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    Crashworthiness Performance Simulation and Analysis of Combined-Type Landing Gear Buffer

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 004::page 04022049
    Author:
    Xingbo Fang
    ,
    Hu Chen
    ,
    Yuying Han
    ,
    Xinhong Xie
    ,
    Xiaohui Wei
    ,
    Hong Nie
    DOI: 10.1061/(ASCE)AS.1943-5525.0001444
    Publisher: ASCE
    Abstract: To improve the crashworthiness of the landing gear buffer, an oleo-pneumatic buffer combined with an expansion tube is proposed in this paper. A numerical analytical model based on deformation theory was used to acquire the buffer force of the combined-type buffer during crushing. A finite-element model (FEM) was established to simulate the crushing process of the landing gear expanding buffer at the crash speed. The buffer force–displacement curve was exported from the analysis results, and the buffer force in the stable period was compared with that obtained from the theoretical analytical model. The deviation, 10.99%, verified the effectiveness of the expansion tube FEM model. Buffer performance analysis models of oleo-pneumatic and metal expansion tube oleo-pneumatic combing buffers with high- and low-pressure chambers were established. A parametric model of the landing gear was established. The crashworthiness response of different landing gear buffers at crash speed was studied. The results proved the high buffer efficiency of the combined-type buffer and its superiority and feasibility.
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      Crashworthiness Performance Simulation and Analysis of Combined-Type Landing Gear Buffer

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4286187
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    contributor authorXingbo Fang
    contributor authorHu Chen
    contributor authorYuying Han
    contributor authorXinhong Xie
    contributor authorXiaohui Wei
    contributor authorHong Nie
    date accessioned2022-08-18T12:11:58Z
    date available2022-08-18T12:11:58Z
    date issued2022/04/27
    identifier other%28ASCE%29AS.1943-5525.0001444.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4286187
    description abstractTo improve the crashworthiness of the landing gear buffer, an oleo-pneumatic buffer combined with an expansion tube is proposed in this paper. A numerical analytical model based on deformation theory was used to acquire the buffer force of the combined-type buffer during crushing. A finite-element model (FEM) was established to simulate the crushing process of the landing gear expanding buffer at the crash speed. The buffer force–displacement curve was exported from the analysis results, and the buffer force in the stable period was compared with that obtained from the theoretical analytical model. The deviation, 10.99%, verified the effectiveness of the expansion tube FEM model. Buffer performance analysis models of oleo-pneumatic and metal expansion tube oleo-pneumatic combing buffers with high- and low-pressure chambers were established. A parametric model of the landing gear was established. The crashworthiness response of different landing gear buffers at crash speed was studied. The results proved the high buffer efficiency of the combined-type buffer and its superiority and feasibility.
    publisherASCE
    titleCrashworthiness Performance Simulation and Analysis of Combined-Type Landing Gear Buffer
    typeJournal Article
    journal volume35
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001444
    journal fristpage04022049
    journal lastpage04022049-9
    page9
    treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 004
    contenttypeFulltext
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