发明名称 Hole angularity gage with out-of-tolerance indicator, and methods of operation and manufacture thereof
摘要 <p>An embodiment of a hole angularity gage includes a gage body and a contact disc positioned within the gage body. The contact disc includes a central opening defined by an inner edge. The gage also includes a center pin that extends through the central opening, and a hole probe adapted to rotate the center pin from a primary gage axis toward the contact disc's inner edge. The gage also includes an indicator adapted to activate when the center pin makes contact with the contact disc. Another embodiment of a hole angularity gage includes a hole probe and a circuit. The circuit includes an indicator and a switch, which is adapted to close when the hole probe is rotated by an angle greater than a gage setting angle. The indicator is adapted to activate when the switch is closed. Other embodiments include methods for using and manufacturing hole angularity gages.</p>
申请公布号 GB2450246(B) 申请公布日期 2010.01.06
申请号 GB20080010811 申请日期 2008.06.12
申请人 THE BOEING COMPANY 发明人 KIN Y WONG;LEWIS J SPRAGUE
分类号 G01B5/245;G01B7/305 主分类号 G01B5/245
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