Method for researching action mechanism of trace element phosphorus in wrought superalloy and application
A technology for deforming superalloys and trace elements, applied in the field of superalloys, can solve the problems that the existence mode and action mechanism of deformed superalloys are not unified, the distribution and action are difficult, and the composition and structure of superalloys are complex.
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Embodiment 1
[0057] 1. Alloy composition
[0058] A furnace of IN706 master alloy was melted, its composition (weight fraction, %): 41.3Ni, 16.21Cr, 1.92Ti, 3.0Nb, 0.37Al, 0.022C, <0.001B, 0.002P, Fe balance. Cut out the master alloy, add 6 different contents of P (0.002%, 0.004%, 0.007%, 0.010%, 0.014%, 0.025), and remelt into daughter alloys.
[0060] vacuum induction melting
[0061] 3. Thermal processing of alloys
[0062] The ingot is homogenized at 1150℃×30h+1190℃×30h
[0063] Heating temperature: 1110±10℃, 4 hours
[0064] Open forging temperature: 1000±10℃
[0065] Final forging temperature: 950°C
[0066] 4. Heat treatment of alloy
[0067] Solution treatment: 920℃~1190℃, keep warm for 5min-4h and then air-cooled / water-cooled.
[0068] Aging treatment: 845°C, 3 hours, 730°C, 10 hours, 55°C / h furnace cooling, 620°C, 8 hours, air cooling.
[0069] 5. Alloy structure and properties
[0070] 1) Microstructure and properties of alloy after solution ...
Embodiment 2
[0085] 1. The composition of Ni-Cr alloy is shown in Table 1
[0086] The composition (wt.%) of the Ni-Cr alloy of table 1 different P content
[0087]
[0088] 2. Alloy smelting
[0089] vacuum induction melting
[0090] 3. Thermal processing of alloys
[0091] Heating temperature: 1110±10℃, 4 hours
[0092] Open forging temperature: 1000±10℃
[0093] Final forging temperature: 950°C
[0094] 4. Heat treatment of alloy
[0095] Solution treatment: 1100℃, 1 hour, water cooling and furnace cooling
[0096] Aging treatment: 720°C, 10 hours, 55°C / h furnace cooling, 620°C, 8 hours, air cooling
[0097] 5. Alloy structure and properties
[0098] The Ni-Cr alloys were solid-dissolved at 1100°C for 1 hour, and the microstructure and morphology of the alloys were significantly different under different cooling methods. Rapid water cooling showed no precipitates at the grain boundaries and within the grains. Slow furnace cooling, there are precipitated phases at the grain b...
Embodiment 3
[0102] 1. The composition of Ni-Cr-Fe alloy is shown in Table 3
[0103] The composition (wt.%) of the Ni-Cr-Fe alloy of table 3 different P contents
[0104]
[0105] 2. Alloy smelting and thermal processing
[0106] Alloy smelting and thermal processing are the same as in Example 2.
[0107] 3. Heat treatment of alloy
[0108] Solution treatment: 1100℃, 1 hour, water cooling
[0109] Aging treatment: 800°C, 8 hours, water cooling
[0110] 4. Alloy structure and properties
[0111] 1) Microstructure and properties of alloy after solution treatment
[0112] (1) Alloy structure
[0113] The microstructure of Ni-Cr-Fe alloy under solid solution condition is as follows: Figure 12 As shown, each alloy was solid-dissolved at 1100°C for 1 hour and then furnace-cooled, a large number of carbides were precipitated on the grain boundaries, and there was no precipitated phase in the grains.
[0114] (2) Tensile properties
[0115] The tensile properties of the alloy after f...
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