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Hole Alignment Tolerance Stacking Issues

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Technical Document Series Hole Alignment Tolerance Stacking Issues M&CT -TECH-99-025 October 1999 Mathematics and Computing Technology Phantom Works Phantom Works, Mathematics & Computing Technology A Division of The Boeing Company BOEING THIS DOCUMENT IS: Controlled by Mathematics and Engineering Analysis, G-6400 Prepared under D Contract DIR&D DCD/OH D Prepared on Sun Filed under Document No. M&CT-TECH-99-02S Title Hole Alignment Tolerance Stacking Issues Original Release Date October 1999 @ The information contained herein is NOT BOEING PROPRIETARY or BOEING LIMITED o Boeing Limited o Boeing Proprietary Prepared by: Fritz Scholz Approved by: Roberto E. Altschul i Hole Alignment Tolerance Stacking Issues Fritz Scholz M&CT-TECH-99-025 October 1999 Copyright 1999 The Boeing Company Phantom Works Mathematics and Computing Technology Box 3707, MIS 7L-21 Seattle, WA 98124-2207 Hole Alignment Tolerance Stacking IssuesFr i t z S ch o l z Mathematics and Computing TechnologyBoeing Phantom WorksFebruary 24, 1999AbstractEach of two parts hasKcoordination holes w

We consider various aspects of the coordination hole tolerance stacking problem. They arise when trying to mate two parts, such as stringers to skins, skins to skins, and panels to frames, etc., by placing (temporary) fasteners through matching hole pairs or hole triplets. Usually there will be K such hole pairs or triplets, where K 2and K

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