Sort by:
Publication Type:
Open access:
Publication Date:
Periodicals:
Search results
Online since: July 2021
Authors: Ilya V. Gorshkov, M.A. Popov, Aleksei D. Khalimonenko, E.G. Zlotnikov
Cutting ceramic composition: 1 - aluminum oxide (Аl2О3); 2 - refractory metal carbides (TiС, WC, MoC)
The main factors affecting the cutting properties of ceramic cutting inserts are the microstructural parameters of the material, which include the number, distribution pattern and size of carbide inclusions.
The more ceramic grains are distributed over the area of ceramic plates and the smaller their size, the better the cutting properties and performance of the tool material [1-3].
Result and Discussion Studies have shown [1] that ceramic plates with the smallest diameters and with the largest number of carbide grains distributed over the area have a higher electrical resistance (about 100 Ω), and ceramic plates with the smallest diameters and with the least amount of carbide grains distributed over the area have lower electrical resistance (about 10 Ω).
As can be seen from the applied materials (Fig. 5), for ceramic specimens with an electrical resistance close to R = 100 Ω, the distribution of carbide grains is larger over the area and their size is smaller than for ceramic specimens with an electrical resistance close to R = 10 Ω.
The more ceramic grains are distributed over the area of ceramic plates and the smaller their size, the better the cutting properties and performance of the tool material [1-3].
Result and Discussion Studies have shown [1] that ceramic plates with the smallest diameters and with the largest number of carbide grains distributed over the area have a higher electrical resistance (about 100 Ω), and ceramic plates with the smallest diameters and with the least amount of carbide grains distributed over the area have lower electrical resistance (about 10 Ω).
As can be seen from the applied materials (Fig. 5), for ceramic specimens with an electrical resistance close to R = 100 Ω, the distribution of carbide grains is larger over the area and their size is smaller than for ceramic specimens with an electrical resistance close to R = 10 Ω.
Online since: September 2010
Authors: Támas Korim
Changes in
macrostructure resulting from repeated thermal shocks were studied and a decrease in both the
number and size of intergranular and intragranular interlacing fractures was observed [8]; this is the
so-called self-healing effect.
Figure 3 demonstrates the change in flexural strength of doped AT samples as a function of number of thermal shock cycles.
After the 10 th cycle this process reverses and more and larger fractures develop in the structure, which reduces strength inevitably. 0 5 10 15 20 25 30 35 0 5 10 15 20 25 30 35 40 45 number of cycles flexural strenght AT ATF05 ATF1 ATF2 ATF3 ATF5 Fig. 3 Change in flexural strength of Fe2O3 doped AT samples as a function of number of thermal shock cycles Morphological analyses were performed to support the results of strength tests.
Individual grain sizes vary in the range of 40-60 µm.
In the electron microscope image taken after the 10 th cycle (Figure 5) no further structural degradation can be detected, on the contrary, the number of fractures in the sample decreased and there are smaller and allied grains (with size about 10-30 µm).
Figure 3 demonstrates the change in flexural strength of doped AT samples as a function of number of thermal shock cycles.
After the 10 th cycle this process reverses and more and larger fractures develop in the structure, which reduces strength inevitably. 0 5 10 15 20 25 30 35 0 5 10 15 20 25 30 35 40 45 number of cycles flexural strenght AT ATF05 ATF1 ATF2 ATF3 ATF5 Fig. 3 Change in flexural strength of Fe2O3 doped AT samples as a function of number of thermal shock cycles Morphological analyses were performed to support the results of strength tests.
Individual grain sizes vary in the range of 40-60 µm.
In the electron microscope image taken after the 10 th cycle (Figure 5) no further structural degradation can be detected, on the contrary, the number of fractures in the sample decreased and there are smaller and allied grains (with size about 10-30 µm).
Online since: May 2012
Authors: K. Khan
The spinel ferrites show interesting structural properties in the nano crystalline form compared with those of the micrometer-size grains.
A series of CoFe2-2xZrxMnxO4 (0.10.4) spinel ferrite samples are prepared by the chemical co-precipitation method [6] and the changes in a number of parameters, namely, lattice parameter, porosity, X-ray density and bulk density have been reported.
The theoretical density was calculated using the formula (5) where 8 stands for the number of formula units in a unit cell, N is the Avogadro’s number, M is the molecular weight of the one formula unit and V is the volume of the unit cell.
