Servo bat-wing aircraft

An aircraft and bat wing technology, applied in the field of aircraft design, can solve problems such as narrow detection range, hidden flight safety hazards, and low ranging accuracy, and achieve the effects of improving energy utilization efficiency, increasing light-receiving area, and high ranging accuracy.

Pending Publication Date: 2022-07-08
BEIHANG UNIV
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0004] In addition, most of the existing flapping-wing aircraft are designed to imitate insects and birds, and their flight efficiency is relatively low, which is not conducive to prolonging the endurance time. They can only perform reconnaissance missions during the day, and cannot effectively identify them when flying at night. Surrounding obstacles, there is a greater flight safety hazard
Although some obstacle avoidance devices have been used, they are generally developed based on ultrasonic ranging technology or infrared ranging technology. Ultrasonic waves are not limited by visible light, and batwing aircraft will not be disturbed by propeller vibration, but the ranging accuracy is low. , the detection range is narrow, and it is greatly affected by windy weather; the infrared light ranging accuracy is high, and the range can reach tens of meters, but it cannot work in an environment where there is no visible light at all. Therefore, neither of the two ranging methods can achieve all-weather obstacle avoidance flight

Method used

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Embodiment Construction

[0032] In order to understand the above objects, features and advantages of the present invention more clearly, the present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments. It should be noted that the embodiments of the present invention and the features in the embodiments may be combined with each other under the condition of no conflict.

[0033] Many specific details are set forth in the following description to facilitate a full understanding of the present invention. However, the present invention can also be implemented in other ways different from those described herein. Therefore, the protection scope of the present invention is not limited by the specific details disclosed below. Example limitations.

[0034] A servo bat-wing aircraft, comprising a bat-wing aircraft body 1 and a photovoltaic energy system 2 installed on the bat-wing aircraft body 1, an intelligent obstacle avoidance and flight co...

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Abstract

The invention belongs to the field of aircraft design, and discloses a servo bat-wing aircraft which comprises a bat-wing aircraft body, a photovoltaic energy system, an intelligent obstacle avoidance and flight control system, a communication link system and a task load. The servo-type bat-wing aircraft can realize a task mode of long-term servo and intermittent reconnaissance, namely, the servo-type bat-wing aircraft is hidden on a roof in the daytime, collects energy by utilizing a photovoltaic energy system and reconnaissance is carried out on a specified area at night, so that the limitation of frequent recovery, charging and discharging of a traditional unmanned aerial vehicle is broken through; the flapping of the flexible bat wings during flight is higher in efficiency and lower in noise compared with a fixed wing and a rotor wing, and hidden reconnaissance is more facilitated; the intelligent obstacle avoidance and flight control system has the advantages of ultrasonic wave and infrared light distance measurement, and can assist the aircraft to complete night obstacle avoidance flight; the communication link system supports a Beidou satellite communication function, so that the instruction and image transmission of the aircraft is not limited by distance any more.

Description

technical field [0001] The invention belongs to the field of aircraft design, and in particular relates to a servo bat-wing aircraft. Background technique [0002] The existing flapping-wing aircraft has the advantages of low flight noise and strong concealment, and can be used for low-altitude reconnaissance. However, due to the limited capacity of the mounted battery, reconnaissance tasks can only be performed within a small radius centered on the ground station, and both release and recovery must rely on manual operations, and do not have the ability to obtain energy autonomously. Each reconnaissance mission After completion, it needs to be returned for charging and maintenance, which makes the ground support work more cumbersome. [0003] The Chinese patent application with publication number CN113002772A discloses a flap-integrated imitation bat flapping-wing aircraft, which uses a DC brushless motor unit as a driving mechanism, and reduces the rotational speed and inc...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/02B64D27/24
CPCB64C33/02B64D27/24B64D2211/00B64U10/40B64U50/19B64U2101/00Y02T50/60
Inventor 张良马东立杨穆清刘天泽关皓孙福东
Owner BEIHANG UNIV
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