A simulation of the fatigue life of light aircraft glass fibre-reinforced composites landing gear

Chen, P. W.; Huang, Woei-Kae

doi:10.1179/1432891715z.0000000001947

Materials Research Innovations

2015

DOI: 10.1179/1432891715z.0000000001947

|View full text |Cite

A simulation of the fatigue life of light aircraft glass fibre-reinforced composites landing gear

P. W. Chen

Woei-Kae Huang

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2022

Publication Types

Select...

Article1

Relationship

Self Cite0

Independent1

Authors

Journals

Cited by 1 publication

(1 citation statement)

References 3 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Ti-10V-2Fe-3Al alloy has the highest safety factor and minimum stress value compared to other materials. Chen and Huang [11] analyzed the material of the landing gear in the Ansys software by selecting a glass fiber-reinforced composite.…”

mentioning

confidence: 99%

A Novel Design and Structural Analysis of Spring Landing Gear for Unmanned Air Vehicles

Gök

Cihan

2022

Hittite Journal of Science and Engineering

View full text Add to dashboard Cite

Aircraft are subjected to an impact load during landing. This situation becomes more important for unmanned aerial vehicles that are remotely controlled and must serve in extreme conditions. Because the landing gear should absorb this impact load as much as possible and prevent damage to the unmanned aerial vehicle body and its components. In this study, a landing gear design has been developed for unmanned aerial vehicles that can absorb more impact load during landing. Numerical analyzes were performed to determine the fatigue life and the maximum impact load that the developed design can withstand. In addition, a conventional landing gear was modeled and the results were compared. The properties of 7075-T6 Aluminum alloy were used as the landing gear material. As a result of the finite element analyzes made with Ansys software, it has been understood that the newly designed landing gear can absorb more energy than the conventional landing gear. It has also been determined that it can be used at values up to 3700N impact load.

show abstract

mentioning

confidence: 99%

A Novel Design and Structural Analysis of Spring Landing Gear for Unmanned Air Vehicles

Gök

Cihan

2022

Hittite Journal of Science and Engineering

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

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.

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.

A simulation of the fatigue life of light aircraft glass fibre-reinforced composites landing gear

Cited by 1 publication

References 3 publications

A Novel Design and Structural Analysis of Spring Landing Gear for Unmanned Air Vehicles

A Novel Design and Structural Analysis of Spring Landing Gear for Unmanned Air Vehicles

Contact Info

Product

Resources

About