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A Piezoelectric Energy Harvester for Local Aeroelastic Vibration of Airfoil Pit

A technology of aeroelasticity and vibration pressure, which is applied in the direction of piezoelectric effect/electrostrictive or magnetostrictive motors, electrical components, machines/engines, etc., which can solve the problem of low endurance of airfoil aircraft

Active Publication Date: 2022-08-02
SHANDONG UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to solve the problem of the low endurance of the airfoil aircraft, the present invention provides an airfoil aircraft by fully utilizing the wing vibration energy caused by the environment during the flight according to the structural characteristics of the wing of the airfoil aircraft and the vibration characteristics of the wing during flight. The local aeroelastic vibration piezoelectric energy harvester of the wing surface pit and the technical solution to realize the independent energy supply of the airfoil aircraft, so that the originally dissipated energy can be recovered and reused

Method used

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  • A Piezoelectric Energy Harvester for Local Aeroelastic Vibration of Airfoil Pit
  • A Piezoelectric Energy Harvester for Local Aeroelastic Vibration of Airfoil Pit
  • A Piezoelectric Energy Harvester for Local Aeroelastic Vibration of Airfoil Pit

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Embodiment Construction

[0020] combine figure 1 and figure 2 The embodiment of the device is described. The device is composed of three parts: movement, torsion, and generation of piezoelectric vibrators in airfoil pits. The specific moving parts include: linear sliding guide 7, slider 14, U-shaped baffle 3, telescopic Spring 4 and other structures; specific torsion parts include: wing 10, rotating shaft 8, rolling bearing 11, 90° torsion spring 6 and other structures; specific airfoil pit vibration power generation parts include: flexible support layer 901, flexible piezoelectric layer 902, mass block 903, energy storage circuit and other structures. Its connection structure is as follows: the linear sliding guide 7 is fixed on the base 1, the slider 14 is placed on the track of the linear sliding guide 7, the L-shaped card plate 2 fixes the U-shaped baffle 3 on the base 1, and one end of the telescopic spring 4 is Connect to the U-shaped baffle 3 and one end to the bearing cover 13 . The bearin...

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Abstract

The invention discloses a local aeroelastic vibration piezoelectric energy harvester of airfoil pits, which relates to the fields of clean energy and piezoelectric power generation. The invention consists of a base, an L-shaped clamping plate, a U-shaped baffle, a telescopic spring, a strip baffle, a 90° torsion spring, a linear sliding guide rail, a rotating shaft, a pit vibrator, a wing, a bearing, a bearing seat, and a bearing cover. And the slider is composed of three parts: the moving part, the torsion part and the airfoil pit vibrator power generation part. The moving part and the torsion part realize the pitch vibration form of the airfoil structure flutter under the wind speed. The airfoil structure generates aeroelastic vibration under the excitation of wind flow; then the wall dimples generate local aerodynamic force and inertial force, so that the dimples generate local vibration, and the aeroelastic vibration energy is converted into electrical energy through the piezoelectric vibrator of the airfoil dimples . The device converts the aeroelastic vibration energy generated when the airfoil structure flies in the air into electrical energy, and provides a good solution for improving the endurance of the airfoil aircraft.

Description

technical field [0001] The invention relates to the field of clean energy and piezoelectric power generation, in particular to a local aeroelastic vibration piezoelectric energy harvester of airfoil pits. Background technique [0002] In recent years, small airfoil vehicles (UAVs) have been widely used in aerial photography, detection, reconnaissance, rescue, etc., and also have important application value and strategic significance in the fields of civilian and military products, and have become a hot spot of scientific and technological development at home and abroad. Research institutions in various countries are committed to the research of small airfoil aircraft, and lightweight, automated and intelligent designs emerge in an endless stream. However, the current problems of endurance of small airfoil aircraft and the continuous energy supply of airborne electronic equipment are the key factors restricting the development of aircraft. The traditional energy supply method...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F03G7/08H02N2/18
CPCF03G7/08H02N2/186
Inventor 宋汝君于蓬勃张磊安侯成伟张慧荣杨先海
Owner SHANDONG UNIV OF TECH