发明名称 Thermal protection device, in particular for an aerospace vehicle
摘要 The thermal protection device is made up of a plurality of juxtaposed unit modules each comprising a fairing element provided with fixing tabs and thermal insulation integrated in the fairing element. The gap between neighboring fairing elements is limited to the minimum width necessary for accommodating thermal expansion thereof. The connection means which releasably connect the fixing tab to a primary structure to be protected comprise a ball fixed to the fixing tab in adjustable manner and capable of being locked in a corresponding socket of a retaining part fixed to the primary structure. The ball is locked in its socket by means of a bolt capable of being released by action exerted against a resilient return force.
申请公布号 US5489074(A) 申请公布日期 1996.02.06
申请号 US19940220807 申请日期 1994.03.31
申请人 SOCIETE EUROPEENNE DE PROPULSION 发明人 ARNOLD, THIBAULT;LACOMBE, ALAIN;TUAL, MICHEL
分类号 B64C1/38;B64G1/58;F16C11/06;(IPC1-7):B64G1/22;B64C1/12 主分类号 B64C1/38
代理机构 代理人
主权项
地址