The application relates to a method for manufacturing shimless assembly synchronously. The method aims to reduce and/or eliminate the need for shims in manufacturing assemblies, such as in manufacturing of aircraft wings. Exemplary methods include predicting a set of predicted manufacturing dimensions within a range of predetermined allowances for a first part, manufacturing the first part, scanning the first part to determine a set of actual manufacturing dimensions for the first part, and at least beginning manufacturing a second part before the scanning the first part is completed. The second part may be manufactured based on the set of predicted manufacturing dimensions for the first part. Once the scan of the first part is completed, the set of predicted manufacturing dimensions may be compared to a set of actual manufacturing dimensions to check for any non-compliant deviances between the predicted and actual manufacturing dimensions. Repairs and local re-scans may be performed in the areas of the non-compliant deviances, which may streamline manufacturing.

    本申请涉及无垫片组件的同步制造的方法。方法旨在减少和/或消除在制造组件中,诸如在飞机机翼的制造中,对垫片的需要。示例性方法包括:在第一部件的预定允许公差范围内预测一组预测制造尺寸;制造第一部件;扫描第一部件,以确定第一部件的一组实际制造尺寸;以及至少在扫描第一部件之前完成开始制造第二部件。可基于第一部件的一组预测制造尺寸来制造第二部件。一旦完成对第一部件的扫描,就可将一组预测制造尺寸与一组实际制造尺寸相比较,以检查预测制造尺寸和实际制造尺寸之间是否存在任何不符合要求的偏差。修理和局部重新扫描可在不符合要求的偏差的区域进行,这可简化制造过程。


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    Titel :

    Method for manufacturing shimless assembly synchronously


    Weitere Titelangaben:

    无垫片组件的同步制造的方法


    Beteiligte:

    Erscheinungsdatum :

    2020-04-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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