Statistical tolerancing
AssigneeThe Boeing Company
InventorsRobert E. Atkinson, Teresa S. Miller, Friedrich-Wilhelm Scholz
Life of this patent
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AssigneeThe Boeing Company
InventorsRobert E. Atkinson, Teresa S. Miller, Friedrich-Wilhelm Scholz
Estimating the term…
A process of establishing valid statistical dimensional tolerance limits for designs of detail parts that will enable accurate prediction of an economically acceptable degree of non-conformance of a large flexible end item assembly, having a set of predetermined dimensional tolerances, made from the detail parts, wherein the detail part tolerances are enlarged substantially compared to tolerances that would be necessary using an arithmetic "worst case" approach to remain within the end assembly tolerances while remaining within preestablished stress limits of the parts. A preferred assembly sequence for assembling the parts into the assembly is selected and validated. Locations, numbers and size of coordination features to be machined in said detail parts are selected, by which the parts are located relative to each other and fastened together to form the assembly. Individual part statistical dimensional tolerances are established as a fabrication requirement for the parts that enable the parts to be economically produced and assembled into assemblies that meet the predetermined assembly dimensional tolerances. The parts are produced to the individual statistical dimensional tolerances in a capable process, having a Cpk equal to at least 1.0, while holding the mean values of the statistically determined dimensions of the individual parts to within a predetermined percentage of the nominal dimension. The end item is assembled in accordance with the preferred assembly sequence by locating the parts relative to each other by reference to the coordination features as the primary determinator of assembly configuration.
A process for establishing valid statistical dimensional tolerance limits, that are enlarged substantially compared to tolerances established by an arithmetic "worst case" approach, for designs of detail parts and will enable accurate prediction of an economically acceptable degree of non-conformance of an end item assembly made from said parts, comprising:
A process for establishing valid statistical detail part dimensional tolerance limits that will enable accurate prediction of an economically acceptable degree of non-conformance of a large flexible assembly made from said parts, comprising:
An assembly having a predetermined set of dimensional tolerances, made from a plurality of parts each having a set of individual tolerances, comprising:
A process of assembling large flexible structural assemblies having predetermined assembly dimensional tolerances from a plurality of individual parts, some of which are flexible, while remaining within established preload stress limits of said parts, comprising:
A process of assembling a large flexible structure, having a set of predetermined dimensional tolerances, from a plurality of individual parts, some of which are flexible, while remaining within preestablished stress limits of said parts, comprising:
A process of assembling a large flexible assembly from a plurality of individual parts, some of which are flexible, while remaining within predetermined dimensional tolerances of said structure and within preestablished stress limits of said parts, comprising:
A process of ensuring an accurate assembly made from parts assembled with minimal use of hard tooling, at least some of which parts are flexible, comprising:
A detail part from a population of parts with statistically characterized predetermined dimensional tolerances, having a predetermined set of dimensional tolerances for attachment into an assembly having predetermined assembly tolerances from which said detail part tolerances was derived, comprising:
Dependencies are inferred from the claim text.