发明名称 Clamping fastener grip length indicator
摘要 A temporary fastener includes a grip length indicator. By machining a flattened area into a body of the temporary fastener, by engraving an scale into the flattened area, and by attaching an indicator dot visible in the groove to a moving part of an internal assembly of the temporary fastener, the grip length of the installed temporary fastener may be read directly on the scale while the temporary fastener applies a clamp-up force to a structure. By using the temporary fastener of the present invention, it is possible to determine a fastener hole length while a temporary fastener is installed. Using the method for determining a fastener grip length of the present invention enables the effective determination of the correct fastener grip length for each particular fastener hole of a large structure, such as an aircraft airframe.
申请公布号 US7070375(B2) 申请公布日期 2006.07.04
申请号 US20040966178 申请日期 2004.10.15
申请人 THE BOEING COMPANY 发明人 HOECKELMAN LESLIE A.
分类号 F16B13/06;B23Q3/14;F16B43/00;G01B5/00 主分类号 F16B13/06
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