发明名称 Method and device for releasing the pre-load initially applied to a mechanism such as an on-board bearing in a spacecraft.
摘要 In spacecraft, mechanisms such as ball-bearings (14,14') are put under an initial pre-load to enable them to tolerate the vibrations caused by launching, without resulting in looseness. A member (34) made of a shape-memory material makes it possible, owing for example to its lengthening, to release this pre-load when the craft is in operational mode. This release may be triggered by, in particular, a heating resistor (36) which when a current is applied raises the member (34) above its shape-changing temperature. <IMAGE>
申请公布号 EP0466993(B1) 申请公布日期 1995.01.04
申请号 EP19900402075 申请日期 1990.07.18
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 SCHOEFFTER, JEAN-PIERRE
分类号 B64G1/22;B64G1/44;B64G1/64;B64G1/66;F16C25/08;F16C41/04 主分类号 B64G1/22
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