2010
DOI: 10.1016/j.matdes.2009.08.037
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HVOF sprayed WC–Co coatings: Microstructure, mechanical properties and friction moment prediction

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Cited by 60 publications
(32 citation statements)
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“…The heat required to melt the binder phase often results in the deterioration of the carbide and binder phases by decarburization, phase changes, high temperature oxidation and grain growth [1][2][3][4][5][6][7]. Brittle and hard W 2 C, W and undesirable η phases are usually the result of this deterioration, which decreases the overall mechanical and wear properties of the coatings [8][9][10].…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…The heat required to melt the binder phase often results in the deterioration of the carbide and binder phases by decarburization, phase changes, high temperature oxidation and grain growth [1][2][3][4][5][6][7]. Brittle and hard W 2 C, W and undesirable η phases are usually the result of this deterioration, which decreases the overall mechanical and wear properties of the coatings [8][9][10].…”
Section: Introductionmentioning
confidence: 99%
“…This process involves limited to no melting during coating deposition; thus avoiding the decomposition of the carbide phase. The chemical composition and bulk properties of the coatings typically remain identical to the parent powders [1][2][3][4][5][6][7].…”
Section: Introductionmentioning
confidence: 99%
“…The fracture toughness K c was calculated according to the Wilshaw Eq. (1) [26] (the result was the average value of ten measurements), where P, a and c are the load of Huayin HV5 type Vickers hardness meter (5 kg), half the length of indentation diagonal and half the length of the crack, respectively.…”
Section: Characterizationmentioning
confidence: 99%
“…Among the several technologies for depositing metallic coatings on metallic substrates, thermal spray high-velocity oxygen-fuel (HVOF) is one of the most versatile [8] and efficient technologies, with many multiscale features [9,10], capacity to produce homogeneous [11] and very dense coatings [12][13][14][15][16][17] with porosity levels typically in the range 0.1-2% [13], low oxide content [11,12], high hardness [13,18], excellent bond strength frequently exceeding 69 MPa [11,13,19], and low decarburization [13,20]. Also, the low gas temperature of particles avoids superheating during flight and preserves the nanocrystalline structure of the starting powders of the coating [21].…”
Section: Introductionmentioning
confidence: 99%