure assembly strength, etc., to achieve the effect of strengthening installation points, reducing air resistance, and ensuring assembly strength

Pending Publication Date: 2021-02-05
深圳市蜉飞科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The problem is that because the power system provides power and lift to the aircraft through the propeller, the assembly strength and ai

Method used

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  • Aircraft provided with low-resistance hanging wall
  • Aircraft provided with low-resistance hanging wall
  • Aircraft provided with low-resistance hanging wall

Examples

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Example Embodiment

[0023]The following specific examples illustrate the implementation of the present invention. Those skilled in the art can easily understand other advantages and effects of the present invention from the content disclosed in this specification.

[0024]It should be noted that the structure, ratio, size, etc. shown in the drawings of this specification are only used to match the content disclosed in the specification for people familiar with this technology to understand and read, and are not used to limit the implementation of the present invention. Therefore, it has no technical significance. Any structural modification, proportional relationship change, or size adjustment should still fall within the scope of the present invention without affecting the effects and objectives that can be achieved by the present invention. The technical content can cover the range. At the same time, terms such as "upper", "lower", "left", "right", "middle" and "one" cited in this specification are only...

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Abstract

The invention provides an aircraft provided with low-resistance hanging walls, which comprises an aircraft body, wings, an empennage, a power device and at least two hanging walls, the two hanging walls are arranged on the lower surfaces of the wings positioned on two sides of the center line direction of the aircraft body, a left embedding groove is formed in the lower surface of a left wing body, and a right embedding groove is formed in the lower surface of a right wing body; each hanging wall comprises a shell with a lower opening cavity and conical arc cylinders extending out along the two ends of the shell, each shell comprises a shell body part and a windward side shell part arranged at the top of the shell body, the upper half part of each conical arc cylinder is integrally connected with the shell body part, and the lower half part of each conical arc cylinder extends out of the opening of the lower opening cavity of the shell body; one part of the fasteners respectively penetrate through the glass fiber plate and the windward side shell part on the same side of the left wing body and are locked in the lock hole of the left embedding groove, and the other part of the fasteners respectively penetrate through the glass fiber plate and the windward side shell part on the same side of the right wing body and are locked in the lock hole of the right embedding groove. Compared with the prior art, air resistance generated by wall hanging is reduced, and the flight speed is increased.

Description

technical field [0001] The invention belongs to the technical field of flight equipment, and relates to an aircraft equipped with a low-resistance hanging wall. Background technique [0002] At present, with the development of unmanned aerial vehicles, the requirements for the stability and durability of small aircraft are increasing day by day. [0003] In the prior art, there is a kind of aircraft, comprising fuselage, wing, empennage, power plant, wing comprises the left wing body that is arranged on the left side of fuselage and the right wing body that is arranged on the right side of fuselage, and empennage is arranged on the fuselage rear end. The existing problem is: because the power system provides power and lift to the aircraft through the propeller, the assembly strength and air resistance cannot be effectively guaranteed during the flight of the aircraft, resulting in the inability to increase the flight speed. [0004] For this reason, the present invention p...

Claims

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Application Information

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IPC IPC(8): B64C3/36
CPCB64C3/36
Inventor 吴成能
Owner 深圳市蜉飞科技有限公司
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