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    A Dynamic Loading Mechanism for a Morphing Winglet

    Source: Journal of Mechanisms and Robotics:;2022:;volume( 015 ):;issue: 005::page 54501
    Author:
    Buchkazanian, Raffi S.;Campos, Gabriel H.;Xi, Fengfeng (Jeff)
    DOI: 10.1115/1.4055572
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A loading mechanism for a variable cant angle morphing winglet is proposed in this paper. The mechanism provides a method of loading a morphing winglet with the simulated aerodynamic lift force by maintaining its application direction always orthogonal to the surface of the winglet throughout the range of motion. The loading mechanism is developed by type synthesis of fourbar linkages through enumeration of prismatic and revolute joints. The final design is a RPRP fourbar linkage modified by merging the middle PR joint together to form a planar joint named Sharkfin. The shape of Sharkfin is optimized to minimize its weight effect on the overall loading system. A halfscale prototype was built as a reference to address several implementation issues including the neutral loading condition. Afterwards, a fullsize dynamic loading mechanism was successfully constructed and implemented to load test a fullsize morphing winglet.
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      A Dynamic Loading Mechanism for a Morphing Winglet

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4288824
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    contributor authorBuchkazanian, Raffi S.;Campos, Gabriel H.;Xi, Fengfeng (Jeff)
    date accessioned2023-04-06T12:57:17Z
    date available2023-04-06T12:57:17Z
    date copyright11/24/2022 12:00:00 AM
    date issued2022
    identifier issn19424302
    identifier otherjmr_15_5_054501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4288824
    description abstractA loading mechanism for a variable cant angle morphing winglet is proposed in this paper. The mechanism provides a method of loading a morphing winglet with the simulated aerodynamic lift force by maintaining its application direction always orthogonal to the surface of the winglet throughout the range of motion. The loading mechanism is developed by type synthesis of fourbar linkages through enumeration of prismatic and revolute joints. The final design is a RPRP fourbar linkage modified by merging the middle PR joint together to form a planar joint named Sharkfin. The shape of Sharkfin is optimized to minimize its weight effect on the overall loading system. A halfscale prototype was built as a reference to address several implementation issues including the neutral loading condition. Afterwards, a fullsize dynamic loading mechanism was successfully constructed and implemented to load test a fullsize morphing winglet.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Dynamic Loading Mechanism for a Morphing Winglet
    typeJournal Paper
    journal volume15
    journal issue5
    journal titleJournal of Mechanisms and Robotics
    identifier doi10.1115/1.4055572
    journal fristpage54501
    journal lastpage545017
    page7
    treeJournal of Mechanisms and Robotics:;2022:;volume( 015 ):;issue: 005
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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