The invention belongs to the technical field of airplane structure strength test design, and particularly relates to a loading device for an airplane structure strength test, which is used for loading a loading point on an airplane structure only by connecting the end part of a load loading steel rope with the loading point on the airplane structure, so that the situations of structural space limitation and difficulty in installation can be avoided, and the test efficiency is improved. The actuator cylinder can be selected to be connected to the corresponding load loading connector on the load amplification block according to the actual load loading requirement, and the loading capacity of the actuator cylinder is correspondingly amplified by utilizing the lever principle, so that the loading capacity of the actuator cylinder is improved, and the load loading precision is ensured.

    本申请属于飞机结构强度试验设计技术领域,具体涉及一种飞机结构强度试验用加载装置,以其对飞机结构上加载点进行载荷加载,仅需要以载荷加载钢绳的端部连接飞机结构上的加载点,可避免受到结构空间限制,难以进行安装的情形,且可根据实际载荷加载需求的大小,选择将作动筒连接到载荷放大块上相应的载荷加载接头上,利用杠杆原理,对作动筒的加载能力进行相应的放大,以此提升作动筒的加载能力,以及保证载荷加载的精度。


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    Titel :

    Loading device for airplane structure strength test


    Weitere Titelangaben:

    一种飞机结构强度试验用加载装置


    Beteiligte:
    CAO YING (Autor:in) / LU XUEFENG (Autor:in) / SU YUFENG (Autor:in) / DU JINZHU (Autor:in)

    Erscheinungsdatum :

    26.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES



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