Clamping fastener grip length indicator
AssigneeThe Boeing Company
InventorLeslie A. Hoeckelman
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AssigneeThe Boeing Company
InventorLeslie A. Hoeckelman
Estimating the term…
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.
A method for determining a fastener hole length, comprising:
A method for determining a fastener grip length of a fastener used in an aircraft airframe assembly, comprising:
A method for assembling an aircraft airframe, comprising:
Dependencies are inferred from the claim text.