Xiangbing Wu , Jieliang Zhao , Tonghui Fan , Xuemei Chen , Junlan Li , Wenzhong Wang , Shaoze Yan
{"title":"受蜜蜂腹部启发的航空航天飞行器变形鼻锥集成变形锁定设计","authors":"Xiangbing Wu , Jieliang Zhao , Tonghui Fan , Xuemei Chen , Junlan Li , Wenzhong Wang , Shaoze Yan","doi":"10.1016/j.ast.2025.111023","DOIUrl":null,"url":null,"abstract":"<div><div>Active adjustment of aerodynamic shape by morphing mechanisms is an effective means to improve the environmental adaptability and maneuverability of aerospace vehicles. In this paper, inspired by the deformation mechanism of honeybee abdomen, a series-parallel morphing nose cone (MNC) mechanism that can realize deformation motions in four levels (2 levels of stretching and 2 levels of bending) and two directions (<em>z</em>-direction and <em>x</em>-direction) is designed. A deformation-locking integrated design method is innovatively proposed to achieve the locking of MNC at any position. Based on the screw theory, the branch-chain synthesis and degree of freedom (DOF) analysis of the mechanism are completed. The kinematics and dynamics models of the proposed mechanism are constructed, and its motion characteristics and working space are analyzed. Aiming at the problem with the heavier driving burden in the starting stage, the driving torque in the initial stage was designed to be compensated. Compensated start-up torque is significantly reduced, and the torque curve is smoother. Finite element analysis confirmed that the design of the locking chains and the force self-locking mechanism greatly enhances the axial stiffness of the MNC. A functional prototype of MNC is manufactured and the deformation experiments are conducted. The prototype can achieve eight independent morphing configuration processes and stable locking at any position, with a maximum bending angle of 19.65°, a maximum stretching of 79.55 mm, a maximum stretching rate of 14.75 %, and a motion deviation of <3 %.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"168 ","pages":"Article 111023"},"PeriodicalIF":5.8000,"publicationDate":"2025-09-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Morphing nose cone with integrated deformation-locking design for aerospace vehicle inspired by honeybee abdomen\",\"authors\":\"Xiangbing Wu , Jieliang Zhao , Tonghui Fan , Xuemei Chen , Junlan Li , Wenzhong Wang , Shaoze Yan\",\"doi\":\"10.1016/j.ast.2025.111023\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Active adjustment of aerodynamic shape by morphing mechanisms is an effective means to improve the environmental adaptability and maneuverability of aerospace vehicles. In this paper, inspired by the deformation mechanism of honeybee abdomen, a series-parallel morphing nose cone (MNC) mechanism that can realize deformation motions in four levels (2 levels of stretching and 2 levels of bending) and two directions (<em>z</em>-direction and <em>x</em>-direction) is designed. A deformation-locking integrated design method is innovatively proposed to achieve the locking of MNC at any position. Based on the screw theory, the branch-chain synthesis and degree of freedom (DOF) analysis of the mechanism are completed. The kinematics and dynamics models of the proposed mechanism are constructed, and its motion characteristics and working space are analyzed. Aiming at the problem with the heavier driving burden in the starting stage, the driving torque in the initial stage was designed to be compensated. Compensated start-up torque is significantly reduced, and the torque curve is smoother. Finite element analysis confirmed that the design of the locking chains and the force self-locking mechanism greatly enhances the axial stiffness of the MNC. A functional prototype of MNC is manufactured and the deformation experiments are conducted. The prototype can achieve eight independent morphing configuration processes and stable locking at any position, with a maximum bending angle of 19.65°, a maximum stretching of 79.55 mm, a maximum stretching rate of 14.75 %, and a motion deviation of <3 %.</div></div>\",\"PeriodicalId\":50955,\"journal\":{\"name\":\"Aerospace Science and Technology\",\"volume\":\"168 \",\"pages\":\"Article 111023\"},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2025-09-30\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Science and Technology\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1270963825010867\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825010867","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Morphing nose cone with integrated deformation-locking design for aerospace vehicle inspired by honeybee abdomen
Active adjustment of aerodynamic shape by morphing mechanisms is an effective means to improve the environmental adaptability and maneuverability of aerospace vehicles. In this paper, inspired by the deformation mechanism of honeybee abdomen, a series-parallel morphing nose cone (MNC) mechanism that can realize deformation motions in four levels (2 levels of stretching and 2 levels of bending) and two directions (z-direction and x-direction) is designed. A deformation-locking integrated design method is innovatively proposed to achieve the locking of MNC at any position. Based on the screw theory, the branch-chain synthesis and degree of freedom (DOF) analysis of the mechanism are completed. The kinematics and dynamics models of the proposed mechanism are constructed, and its motion characteristics and working space are analyzed. Aiming at the problem with the heavier driving burden in the starting stage, the driving torque in the initial stage was designed to be compensated. Compensated start-up torque is significantly reduced, and the torque curve is smoother. Finite element analysis confirmed that the design of the locking chains and the force self-locking mechanism greatly enhances the axial stiffness of the MNC. A functional prototype of MNC is manufactured and the deformation experiments are conducted. The prototype can achieve eight independent morphing configuration processes and stable locking at any position, with a maximum bending angle of 19.65°, a maximum stretching of 79.55 mm, a maximum stretching rate of 14.75 %, and a motion deviation of <3 %.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.