DocumentCode
3162475
Title
Notice of Retraction
Dynamic simulation on retractionextension system of an aircraft
Author
Guoming Ji ; Liang Zhang ; Meng Dong
Author_Institution
Aircraft Dept., Northwestern Polytech. Univ., Xi´an, China
fYear
2011
fDate
8-10 Aug. 2011
Firstpage
3939
Lastpage
3944
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
This paper provides a detailed discussion on the simulation of a landing gear retraction /extension(R/E) system. Section 2 of the full paper presents a general description of the R/E system and its retraction procedure. A mathematical model of the R/E system is introduced by Section 3, which gives a basic idea for numerically modeling this mechanism. Section 4 brings up the procedures for constructing the simulation model in LMS Virtual. Lab Motion and Imagine.Lab AMEsim. After analyzing the simulation results of the kinematics and the hydraulic and pneumatic features in section 5, we draw the conclusion that the R/E system design satisfies the requirements imposed by AFSC DH2-1, and measures should be taken to minimize its internal impact.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
This paper provides a detailed discussion on the simulation of a landing gear retraction /extension(R/E) system. Section 2 of the full paper presents a general description of the R/E system and its retraction procedure. A mathematical model of the R/E system is introduced by Section 3, which gives a basic idea for numerically modeling this mechanism. Section 4 brings up the procedures for constructing the simulation model in LMS Virtual. Lab Motion and Imagine.Lab AMEsim. After analyzing the simulation results of the kinematics and the hydraulic and pneumatic features in section 5, we draw the conclusion that the R/E system design satisfies the requirements imposed by AFSC DH2-1, and measures should be taken to minimize its internal impact.
Keywords
aerospace components; aerospace engineering; aircraft; gears; hydraulic systems; kinematics; pneumatic systems; Imagine.Lab AMEsim; LMS Virtual; Lab Motion; R/E system design; aircraft; dynamic simulation; hydraulic feature; kinematics; landing gear retraction-extension; mathematical model; pneumatic feature; retraction-extension system; Actuators; Force; Gears; Joints; Mathematical model; Numerical models; Pistons; Virtual. Lab; cosimulation; landing gear; retraction/extension system;
fLanguage
English
Publisher
ieee
Conference_Titel
Artificial Intelligence, Management Science and Electronic Commerce (AIMSEC), 2011 2nd International Conference on
Conference_Location
Dengleng
Print_ISBN
978-1-4577-0535-9
Type
conf
DOI
10.1109/AIMSEC.2011.6010004
Filename
6010004
Link To Document