2021
DOI: 10.1108/aeat-10-2020-0237
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A novel retractable landing gear of a light amphibious airplane design, synthesis, analysis, and implementation

Abstract: Purpose The purpose of this paper is to present a novel retractable main landing gear for a light amphibious airplane, while the design, synthesis and analysis are given in details for constructing the main landing gear. Design/methodology/approach The constraint three-position synthesis has given the correct path of all linkages that suitably fit the landing gear into the compartment. The additional lock-link is introduced into the design to ensure the securement of the mechanism while landing. Having the t… Show more

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Cited by 4 publications
(2 citation statements)
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“…Yin et al [19] studied the single-sidestay (SSS) main landing gear, analyzed the impact of the unlocking force on the retraction process of the landing gear, and optimized the critical unlocking force. Sinchai et al [20] optimized the unlock spring stiffness by conducting a kinematics bifurcation analysis and tremendously reduced the actuator force. In the research of DSS landing gear, Knowles et al [21] addressed the issue of the unlocking and locking of 3D retraction landing gear being very sensitive to related parameters.…”
Section: Introductionmentioning
confidence: 99%
“…Yin et al [19] studied the single-sidestay (SSS) main landing gear, analyzed the impact of the unlocking force on the retraction process of the landing gear, and optimized the critical unlocking force. Sinchai et al [20] optimized the unlock spring stiffness by conducting a kinematics bifurcation analysis and tremendously reduced the actuator force. In the research of DSS landing gear, Knowles et al [21] addressed the issue of the unlocking and locking of 3D retraction landing gear being very sensitive to related parameters.…”
Section: Introductionmentioning
confidence: 99%
“…Chi et al [4] developed a compliant gripper with nearly parallel gripping motion using topology and dimensional synthesis approach, selected a nondominated multi-objective genetic algorithm for the optimal design process to meet various design goals, and developed a kinetostatic model based on the chained beam constraint model for force-displacement analysis of the designs. Chinvorarat et al [5] presented a retractable main landing gear for a light amphibious airplane, while the design, synthesis, and analysis are given for constructing the main landing gear. The constraint three-position synthesis has given the correct path of all linkages that suitably fit the landing gear into the compartment.…”
Section: Introductionmentioning
confidence: 99%