Dergiler / Uluslararası Mühendislik Araştırma ve Geliştirme Dergisi / 2017 / Cilt: 9 - Sayı: 3

Friction Reducing Composite Plating in Rocket Launchers

Sayfa
1–5
Yayın Tarihi
2017-12-26
DOI
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⚡ TL;DR(1 Cümlede Hızlı Çıkarım)

It is revealed that the particles with small size and high concentration are more effective in decreasing the friction coefficient.

📌 3 Maddede Bu Makale

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Amaç & Hipotez:Composite plating is commonly used for reducing friction and wear.
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Temel Bulgular & Veri:Steel specimens were coated by nickel including MoS2 particles in this study.
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Sonuç & Katkı:It is revealed that the particles with small size and high concentration are more effective in decreasing the friction coefficient.
🔬Tür:Araştırma Makalesi
📍Kapsam:Genişletilmiş Akademik Örneklem
⚙️Değişkenler:MoS2 · nickel · electroplating

Abstract

Composite plating is commonly used for reducing friction and wear. It is a method that can be used in the environments exposed to friction such as rocket launchers. Steel specimens were coated by nickel including MoS2 particles in this study. The effects of MoS2 particle concentration and particle size on the coefficient of friction and the amount of wear were determined by pin on disc tribometer. It is revealed that the particles with small size and high concentration are more effective in decreasing the friction coefficient.

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Bu Makaleye Atıf Yap

GÜLER, E. S., KARAKAYA, İ. (2017). Friction Reducing Composite Plating in Rocket Launchers. Uluslararası Mühendislik Araştırma ve Geliştirme Dergisi, Cilt: 9 - Sayı: 3, 1–5. https://ajindex.com/articles/889492

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Kaynakça (6)

  1. ASTM-G99-95a (2000), Standard Test Method for Wear Testing with a Pin-on-Disk Apparatus, ASTM International. Cardinal, M.F., Castro, P.A., Baxi J., Liang, H., Williams, F.J. (2009). Characterization and frictional behavior of nanostructured Ni-W-MoS2 composite coatings. Surface and Coatings Technology, 204(1-2), 85-90.
  2. Charles, J., Barker, L. and Kern, W. K. (1963). Aircraft rocket launcher US 3077144 A Hilton, M.R. and Fleischauer,P.D. (1992). Applications of Solid Lubricant Films in Spacecraft. Surface and Coating Technology, 54-55, 435-441.
  3. Hou, K.-H., Wang, H.-T., Sheu, H.-H. and Ger, M.-D. (2014). Preparation and wear resistance of electrodeposited Ni–W/diamond composite coatings. Applied Surface Science, 308, 372–379.
  4. Huang, Z.-j. and Xiong D.-s. (2008). MoS2 coated with Al2O3 for Ni-MoS2/Al2O3 composite coatings by pulse electrodeposition. Surface and Coatings Technology, 202(14), 3208-3214.
  5. Saraloglu Guler, E., İ. Karakaya, and E. Konca (2013). Effect of Electrodeposition Parameters on the Current Density of Hydrogen Evolution Reaction in Ni and Ni-MoS2 Composite Coatings. Int. J. Electrochem. Sci., 8, 5496 - 5505. Siopis, M.J. and Cowan, R.S. (2014). Electromagnetic Launch Technology (EML). International Symposium on Electromagnetic Launch Technology, 7-11
  6. July, San Diego, 865.