The resistivity of the ferrites in general, depends on different factors such as the density, porosity, grain size etc.
n =NADmPFe / M (7) where NA, Dm and M are the Avogadro’s number, mass density and molecular weight of the corresponding sample, respectively and PFe is the number of iron atoms in the formula CoFe2-2xZrxMnxO4 (0.10.4).
A series of CoFe2-2xZrxMnxO4 (0.10.4) spinel ferrite samples are prepared by the chemical co-precipitation method [6] and the changes in a number of parameters, namely, lattice parameter, porosity, X-ray density and bulk density have been reported.
The theoretical density was calculated using the formula (5) where 8 stands for the number of formula units in a unit cell, N is the Avogadro’s number, M is the molecular weight of the one formula unit and V is the volume of the unit cell.
The resistivity of the ferrites in general, depends on different factors such as the density, porosity, grain size etc.
n =NADmPFe / M (7) where NA, Dm and M are the Avogadro’s number, mass density and molecular weight of the corresponding sample, respectively and PFe is the number of iron atoms in the formula CoFe2-2xZrxMnxO4 (0.10.4).
Online since: September 2013
Authors: De Qiang Li, Hua Xu
Such as Tab 1:
Tab 1: Type and technology of new energy vehicles
New Energy Vehicles
Type
Technology
Energy/Fuel Source
New Fuel Vehicles
clean diesel
oil
reformulated gasoline (RFG)
oil
Gas Vehicles
liquefied petroleum gas (LPG)
oil
liquefied natural gas (LNG)
natural gas
compressed natural gas (CNG)
natural gas
Biofuel Vehicles
bioethanol
grain/non-grain crops
biodiesel
animal and plant oil
Coal-based Methanol and Diethyl Ether Vehicles
coal-methanol
coal
coal-diethyl ether
coal
Electric Vehicles
hybrid electric vehicles (HEV)
oil/ electric power
pure electric vehicles (PEV)
electric power
fuel cell electric vehicles (FCEV)
hydrogen/electric power
solar cell vehicles
solar
The Development of New Energy Vehicles
New Techniques Become More Sophisticated to Promote the Development of New Energy Vehicles.
China's urban new energy vehicle charging system, the backwardness of the infrastructure has also led to a number of potential consumers in a wait state.
We should steer a number of enterprise-led, research institutions and universities actively involved in industrial technology innovation alliance.
We should encourage the relevant social subjects participate actively, increase investment to development a number of the industry chain aggregation requirements, has strong technical innovation ability is the key part of the enterprise, respectively, cultivate backbone enterprises in the drive motor, the efficient transmission and other fields, the professional automotive electronics enterprises participation shares, with strong international competitiveness and support the development of automobile enterprises.
We should encourage the social subjects to actively participate in and to increase investment for developing some enterprises that is in compliance with a number of industry chain aggregation requirements ,and these enterprises have a strong technological innovation capability key parts, foster leading enterprises in the field of drive motor, high efficiency transmission.
China's urban new energy vehicle charging system, the backwardness of the infrastructure has also led to a number of potential consumers in a wait state.
We should steer a number of enterprise-led, research institutions and universities actively involved in industrial technology innovation alliance.
We should encourage the relevant social subjects participate actively, increase investment to development a number of the industry chain aggregation requirements, has strong technical innovation ability is the key part of the enterprise, respectively, cultivate backbone enterprises in the drive motor, the efficient transmission and other fields, the professional automotive electronics enterprises participation shares, with strong international competitiveness and support the development of automobile enterprises.
We should encourage the social subjects to actively participate in and to increase investment for developing some enterprises that is in compliance with a number of industry chain aggregation requirements ,and these enterprises have a strong technological innovation capability key parts, foster leading enterprises in the field of drive motor, high efficiency transmission.
Online since: October 2014
Authors: Marius Turnea, Dragos Arotaritei, Mariana Rotariu, Mihai Ilea
The proliferation stage is characterized by angiogenesis, collagen deposits, tissue grain formation, epithelization and wound shrinking.
In kinetic theory for active particles, biphasic systems are characterized by a number of system evolution description variables which is higher than the number of evolution equations.
It is the result of a grain tissue overgrowth (type 3 collagen) where a healed wound used to be and which is progressively replaced by type 1 collagen.
(4) Results The simulations are performed after tegument injury (wound infliction) when the number of AV is equal to the number of ISc of the immune system.
The activity of the entities at microscopic level u is assumed within the [0,3] range, the number of nodes used for the simulation being m= 20.
In kinetic theory for active particles, biphasic systems are characterized by a number of system evolution description variables which is higher than the number of evolution equations.
