Features of repairing polimer composite parts with self-contained repair equipment

Authors

  • O. V. Andrieiev Antonov company, Kiev, Ukraine
  • B. V. Lubkin National aerospace university named Gukovskiy «KHAI», Kharkov, Ukraine
  • V. S. Petropolskyy Antonov company, Kiev, Ukraine
  • V. S. Nitka Antonov company, Kiev, Ukraine

DOI:

https://doi.org/10.20535/2521-1943.2018.84.151653

Keywords:

composite material, self-contained repair equipment, repair, design and technological solutions, thermo blanket, heating, vacuumization, curing, defect, technology

Abstract

This paper covers development of repair procedures for the polymer composite (PC) structures using the off-line repair equipment (ORE). The ORE capabilities and examples of use are described. Several design and technological solutions for repair of PC components with the use of ORE directly on the aircraft have been developed. Procedures for repair of defective areas in the PC components of the transport aircraft are described.

Strength properties and reparability have been analyzed upon completion of the activities. Recommendations on the use of ORE during repair on the aircraft in the field conditions have been developed. 

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Published

2018-12-26

How to Cite

[1]
O. V. Andrieiev, B. V. Lubkin, V. S. Petropolskyy, and V. S. Nitka, “Features of repairing polimer composite parts with self-contained repair equipment”, Mech. Adv. Technol., vol. 84, no. 3(84), pp. 69–74, Dec. 2018.

Issue

No. 3(84) (2018)

Section

Original study

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