Research on Influence Factors of Landing Gear Retractile Hydraulic System Performance Degradation

Wu Feng Zhu; Zhong Yan; Qing Wei Xin

doi:10.4028/www.scientific.net/AMM.599-601.409

Paper Titles

Pre-Deformed Design of Optical Lenses with Reverse Engineering and Virtual Manufacturing
p.391

Research and Development of a Knowledge-Based System for Blanking Die
p.396

Research on Attitude Singularity Problem of Small Tail-Sitter Aircraft
p.401

Research on CNC Machining System of Directly Driven by Image Based on PMAC
p.405

Research on Influence Factors of Landing Gear Retractile Hydraulic System Performance Degradation
p.409

Research on the Forming Path for Fabricating the Sheet-Metal Part with Non-Horizontal End Face Using CNC Incremental Forming
p.413

Research on the Simulation of NC Milling Program Based on VERICUT Oriented to the Five-Axis Micro-Milling System
p.417

Research on the Stress Uniformity of the High Speed Bearing with Heavy Load in Cold Rolling
p.422

Research on Typical Vibration Accelerations of Wind Wheel Changing with Yaw Angle
p.426

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 599-601Research on Influence Factors of Landing Gear...

Research on Influence Factors of Landing Gear Retractile Hydraulic System Performance Degradation

Abstract:

Simulation model of landing gear hydraulic system is built based on AMESim, several key influence factors of performance degradation of landing gear hydraulic system are analyzed, such as changes of restrictor orifice diameter, initial pressure of accumulator, viscosity and gas percentage of oil , etc. The simulation results bring valuable reference to aircraft maintenance.

You might also be interested in these eBooks

Frontiers of Manufacturing Science and Measuring Technology IV

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 599-601)

Pages:

409-412

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.599-601.409

Citation:

Cite this paper

Online since:

August 2014

Authors:

Wu Feng Zhu*, Zhong Yan, Qing Wei Xin

Keywords:

AMEsim, Flight Line Maintenance, Hydraulic System, Landing Gear, Simulation

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Jun Li, Zhan-qiang Luo. Simulation of hydraulic system pressure pulse simulator based on AMESim, Machine Tool and Hydraulics. 2011. 07: 39(14), 106-109.

Google Scholar

[2] Yafeng Wu, Jun Guo. Appliance and research on simulation technology of aircraft hydraulic system , Technology Journal of Shen Yang University. 2007. 08, 29(04), 368-371.

Google Scholar

[3] Wufeng Zhu. Aircraft mechanical system . Naval Aeronautical Engineering Insititute QingDao Campus Publisher. 2010. 05.

Google Scholar

[4] Qiang Ding. Hydraulic component design library, Special subject teaching of Shi Guan AMESim hydraulic and pneumatic system and component design. 2007. 01.

Google Scholar

[5] Yongling Fu, Qi Haitao. Instance course of LMS Imagine Lab AMESim system model building and simulation. 2011. 07.

Google Scholar