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Telescopic rotor and aircraft based on rotor

An aircraft and rotor technology, applied in the field of aircraft, can solve the problem of large space occupation, achieve the effect of easy operation, improve the ability to adapt to various complex environments, and improve diversity and portability

Pending Publication Date: 2018-08-14
LUOYANG INST OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The aircrafts in the prior art are all rotorcrafts driven by the motor for lift, and the rotors are mostly fixed structures, it is difficult to adjust the diameter of the rotors during flight, and it takes up a lot of space when stored.

Method used

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  • Telescopic rotor and aircraft based on rotor
  • Telescopic rotor and aircraft based on rotor
  • Telescopic rotor and aircraft based on rotor

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Embodiment Construction

[0034] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present invention, but not all of them.

[0035] A retractable rotor such as Figure 1 to Figure 12 As shown, it includes a rotor shaft 3, a chassis 1, a main drive motor 5, and a drive disc 2 driven by the main drive motor 5 to rotate. The drive disc 2 is provided with an arc-shaped sliding groove 6, and the chassis 1 is provided with a T-shaped sliding groove. 7. The head end of the rotor shaft 3 is provided with a flange 4 that can slide in the arc-shaped sliding groove 6 and the T-shaped sliding groove 7 at the same time without falling out. The main driving motor 5 is installed in the center of the chassis 1, and the positioning shaft 13 of the main driving motor 5 passes through the positioning hole of the chassis 1 and is connected to the fixed coupli...

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Abstract

The invention discloses a telescopic rotor and an aircraft based on the rotor. The rotor comprises a rotor shaft, a chassis, a main drive motor and a drive disc which is driven by the main drive motorto rotate, wherein an arc-shaped slide slot is formed in the drive disc; a T-shaped slide slot is formed in the chassis; and the front end of the rotor shaft can be equipped with a flange which can simultaneously slide in the arc-shaped slide slot and the T-shaped slide slot without drop. On the premise of guaranteeing requirements of flight, the flange at the front end of the rotor shaft bears tangential force in the rotor shaft ring through the arc-shaped slide slot in the drive disc when the main drive motor drives the drive disc to rotate, so that power is provided for simultaneously sliding the rotor shaft in the arc-shaped slide slot and the T-shaped slide slot, and therefore, the rotor shaft linearly moves in the T-shaped slide slot, and the rotor shaft is controlled to extend andshrink relative to the drive disc. Radial extension and shrinkage of the rotor shaft can change ascending force and descending force of the aircraft, so that the aircraft can fly in a complex environment, and therefore, obstacle avoiding ability and reachable range are greatly increased.

Description

technical field [0001] The invention belongs to the technical field of aircraft, and in particular relates to a retractable rotor and an aircraft based on the rotor. Background technique [0002] With the development of society, the application of aircraft is becoming more and more extensive. It can carry a variety of loads such as cameras, fire extinguishers, etc., and can also carry measuring instrument loads for high-altitude detection or high-altitude object throwing. It is widely used in agriculture, entertainment, detection, meteorology, Rescue and other fields. [0003] The aircrafts in the prior art are rotorcrafts driven by motors for lift force, and the rotors are mostly fixed structures, so it is difficult to adjust the diameter of the rotors during flight, and they take up a lot of space when they are stored. Contents of the invention [0004] The purpose of the present invention is to provide a retractable rotor and an aircraft based on the rotor, which can e...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C11/00B64C11/46
CPCB64C11/003B64C11/46
Inventor 朱德荣党保华郑强张天宇王称意张晓俊张泓兴
Owner LUOYANG INST OF SCI & TECH
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