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A Prediction Method of Aircraft Field Assembly Accuracy Based on Measured Data

A technology for on-site assembly and precision prediction, applied in forecasting, data processing applications, instruments, etc., can solve the problems of lack of precision prediction control method, decline in assembly productivity, etc., to improve the success rate of one-time assembly, reduce assembly rework and assembly scrap. Effect

Active Publication Date: 2021-08-24
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

However, in the stage of aircraft on-site assembly and production, there is a lack of effective precision prediction control methods. In addition to leaving assembly margins for certain processes for "installation and adjustment", most of the process assembly is in a "trial assembly" state, resulting in Unnecessary assembly rework and tooling adjustments reduce assembly productivity

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  • A Prediction Method of Aircraft Field Assembly Accuracy Based on Measured Data
  • A Prediction Method of Aircraft Field Assembly Accuracy Based on Measured Data
  • A Prediction Method of Aircraft Field Assembly Accuracy Based on Measured Data

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Embodiment Construction

[0044] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0045] refer to figure 1 , a method for predicting aircraft field assembly accuracy based on measured data provided in an embodiment of the present invention, the method includes the following steps:

[0046] Step 1, convert the fit constraints of each part in the assembly unit into anchor point constraints.

[0047] This step specifically includes:

[0048] (1) Analyze the fit constraints of the constrained parts and the fit features that constitute the fit...

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Abstract

The invention discloses a method for predicting aircraft on-site assembly accuracy based on actual measured data, and relates to the technical field of aircraft assembly. The coordination constraints of each part in an assembly unit are converted into anchor point constraints, and multiple anchor points are selected on each part. , use digital measuring equipment to measure the positioning deviation of each positioning point, establish a positioning analysis model according to the positioning point, and calculate the pose deviation of each part according to the positioning deviation, calculate the position deviation at the key point according to the pose deviation, and follow the assembly Sequentially combine the position deviation of the current part with the positioning deviation of the next part as the positioning deviation of the next part, and input the positioning deviation into the positioning analysis model to obtain the pose deviation, until the analysis of all parts is completed, and the assembly deviation required by the design is obtained, namely Assembly precision. The invention solves the problem that the process assembly accuracy cannot be predicted in the on-site assembly stage of the aircraft, and provides a technical basis for improving the success rate of one-time assembly of the aircraft and reducing assembly rework and assembly scrapping.

Description

technical field [0001] The invention relates to the technical field of aircraft assembly, in particular to a method for predicting the accuracy of aircraft on-site assembly based on actual measurement data. Background technique [0002] In the process of aircraft assembly and production, although process designers are in the process design stage, they control and optimize the assembly accuracy of key processes of aircraft products by adjusting the assembly sequence, positioning reference, assembly tolerance and other assembly processes. However, in actual assembly operations, due to practical factors such as tooling errors, assembly deformation, and part manufacturing deviations, aircraft products do not meet the design requirements after assembly, and incidents of assembly rework and assembly scrapping occur from time to time. [0003] At present, the measures and means of domestic aircraft manufacturers to control the assembly quality are mainly concentrated in the assembl...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06Q10/04G06Q50/04
CPCG06Q10/04G06Q50/04Y02P90/30
Inventor 耿俊浩胡波李五朋刘殷杰张敏田锡天马华
Owner NORTHWESTERN POLYTECHNICAL UNIV