Volume 41 Issue 1
Mar.  2012
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HAN Xiao, ZHU Jia-Qi, ZHOU Feng, CHEN Xiao-Li. Thermal stability of multilayer tetrahedral amorphous carbon films[J]. Infrared and Laser Engineering, 2012, 41(1): 144-148.
Citation: HAN Xiao, ZHU Jia-Qi, ZHOU Feng, CHEN Xiao-Li. Thermal stability of multilayer tetrahedral amorphous carbon films[J]. Infrared and Laser Engineering, 2012, 41(1): 144-148.

Thermal stability of multilayer tetrahedral amorphous carbon films

  • Publish Date: 2012-01-25
  • Using the filtered cathodic vacuum arc(FCVA) deposition technique with a process of changing substrate bias, a stable thick multilayer ta-C film was prepared. The multilayer films with a good adhesion consisted of alternating sp2-rich sublayers Ai and sp3-rich sublayers Bi(i=1,2,3). The sublayers thickness ratio dAi/dBi was about 1.0, and the total thickness of the multilayer film was about 1 m. The calculated compressive stress of sublayers by the Stoney formula revealed an alternating wave change. After anealling at 500 ℃ in vacuum, the Raman spectra suggested the multilayer film had a non-changed sp3-rich microstructure. The nanoindentation measurement showed an increasing hardness and Youngs modulus of the multilayer film after annealing. The nanoscratch test showed the favourable scratch resistance and adhesive properties of multilayer film. The results indicate that the multilayer ta-C film has some excellent mechanical properties and thermal stability. The multilayer film is proper for the optical protective coatings for aeronautics and space applications.
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Thermal stability of multilayer tetrahedral amorphous carbon films

  • 1. Beijing Institute of Space Mechanics & Electricity,Beijing 100076,China;
  • 2. School of Astronautics,Harbin Institute of Technology,Harbin 150080,China

Abstract: Using the filtered cathodic vacuum arc(FCVA) deposition technique with a process of changing substrate bias, a stable thick multilayer ta-C film was prepared. The multilayer films with a good adhesion consisted of alternating sp2-rich sublayers Ai and sp3-rich sublayers Bi(i=1,2,3). The sublayers thickness ratio dAi/dBi was about 1.0, and the total thickness of the multilayer film was about 1 m. The calculated compressive stress of sublayers by the Stoney formula revealed an alternating wave change. After anealling at 500 ℃ in vacuum, the Raman spectra suggested the multilayer film had a non-changed sp3-rich microstructure. The nanoindentation measurement showed an increasing hardness and Youngs modulus of the multilayer film after annealing. The nanoscratch test showed the favourable scratch resistance and adhesive properties of multilayer film. The results indicate that the multilayer ta-C film has some excellent mechanical properties and thermal stability. The multilayer film is proper for the optical protective coatings for aeronautics and space applications.

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