English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Tools annual

Global: Zendy Free Plan

Global: Zendy Tools monthly

Global: Zendy Plus monthly

Buffer performance system or the resistance force of a landing gear mechanical structure is one of the key points for aircraft landing gear design as not only does it provide structural strength but it also ensures smooth landing and a reduction of fuel consumption. This paper investigates the possibility of improving the effectiveness of the buffer performance of a landing gear with a new metering pin design. The shape of the metering pin inside the shock absorber affects directly the buffer absorption efficiency and buffer absorption power. The objective of this research is to gather previous data of existing shock absorbers, analyse its influence throughout different parameters and come up with a new possible improved metering pin design to determine how the efficiency is affected. A new ideal approach to investigate the impact of a new metering pin device on shock absorption efficiency of a landing gear is proposed. Keywords—Buffer performance; metering pin; shock absorber; efficiency; landing gear.

Research on Landing Gear Metering Pin and Analysis of its Impact on the Buffer Performance