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Polymer electrolyte is a good ion conductor in lithium-ion battery with an excellent performance in conductivity, ion mobility and ion transport number.
In the end, numbers of lithium ions have a parallel relationship with relaxation time and elongation of polymer chains.
Brooks [8] have been researched the microstructure of single crystal polymer electrolyte system that containing (PEO) macromolecules of P(EO)3(5 × 106): LiCF3SO3, its reveals crystal structure depends on the size of the grain.

Here in this paper a number of literatures related to optimization of machining parameters are reviewed and the problems related to machining of these Ti-alloys including their effects are summarized.
Fig. 1 Phase diagram of the titanium alloys The microstructures of the Ti-6Al-4V and Ti555.3 alloys are significantly different with respect to the quantities and morphologies of the primary alpha and the transformed beta phases as well as the grain size.
Fig. 2 Microstructure of the titanium alloys [5] Cutting Parameters for Investigation Following the outcomes of research of many researchers it is found that a number of parameters are responsible for proper machining processes.

The total number of aggregated water molecules is proportional to the cluster length.
As a hypothesis, we assume that the deviations cause is changes in the molecules combination geometry into clusters and the cluster different coordination number.
Instead, Pmax is determined by the explosion maximum temperature and the moles additional number formation in explosion products at a system constant volume.
We explained the limited solubility as the all water molecules aggregation by the solute molecules certain number.
Sanket, Development of New Transferable Coarse-Grained Models of Hydrocarbons, J.

Due to their unique properties these materials can be used in a large number of applications.
Estrella, Hydrogen Reduction Route towards the Production of Nano-Grained Alloys - Synthesis and Characterization of Fe2Mo Powder, PhD thesis, Sweden: Department of Material Science and Engineering, Division of Metallurgy of Royal Institute of Technology (2002) [2] M.S.

This increase in number of slip systems at high cutting temperatures could be an explanation to improved ductility of Mg alloys and the resultant continuous chips rather than short breaking chips observed in machining of Mg-Al alloys used in automotive industry such as AM20, AM50, AM60, and AZ91.
Mg-Al alloys with 2 to 9 wt% Al will have more barriers in their dislocations’ path than Mg-Ca (0.8wt%) alloy for the same number of slip systems.
More alloying element in substitutional and/or interstitial form(s) will increase strain fields in both number and intensity.
They used micro grain tungsten carbide inserts.
The FBU formation for the particular case under investigation in this study would be as follow: Stage I (initiation) - thermally softened Mg alloy, with a semi-solid mix at grain boundaries, flows on the rake face of the cutting inserts due to shear action.

However, studies in the subject simultaneously bring a number of issues to light, which require further understanding.
We hold that currently it is viable to concentrate attention on solving the problems of the first stage; interest in such problems is evident in a number of publications [10-14].
Table 1 – Strength of composites in various storage conditions [MPa] Hardening time, [days] Cement Fine-grained cement Composite binder with 50% MA1 additive Composite binder with 50% MA2 additive storage in water air storage storage in water air storage storage in water air storage storage in water air storage 3 12,4 15,4 22,3 22,3 6 7,9 7,6 10,1 6 25,4 19,7 30,9 22,9 8,9 8,3 11,8 9,6 28 49,7 22,6 60,2 29,3 28 8,5 38,9 10,8 Curing under water allows to assess the potential for binder application, while curing under dry conditions simulates behavior of the material in the printed structure.
Conclusion Based on the above, development of composites for construction printing shall be based on a number of principles.
At that, it is assumed, that adjusting its ratio, coarseness and grain distribution one may significantly influence the efficiency of mold compounds being produced.

The dislocation density was low, but sub-grains of one to a few micrometres were observed.
The module includes: (i) nucleation laws predicting the number of stable nuclei formed at each time step; (ii) rate laws calculating the dissolution or the growth rate of particles within each discrete size class; and (iii) a continuity equation, tracking the solute tied up as precipitates.

