The invention discloses a two-stage damping device for a domestic strapdown inertial navigation type aviation gravimeter. The two-stage damping device comprises a base, a first-stage damping material,a middle mass block, a second-stage damping material and a mounting base which are sequentially arranged from bottom to top, wherein the base is used for being mounted and fixed on an airplane, and the mounting base is used for mounting and fixing the aviation gravimeter; vibration of the airplane is transmitted from bottom to top through the base and is gradually reduced, and finally the vibration is transmitted to the aviation gravimeter through the mounting base. According to the two-stage damping device for the domestic strapdown inertial navigation type aviation gravimeter, on the one hand, specific vibration reduction damping, rigidity and specific parameters of the middle mass block are provided, and the actual application requirements of the domestic strapdown inertial navigationtype aviation gravimeter are fully met. Secondly, a laminated structure of the two-stage damping device is provided, and the laminated structure has the advantages of being simple in structure, high in reliability, convenient to assemble and maintain and the like. And thirdly, a clamping groove type mounting and fixing mode between the damping materials and a damping plate is provided, and good safety, reliability and three-dimensional damping performance are achieved.

    一种用于国产捷联惯导式航空重力仪的两级减振装置,包括自下而上依次设置的底座、第一级减振材料、中间质量块、第二级减振材料和安装座;其中,所述底座用于安装固定在飞机上,所述安装座上用于安装固定航空重力仪;所述飞机的振动经所述底座自下而上传递且逐渐减小,最终通过所述安装座传递给所述航空重力仪。本发明一种用于国产捷联惯导式航空重力仪的两级减振装置,一是提供了具体的减振阻尼、刚度和中间质量块的具体参数,充分满足了国产捷联惯导式航空重力仪的实际应用需求;二是提供了两级减振装置的一种层叠式结构,具有结构精简、可靠性强、便于拼装和维修等优点;三是提供了减振材料与减振板之间的卡槽式安装固定方式,具有较好的安全可靠性和三维减振性。


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    Title :

    Two-stage damping device for domestic strapdown inertial navigation type aviation gravimeter


    Additional title:

    一种用于国产捷联惯导式航空重力仪的两级减振装置


    Contributors:
    QU JINHONG (author) / JIANG ZUOXI (author) / DUAN LEYING (author) / ZHOU XIHUA (author) / DENG XIAODAN (author)

    Publication date :

    2021-01-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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