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The designed architecture is based on PC-based injection machines [11-14]. 1.
The system architecture of machine information retrieving agent in the factory is shown in Fig. 1.
The conclusion of this study is described as follows: 1.
References [1] R.
Hsu: Development of Software-as-a-Service Cloud Computing Architecture for Manufacturing Management Systems Based on Virtual COM Port Driver Technology, Applied Mechanics and Materials, Vol. 479-480, No. 5 (2013), pp. 1023-1026

The number of IMCs in the Sn-3.5Ag-1.0Cu-0.4Mg solder is more than that in the Sn-3.5Ag-1.0Cu-0.2Mg.
The interface for Sn-3.5Ag-1.0Cu solder, Sn-3.5Ag-1.0Cu-0.2Mg solder, and Sn-3.5Ag-1.0Cu-0.4Mg solder were shown in this figure.
(2) In the case of Sn-3.5Ag-1.0Cu-0.2Mg solder and Sn-3.5Ag-1.0Cu-0.4Mg solder, the size of β-Sn grain was similar with that in the case of Sn-3.5Ag-1.0Cu solder.
References [1] M.F.
Alloys Compd. 479 (2009) 121-127

The XRD patterns of the film deposited with 3:1 of N2:Ar flow rate ratio (Fig. 1(b)) reveal the highest of the intensity of TiN(111) whereas the lowest is at 1:1 (Fig.1(c)).
Fig.1.
The thickness of TiN film deposited onto SiO2/Si wafer at N2:Ar flow rate ratio: Pure N2, 3:1, 1:1 and 1:3 Fig.2. shows the thickness of TiN films deposited onto SiO2/Si wafer at N2:Ar flow rate ratio: Pure N2, 3:1, 1:1 and 1:3 are 472.8 nm, 550.4 nm, 1549.8 nm and 1827.6 nm, respectively.
Table 1.
N2:Ar flow rate ratio N2:Ar Flow rate [sccm] DC power supply [V, A, kW] Electrical Resistivity [µΩ-cm] Pure N2 40:0 565, 10.6, 6 131.91 3:1 1:1 27:9 21:21 517, 11.4, 6 479, 12.4, 6 127.80 171.87 1:3 8:24 475, 12.5, 6 212.54 Reference [1] M.Boumerzoug, Z.Pang, M.Boudreau and P.Mascher, Appl.Phys.Lett.66, 1995 [2] I.Suni, M.Biomberg, J.Saarilahti and J.Vac, Sci.Technol.

Effect of Erbium on Precipitation of Aged Al-Zn-Mg-Cu-Li Alloy Zhong-kui ZHAO 1, a, Tie-tao ZHOU 2,b, Pei-ying LIU 2,c and Chang-qi CHEN 2,d 1 Materials Science and Engineering School, Shandong Jianzhu University, Jinan 250101, China 2 Materials Science and Engineering school, Beihang University, Beijing 100083, China ajorezhk@163.com, bttzhou@public.fhnet.cn.net, cpyliu@buaa.edu.cn, dchangqichen@yahoo.com Keywords: erbium; precipitation; Al-Zn-Mg-Cu-Li alloy; ageing Abstract. 0.3%Er is added to Al-5.6Zn-1.9Mg-1.6Cu-1.0Li alloy (in wt.%) to investigate the effect of erbium on microstructure of the alloy.
In this paper, 0.3%Er is added to the Al-5.6Zn-1.9Mg-1.6Cu-1.0Li alloy (in wt.%) to investigate the effect of erbium on the microstructure of the alloy.
Experimental Procedure The composition of the alloys studied is Al-5.6Zn-2.0Mg-1.6Cu-1.0Li-0.24Cr (alloy A) and Al-5.6Zn-1.9Mg-1.6Cu-1.0Li-0.3Er (alloy B) (in wt.%), which were melted by a vacuum furnace and then cast in a water-cooled mould under argon protective condition.
References [1] F.
Forum Vol. 475-479 (2005), p. 325 [4] Z.K.

