Design and Simulation of Gradient Wind Gliding Bionic Vehicle

One of the important ways to break the endurance bottleneck of aircraft is to apply the flight strategy of albatrosses obtaining energy from gradient wind fields to glide thousands of miles on aircraft. Based on the body characteristics and flight strategy of albatross, a bionic albatross aircraft with bionic shape, aerodynamic layout and control mode is designed. The lift-drag ratio during cruise is 1.13 times that of conventional aircraft, and the maximum lift-drag ratio is 1.31 times that of conventional aircraft. The maximum drag is reduced by 12% and the wing root load is reduced by 35% through wing tip deformation. According to the behavior of albatross flapping its wings from time to time during gliding, the intermittent dynamic gradient wind gliding method is proposed, and the control performance simulation of bionic albatross aircraft is carried out. The results show that the error between the actual flight path and the gradient wind gliding path is less than 5%, and the energy consumption is 51.5% of uniform flight, which verifies the rationality of the intermittent dynamic gradient wind gliding strategy.

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Publication Details

Journal
SHILAP Revista de lepidopterología
Published
2024-10-01
DOI
https://doi.org/10.12132/issn.1673-5048.2023.0248
Primary Topic
Biomimetic flight and propulsion mechanisms
Type
article
Field-Weighted Citation Impact
0.00
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article

Design and Simulation of Gradient Wind Gliding Bionic Vehicle

SHILAP Revista de lepidopterología
Biomimetic flight and propulsion mechanisms
article

Design and Simulation of Gradient Wind Gliding Bionic Vehicle

article en

Abstract

One of the important ways to break the endurance bottleneck of aircraft is to apply the flight strategy of albatrosses obtaining energy from gradient wind fields to glide thousands of miles on aircraft. Based on the body characteristics and flight strategy of albatross, a bionic albatross aircraft with bionic shape, aerodynamic layout and control mode is designed. The lift-drag ratio during cruise is 1.13 times that of conventional aircraft, and the maximum lift-drag ratio is 1.31 times that of conventional aircraft. The maximum drag is reduced by 12% and the wing root load is reduced by 35% through wing tip deformation. According to the behavior of albatross flapping its wings from time to time during gliding, the intermittent dynamic gradient wind gliding method is proposed, and the control performance simulation of bionic albatross aircraft is carried out. The results show that the error between the actual flight path and the gradient wind gliding path is less than 5%, and the energy consumption is 51.5% of uniform flight, which verifies the rationality of the intermittent dynamic gradient wind gliding strategy.

SHILAP Revista de lepidopterología
Suzhou Institute of Nano-tech and Nano-bionics (CN)
Affordable and clean energy
Openalex Percentile: Top 46%
Biomimetic flight and propulsion mechanisms
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