Stamatakis pointed out that to attenuate the 300~400nm ultraviolet ray the optimal grain size of the spherical TiO2 is 50~120nm, which is close to our calculation result.
Table 6 The thickness of topcoat Mass fraction (%) of nano-TiO2 Serial number 1 2 3 4 5 0 0.98 2.1 3 46µm 43 µm 48µm 45 µm 42 µm 45µm 42µm 46 µm 43 µm 45 µm 41µm 45 µm 43µm 46 µm 43 µm 42µm 44 µm 43 µm 45 µm 46 µm Adhesion force.
Table 8 The resisting impact strength of topcoat Mass fraction (%) of nano-TiO2 Serial number 1 2 3 4 5 0 0.98 2.1 3 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.50J 0.40J 0.40J 0.40J 0.40J 0.40J Hardness.
Table 9 The hardness of topcoat Mass fraction (%) of nano-TiO2 Serial number 1 2 3 4 5 0 0.98 2.1 3 0.52 0.54 0.51 0.55 0.52 0.56 0.58 0.55 0.60 0.58 0.59 0.60 0.62 0.63 0.61 0.62 0.64 0.63 0.65 0.64 Water fastness.
Table 10 The water fastness of topcoat Mass fraction (%) of nano-TiO2 Serial number 1 2 3 4 5 0 0.98 2.1 3 <120h <120h <120h <120h <120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h ＞120h Aging resistance.

It was proposed that the amount of retained martensite increases with increased number of training and thereby promotes the TWME [6].
We have conducted a large number of strain-temperature measurements which encompass the stress-assisted two-way memory effect (SATWME) and TWME.
Increase in the number of training cycles resulted in the progressive increase of Ms, while showing progressive decrease of As-temperature.
These dislocations tangles and the density increases with increased number of training cycles.
Deforming the specimen beyond the stress-plateau region causes further detwinning and reorientation of martensite, accompanied by a high density of dislocations forming at the grain boundaries (Fig. 12(a)).

An average diameter of beta grain is around 20 μm.
Plain fatigue properties in air: Maximum cyclic stress-fatigue life (the number of cycles to failure) curves, i.e., S-N curves, obtained from plain fatigue tests on TNTZST and TNTZCR conducted with various thermomechanical treatments in air are shown in Fig. 2, along with ranges of fatigue limits of hot-rolled and cast Ti-6Al-4V ELI and Ti-6Al-7Nb [12].
in air. 300 400 500 600 700 800 900 300 400 500 600 700 800 900 Maximum Cyclic Stress,σmax/MPa Number of Cycles to Failure，Nf 105 106 107 104 Fati gue Limit Range of Ti-6Al-4V ELI Fati gue Limit Range of Ti-6Al-7Nb TNTZST TNTZST Aged at 598 K TNTZST Aged at 673 K TNTZST Aged at 723 K TNTZCR Aged at 598 K TNTZCR Aged at 673K TNTZCR TNTZCR Aged at 723 K Non Failure at 107 Cycles High Cycle Fatigue Life Region Low Cycle Fati gue Li fe Region with that of TNTZST and TNTZCR in both the low-(less than 10 5 cycles) and high-cycle (more than 105 cycles) fatigue life regions.
The notch fatigue strengths of aged TNTZST and TNTZCR at stress concentration 10 104 105 106 107 108 3 200 300 400 500 600 700 Maximum Cyclic Stress, σmax/MPa Number of Cycles to Failure, Nf TNTZST TNTZST Aged at 598 K TNTZST Aged at 673 K TNTZST Aged at 723 K TNTZCR Aged at 598 K TNTZCR Aged at 673K TNTZCR TNTZCR Aged at 723 K Fig. 3 S-N curves of TNTZ subjected to various thermo-mechanical treatments obtained from notchfatigue tests at (a) stress concentration factors of 2 and (b) 6 in air. 100 200 300 400 500 10 104 105 106 107 108 3 Maximum Cyclic Stress, σmax/MPa Number of Cycles to Failure, Nf (a) (b) 10 104 105 106 107 108 3 200 300 400 500 600 700 Maximum Cyclic Stress, σmax/MPa Number of Cycles to Failure, Nf TNTZST TNTZST Aged at 598 K TNTZST Aged at 673 K TNTZST Aged at 723 K TNTZST TNTZST Aged at 598 K TNTZST Aged at 673 K TNTZST Aged at 723 K TNTZCR Aged at 598 K TNTZCR Aged at 673K TNTZCR TNTZCR Aged at 723 K
TNTZCR Aged at 598 K TNTZCR Aged at 673K TNTZCR TNTZCR Aged at 723 K Fig. 3 S-N curves of TNTZ subjected to various thermo-mechanical treatments obtained from notchfatigue tests at (a) stress concentration factors of 2 and (b) 6 in air. 100 200 300 400 500 10 104 105 106 107 108 3 Maximum Cyclic Stress, σmax/MPa Number of Cycles to Failure, Nf (a) (b) factors of 2 and 6 decrease by 30% to 40% and 50% to 60%, respectively, as compared with the plain fatigue strengths in the low-fatigue life region (Fig. 2).