Various systems and methods are disclosed for a layered tile insulation system for a spacecraft configured to withstand vibrations, high temperatures, and extreme thermal gradients. A layered tile insulation system includes at least one layered tile, each of the at least one layered tile including an outer layer having a first interlocking surface of a first set of interlocking features and an inner layer having a second interlocking surface of a second set of interlocking features, the outer layer configured to couple with the inner layer, thus, the mechanical joint is formed by interlocking of the first interlocking surface and the second interlocking surface.

    本发明公开了空间飞行器的分层瓦隔热系统的多种系统和方法,分层瓦隔热系统被配置为可承受振动、高温和极端热梯度。分层瓦隔热系统包括至少一个分层瓦,所述至少一个分层瓦的每个分层瓦包括具有第一组互锁特征的第一互锁表面的外层和具有第二组互锁特征的第二互锁表面的内层,外层被配置为与内层耦合,从而通过第一互锁表面与第二互锁表面的互锁形成机械接头。


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    Titel :

    High-temperature layered tile heat insulation system for aerospace craft


    Weitere Titelangaben:

    一种用于航空航天飞行器的高温分层瓦隔热系统


    Beteiligte:
    HORNING MICHAEL (Autor:in) / HOFMANN MARTIN (Autor:in) / MOYNIHAN KEVIN (Autor:in) / SLINGSBY ROBERT (Autor:in)

    Erscheinungsdatum :

    26.08.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse



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