发明名称 MOTION REDUCING FLEXURE STRUCTURE
摘要 A flexure/actuator (116a, 116b, 116c) is configured to reliably provide motion reduction, e.g. for positioning or adjusting telescope or other technical or scientific instrument components (112), with respect to a support structure (114), preferably at cryogenic as well as higher temperatures. The flexure can be constructed to provide support and strength, preferably in all axes, such as may be needed to withstand launch forces. Preferably flexure axes are defined at upper and lower edges of sidewalls and at intermediate positions of sidewalls. Actuator activation adjusts distance between sidewall intermediate flexures and, by operation of sidewall flexures, adjusts the distance between upper and lower surfaces with a desired reduction ratio.
申请公布号 WO9926092(A1) 申请公布日期 1999.05.27
申请号 WO1998US23582 申请日期 1998.11.05
申请人 BALL AEROSPACE & TECHNOLOGIES CORP. 发明人 SLUSHER, ROBERT, B.
分类号 G02B7/182;(IPC1-7):G02B5/08;G02B26/08 主分类号 G02B7/182
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