Aircraft with replaceable protective cover

A technology for an aircraft and a cover body, applied in the field of aircraft, can solve the problems of inconvenient replacement, damaged propellers, difficult to repair, etc., and achieve the effect of firm structure and convenient operation

Inactive Publication Date: 2017-01-18
SHANGHAI XPARTNER ROBOTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Its specific disclosed structure does not include protective measures, which may cause damage to the propeller when encountering special conditions during flight
[0005] Even for some UAVs with protective nets, by adding incomplete fan-shaped propeller lower protective nets, they all adopt an integrated design with the arm, which is not easy to replace
[0006] The other part of the aircraft protective net is mostly integrated with the fuselage or fixed by bonding. Once damaged in flight, it will be difficult to repair
Moreover, the flight protection net has a great influence on the airflow, and the use of the adhesive protection net cannot be conveniently selected and replaced according to the use situation or shape requirements
[0007] Therefore, there is a lack of a protective cover that can effectively protect the blades in the duct of the aircraft and is convenient for replacement in the prior art.

Method used

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  • Aircraft with replaceable protective cover
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Examples

Experimental program
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Effect test

Embodiment Construction

[0043] as the picture shows, figure 1 It is a structural schematic diagram of the present invention, figure 2 It is a structural schematic diagram of a circular cover body not installed in the present invention, an aircraft with a replaceable protective cover, comprising: a fuselage 1, the fuselage 1 has a duct 2, and the duct 2 is provided with a propeller 4, and the duct 2 It is a tubular structure, wherein a plurality of slots 21 are provided between the end surface and the inner wall of the duct 2, and a plurality of snap keys 51 are matched on the outer edge of a circular cover body 5; each snap key 51 is matched and embedded in a slot 21. The circular cover body 5 is installed in the card slot 21 through the card key 51, and the structure of the card connection facilitates disassembly and replacement operations under the premise of ensuring stability.

[0044] Further, a pillar is installed vertically in the side wall of each duct 2, and the pillar can adopt a polygona...

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PUM

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Abstract

The invention discloses an aircraft with a replaceable protective cover. The aircraft comprises an aircraft body, the aircraft body is provided with a duct, and the duct is internally provided with an airscrew, wherein a plurality of clamping grooves are arranged between the end face and the inner wall of the duct, and a plurality of clamping keys are matched on the outer edge of a round cover body; each clamping key is matched and embedded into the clamping groove. Compared with the prior art, the aircraft with the replaceable protective cover effectively solves the problem of lack of a firm-structure protective cover capable of being conveniently replaced in the prior art, the round cover body is fixed through the clamping groove between the duct and the aircraft body, the round cover body is dismantled only by rotating while the airscrew in the duct is protected, and the operation is quite convenient.

Description

technical field [0001] The invention discloses an aircraft, in particular to an aircraft with a replaceable protective cover. Background technique [0002] The protective net of the aircraft is mainly used to protect the propeller. During the operation, it can avoid the damage to personnel caused by high-speed rotation, so the protective net is very important. [0003] Some unmanned aerial vehicles in the prior art do not have any protective measures for the flying propellers, which cannot provide effective protection for the safety of flight. [0004] Application number: 201010220017.X's invention application discloses a small electric ducted propeller intelligent unmanned aerial vehicle. The aircraft is composed of a duct enclosure, a bracket, a coaxial counter-rotating propeller, a fairing, a battery, an electric motor, a drive control circuit and a microcontroller. The appearance of the body is dish-shaped, and a duct enclosure is added outside the rotor, which elimina...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C1/06B64C39/00B64D29/04
CPCB64D29/04B64U30/299B64U50/19B64U10/14B64U30/294B64U20/70
Inventor 恽为民叶鹏庞作伟
Owner SHANGHAI XPARTNER ROBOTICS
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