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。
High-temperature layered tile heat insulation system for aerospace craft
一种用于航空航天飞行器的高温分层瓦隔热系统
2022-08-26
Patent
Electronic Resource
Chinese
High temperature layered tile insulation system for aerospace vehicles
European Patent Office | 2022
|HIGH TEMPERATURE LAYERED TILE INSULATION SYSTEM FOR AEROSPACE VEHICLES
European Patent Office | 2021
|HIGH TEMPERATURE LAYERED TILE INSULATION SYSTEM FOR AEROSPACE VEHICLES
European Patent Office | 2022
|HIGH TEMPERATURE LAYERED TILE INSULATION SYSTEM FOR AEROSPACE VEHICLES
European Patent Office | 2021
|