It is the result of a grain tissue overgrowth (type 3 collagen) where a healed wound used to be and which is progressively replaced by type 1 collagen.
(4) Results The simulations are performed after tegument injury (wound infliction) when the number of AV is equal to the number of ISc of the immune system.
The activity of the entities at microscopic level u is assumed within the [0,3] range, the number of nodes used for the simulation being m= 20.
Online since: June 2012
Authors: Bin Cheng, Zong Zhan Li, Shang Nan Song
Tile board room, with wooden load-bearing structure, creats a unique Shan-jia structure with a large number of wooden components and junction exposed, and it is a variant of multi-column landing Chuandou structure.
Flat Form “|” shape(numbered Str. 1 in the following), is the simplest one, commonly used in houses with small depth and small area.
“十” shape(numbered Str. 2 in the following), is the more common one, with larger number and broader scope.
The residential used in this paper(Fig. 2.b.)has the data: depth 9.60 m, length 15.69 m, height 6.89 m, and has 7 columns vertical, 3 rows horizontal main Shan-jia structure. “✲” shape(numbered Str. 3 in the following), is the relatively rare one in nowadays.
Without measured data, according the “Code for design of timber structures”, the permissible values of the strength of wood in this analysis are set: tensile strength parallel to grain 8.5MPa, compression strength parallel to grain 12MPa.
Flat Form “|” shape(numbered Str. 1 in the following), is the simplest one, commonly used in houses with small depth and small area.
“十” shape(numbered Str. 2 in the following), is the more common one, with larger number and broader scope.
The residential used in this paper(Fig. 2.b.)has the data: depth 9.60 m, length 15.69 m, height 6.89 m, and has 7 columns vertical, 3 rows horizontal main Shan-jia structure. “✲” shape(numbered Str. 3 in the following), is the relatively rare one in nowadays.
Without measured data, according the “Code for design of timber structures”, the permissible values of the strength of wood in this analysis are set: tensile strength parallel to grain 8.5MPa, compression strength parallel to grain 12MPa.
Online since: March 2014
Authors: Xin Chen, Hui Xiang Xu, Yong Qi Wei, Ai Jun Han, Ming Quan Ye, Gong Pei Pan, Ting Liu
Table 2 The test results of Propellant Sensitivity
Number
Li - Al alloy quality ratio of burners/%
Li-Al alloy/g
The impact sensitivity/%
The friction sensitivity/%
0
0
0
0
0
1
5
0.105
0
0
2
10
0.210
4
4
3
15
0.315
4
8
4
20
0.420
12
16
5
25
0.525
16
20
From the table 2, it can be seen that to add the Li-Al alloy powder into the B/PTFE fuel rich propellant, the impact sensitivity and friction sensitivity of the propellant can be improved.
Table 3 The test results of propellant combustion heat Number The grain total quality/g The quality of ignition composition/g The quality of propellant/g The combustion heat of propellant /(MJ/kg) 0 1.48 0.30 1.18 18.172 1 1.26 0.31 0.95 18.528 2 1.33 0.30 1.03 18.728 3 1.26 0.30 0.96 19.153 4 1.31 0.31 1.00 19.339 5 1.31 0.30 1.01 19.464 Fig. 2 The curve of propellant combustion heat As it can be seen from the above, the maximum heat of combustion of the propellant is 19.464 MJ/kg and the minimum heat of combustion is 18.172 MJ/kg.
In the curve of the heat of combustion, the heat of combustion numerical number increases according to the growth of the Li-Al alloy content and presents the distribution law of increasing gradually.
Burning velocity is that the propellant grain push in distance l along its inward propellant combustion surface in t time under certain conditions, its burning rate r = l/t.
Table 4 The test results of propellant burning temperature and burning velocity Number Li-Al alloy/g Burning temperature/°C Burning velocity/(mm/s) 0 0 767 0.16 1 0.105 782 0.15 2 0.21 815 0.18 3 0.315 825 0.20 4 0.42 831 0.21 5 0.525 854 0.24 Fig. 3 The curve of propellant burning velocity Fig. 4 The curve of propellant burning temperature The combustion rate is increased with the increase of the content of Li-Al alloy.
Table 3 The test results of propellant combustion heat Number The grain total quality/g The quality of ignition composition/g The quality of propellant/g The combustion heat of propellant /(MJ/kg) 0 1.48 0.30 1.18 18.172 1 1.26 0.31 0.95 18.528 2 1.33 0.30 1.03 18.728 3 1.26 0.30 0.96 19.153 4 1.31 0.31 1.00 19.339 5 1.31 0.30 1.01 19.464 Fig. 2 The curve of propellant combustion heat As it can be seen from the above, the maximum heat of combustion of the propellant is 19.464 MJ/kg and the minimum heat of combustion is 18.172 MJ/kg.
