Interference and Gap Calculation for Composite Component Assembly Based on Measured Data
Author:
Affiliation:

1.AVIC Research Institute for Special Structures of Aeronautical Composite, Aviation Key Lab of Science and Technology onHigh Performance Electromagnetic Windows,Jinan 250023;2.Nanjing University of Aeronautics And Astronautics,Nanjing 210016

Clc Number:

TP391

Fund Project:

Stress generation mechanism and control of aircraft composite structure with complex assembly interface

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    Abstract:

    For the composite component assembly interference problem caused by molding errors, this paper proposed a method of dimensional reduction of composite component assembly interference and clearance based on point cloud data obtained from laser equipment, it converts the interference and clearance calculation of the three-dimensional assembly into the calculation of the two-dimensional boundary distance. Taking a certain type of aircraft random assembly as an example,the feasibility of the proposed method and algorithm is verified through experiments, and the assembly accuracy and efficiency are improved compared with the original assembly process.

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History
  • Received:August 10,2023
  • Revised:October 29,2023
  • Adopted:October 30,2023
  • Online: July 01,2024
  • Published: