Kinematic synthesis and mechanism design of a six-bar jumping leg for elastic energy storage and release based on dead points

Du, Qilong; Fan, Jizhuang; Xu, Tian; Cui, Xiulong; Liao, Jinnong; Xu, Weibin; Zhu, Yanhe; Zhao, Jie

doi:10.1016/j.mechmachtheory.2024.105777

Mechanism and Machine Theory

2024

DOI: 10.1016/j.mechmachtheory.2024.105777

|View full text |Cite

Kinematic synthesis and mechanism design of a six-bar jumping leg for elastic energy storage and release based on dead points

Qilong Du,

Jizhuang Fan,

Tian Xu

et al.

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2024

Publication Types

Select...

Article1

Relationship

Self Cite0

Independent1

Authors

Journals

Cited by 1 publication

References 43 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

Flap and Wing Dynamics for a Light Sport Aircraft Analysis Using a Topological Model

Scutaru,

Vlase,

Marin

2024

Applied Sciences

View full text Add to dashboard Cite

This paper presents a more general method to study the dynamic behavior of a planar mechanism with joints. To do this, Graph Theory is used. A topological description is presented based on which a corresponding graph is attached to any mechanism. This method can be used for both kinematic and dynamic study in the same model, and many of the descriptors used in kinematic analysis can also be used for dynamic analysis. As a final result, the motion equations of the studied mechanical system can be obtained. An application is made to a flap and wing control system of a light sport aircraft. The graph associated with the mechanism first used to determine the field of velocities and accelerations of the mechanism elements is then used to obtain the motion equation for the control system. In this way, Graph Theory proves useful for the parallel study of both the kinematic and dynamic study of such problems.

show abstract

Flap and Wing Dynamics for a Light Sport Aircraft Analysis Using a Topological Model

Scutaru,

Vlase,

Marin

2024

Applied Sciences

View full text Add to dashboard Cite

show abstract

scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.

Contact Info

customersupport@researchsolutions.com

10624 S. Eastern Ave., Ste. A-614

Henderson, NV 89052, USA

Blog Terms and Conditions API Terms Privacy Policy Contact Cookie Preferences Do Not Sell or Share My Personal Information

Made with 💙 for researchers

Part of the Research Solutions Family.

Kinematic synthesis and mechanism design of a six-bar jumping leg for elastic energy storage and release based on dead points

Cited by 1 publication

References 43 publications

Flap and Wing Dynamics for a Light Sport Aircraft Analysis Using a Topological Model

Flap and Wing Dynamics for a Light Sport Aircraft Analysis Using a Topological Model

Contact Info

Product

Resources

About