发明名称 Wärmeschutzvorrichtung, insbesondere für Raumfahrzeuge
摘要 The thermal protection device is formed by a plurality of juxtaposed elemental modules, each including a fairing (streamlining) element (20) fitted with fastening tabs (30) and with a thermal insulation integrated with the fairing element. The gap between neighbouring fairing elements is limited to the minimum value necessary for taking up their thermal expansions. The connection means (40) which releasably join the fastening tabs to a primary structure to be protected comprise a ball joint (44) fixed adjustably to the fastening tab and capable of being locked inside a corresponding housing of a reception part (60) fixed to the primary structure. The ball joint (44) is locked in its housing by means of a finger which can be released by an action exerted against an elastic return force (80). <IMAGE>
申请公布号 DE69403376(T2) 申请公布日期 1998.01.02
申请号 DE1994603376T 申请日期 1994.03.30
申请人 SOCIETE EUROPEENNE DE PROPULSION, SURESNES, FR 发明人 ARNOLD, THIBAULT, F-33110 LE BOUSCAT, FR;LACOMBE, ALAIN, F-33600 PESSAC, FR;TUAL, MICHEL, F-33290 BLANQUEFORT, FR
分类号 B64C1/38;B64G1/58;F16C11/06 主分类号 B64C1/38
代理机构 代理人
主权项
地址