In the curve of the heat of combustion, the heat of combustion numerical number increases according to the growth of the Li-Al alloy content and presents the distribution law of increasing gradually.
Burning velocity is that the propellant grain push in distance l along its inward propellant combustion surface in t time under certain conditions, its burning rate r = l/t.
Table 4 The test results of propellant burning temperature and burning velocity Number Li-Al alloy/g Burning temperature/°C Burning velocity/(mm/s) 0 0 767 0.16 1 0.105 782 0.15 2 0.21 815 0.18 3 0.315 825 0.20 4 0.42 831 0.21 5 0.525 854 0.24 Fig. 3 The curve of propellant burning velocity Fig. 4 The curve of propellant burning temperature The combustion rate is increased with the increase of the content of Li-Al alloy.
Online since: August 2023
Authors: Ákos Meilinger, Gábor Terdik
Typical coarse-grain (CGHAZ) and fine-grained zone (FGHAZ) can be observed.
There is a significant difference between specimen number 1 and number 4.
In case of number 1, the biggest hardness decrease happened in the heat affected zone, the hardness of base material is around 390 HV, and the lowest hardness is 305 HV.
The softened zone area is almost the same like in case of number 1.
Specimen 3 differs significantly from numbers 1 and 2.
There is a significant difference between specimen number 1 and number 4.
In case of number 1, the biggest hardness decrease happened in the heat affected zone, the hardness of base material is around 390 HV, and the lowest hardness is 305 HV.
The softened zone area is almost the same like in case of number 1.
Specimen 3 differs significantly from numbers 1 and 2.
Online since: July 2015
Authors: Jan W. Coenen, Johann Riesch, Till Höschen, Martin Bram, Bruno Jasper, Christian Linsmeier
The etching method 98c from the ASTM E407 standard for pure tungsten is used to reveal the grain structure [10].
The grain size is determined following the ASTM E112 standard [11] (see Table 1).
Small pores, in the order of 200 nm, are detectable at triple points of grains (see Fig. 5c2). 3-Point Bending Tests.
In addition, the grain structure is coarsened since non doped fibers were used.
In addition, FIB analysis reveals that the erbium oxide of the interface forms a complicated 3D structure between the grains of the matrix.
The grain size is determined following the ASTM E112 standard [11] (see Table 1).
Small pores, in the order of 200 nm, are detectable at triple points of grains (see Fig. 5c2). 3-Point Bending Tests.
In addition, the grain structure is coarsened since non doped fibers were used.
In addition, FIB analysis reveals that the erbium oxide of the interface forms a complicated 3D structure between the grains of the matrix.
Online since: May 2014
Authors: K.P. Yuvaraj, B. Senthilkumar
Asadi et al [28] investigated the effects of water cooling treatment, tool rotational direction and friction stir processing pass number on the mechanical properties of friction stir processed AZ91 magnesium alloy.
It has been found that, the elongated pancakelike grains typically produced in conventional thermomechanical processing of this alloy are replaced by equiaxed grains during FSP and the persistence of a shear type deformation texture in the stir zone reflects DRV and GDRX.
DU XingHao et al [16] have analyzed the two-pass friction stir processing (FSP) technique employed to refine grain sizes to a nanoscale and the efficiency of FSP to produce a nano -grained microstructure in the AZ61 alloy is also investigated.
It is found that, it is possible to control the final microstructure including grain size, grain-boundary structure, and dislocation density by changing the processing parameters and cooling rate.
It has been found that, superior tensile strength can be obtained due to the fine grains in the joint and it yields higher tensile strength.
It has been found that, the elongated pancakelike grains typically produced in conventional thermomechanical processing of this alloy are replaced by equiaxed grains during FSP and the persistence of a shear type deformation texture in the stir zone reflects DRV and GDRX.
DU XingHao et al [16] have analyzed the two-pass friction stir processing (FSP) technique employed to refine grain sizes to a nanoscale and the efficiency of FSP to produce a nano -grained microstructure in the AZ61 alloy is also investigated.
It is found that, it is possible to control the final microstructure including grain size, grain-boundary structure, and dislocation density by changing the processing parameters and cooling rate.
It has been found that, superior tensile strength can be obtained due to the fine grains in the joint and it yields higher tensile strength.