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    • 1. 发明授权
    • Space shuttle damping and isolating device
    • 航天飞机阻尼隔离装置
    • US09004469B2
    • 2015-04-14
    • US13771381
    • 2013-02-20
    • EADS CASA Espacio S.L.
    • Miguel Lancho Doncel
    • F16M13/00F16F7/00B64G1/64F16F15/02F16F15/073F16F1/20F16F1/368
    • F16F7/00B64G1/641F16F1/20F16F1/368F16F15/022F16F15/073
    • A device used for providing dynamic isolation and damping of dynamic vibrations, in a passive way, originated in the launch vehicle of a space shuttle and reaching the payload or satellite. The device comprises a plurality of identical elementary unit elements, such that the device is designed in a modular way, allowing the individual modularity of each of the elementary unit elements. Each of the elementary unit elements is tailored and designed individually, and the complete device can be designed for each particular application and payload needed as a function of each of the elementary unit elements allowing an easy design and lower costs, for a wide range of payload applications. Each elementary unit element comprises a spring component and a damping component, such that the functionalities provided for each component are separated and can be individually tailored, thus providing a device having a wider range of adaptation capabilities.
    • 用于以被动方式动态隔离和阻尼动态振动的装置起源于航天飞机的运载火箭并到达有效载荷或卫星。 该装置包括多个相同的基本单元元件,使得该装置以模块化的方式设计,允许每个基本单元元件的各个模块化。 每个基本单元元素被单独设计和设计,并且可以为每个特定应用设计完整的设备,并且可以根据每个基本单元元素所需的有效载荷,从而允许宽范围的有效载荷的简单设计和更低的成本 应用程序。 每个基本单元元件包括弹簧部件和阻尼部件,使得为每个部件提供的功能被分离并且可以被单独地定制,从而提供具有更宽范围的适应能力的装置。