，and 1,2,4-trichlorobenzene was used as solvent.
The typical 13C NMR spectrum of EPR was presented in Fig.1.
The IR spectrum of EPR in the range of 1300~600cm-1 3.
Table 1.
Polymer Testing 28(2009), P475~479 [4]ASTM D 3900-05.

Fig. 1.
As for the complexed film, the C=N band at around 1629 cm-1 in the Schiff base film shifted to 1607 cm-1 [6].
The result showed C18TSB formed 1:2 type complex with Zn(II) ions.
References [1] G.L.
Liu: Thin Solid Films Vol. 479 (2005), p. 269

Table 1.
Parameters of crack growth model Al-alloys DKtho n P q C 2024 T351 2.857 3.353 0.5 1 1.707´10-10 2219 T87 3.187 2.487 0.5 1 1.149´10-9 7075 T7351 3.297 2.529 0.5 1 6.964´10-10 7178 T7651 3.297 1.800 0.5 1 3.001´10-9 (5) Kr is the residual stress intensity factor due to overload, it is given by (equation 5) and Reff is the effective stress ratio
References [1] Jr J.C.
Mech., 5. (1973) 479-497
Mech. 5 (1973) 479-497

The radiator is shielded by depleted 238U (Fig. 1).
The coefficient of determination R2 reaches values ​​from 0.951 to 1.000 (Table 1).
The equation (1) was used for calculation.
Table 2: Measurements on spruce samples Samples Cross section [mm] Frequency of pulses ρ gravimetric [kg/m3] ρ radiometry [kg/m3] 95% interval of reliability Difference of ρ [%] S4 119/120 4334,2 495,3 561,6 493,0 - 630,2 13,4 S7 118/141 4353,6 496,9 549,5 482,0 - 617,1 10,6 S7 141/118 4304,0 496,9 515,8 448,5 - 583,2 3,8 S12 118/156 4355,8 507,3 554,4 487,5 - 621,4 9,3 S12 156/118 4274,6 507,3 506,0 438,2 -573,8 -0,3 S6 119/175 4358,0 531,2 557,2 490,6 - 623,8 4,9 S6 175/119 4181,6 531,2 583,0 515,0 - 651,0 9,8 S16 120/194 4414,4 479,3 482,6 415,4 - 549,9 0,7 S16 194/120 4224,6 479,3 476,6 408,3 - 544,9 -0,6 S11 119/217 4385,0 527,2 541,2 473,3 - 609,1 2,7 S11 217/119 4152,4 527,2 537,9 470,0 - 605,7 2,0 S15 119/236 4420,6 486,9 500,6 431,2 - 570,0 2,8 S15 236/119 4203,2 486,9 443,1 371,8 - 514,3 -9,0 Acoustic tests Density is a parameter necessary to determine Edyn by acoustic methods.
References [1] J.

Here, the excitation wavelength was 464 nm and the integrated intensities of I0 and I1 were calculated at the wavelengths between 450−479 nm and that of I2 was at 479−750 nm.
Accordingly, the ηint value was calculated by Eq. (1).
Figure 1.
References [1] L.
Commun. 13 (2016) 1−5

Results and discussion Figure 1 shows the X-ray diffraction patterns of the starting and as-milled Mg55Y15Cu30 powders as a function of milling time.
The as-milled Mg55Y15Cu30 powders were hot pressed at 453 K under a pressure of 1.2GPa for 30 minutes.
The high pressure involved during consolidation can thus prolong the existence of amorphous phase inside Mg55Y15Cu30 powders. 20 30 40 50 60 70 80 10h 7.5h 5.0h 2.5h 1.0h 0.0h Relative Intensity (arb. units) 2θ Y Mg Cu 400 500 600 700 10h 7.5h 5.0h 2.5h 1.0h Extho. heat flow (arb. units) Temperature ( K ) T g442K T x 478K Fig.1 X-ray diffraction patterns of mechanically alloyed Mg55Y15Cu30 powders as a function of milling time.
References [1] A.
Forum 2005; 475-479: 3451-3458