Open Access
Issue
BIO Web Conf.
Volume 17, 2020
International Scientific-Practical Conference “Agriculture and Food Security: Technology, Innovation, Markets, Human Resources” (FIES 2019)
Article Number 00018
Number of page(s) 6
DOI https://doi.org/10.1051/bioconf/20201700018
Published online 28 February 2020

© The Authors, published by EDP Sciences, 2020

Licence Creative CommonsThis is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

1 Introduction

The principle of oils and various technical fluids of purification and drying in force fields remains one of the most common. Various kinds of centrifuges and separators are widely used for this purpose. The principal disadvantage of all centrifuges and separators is the quality deterioration of oil purification at its lowering temperature, the devices complexity and low reliability [1, 2].

Recently, hydrocyclone units have been increasingly used for the various liquids purification, where solid particles are released from the purified oil stream under the influence of centrifugal forces. Hydrocyclone units are more reliable because they have no rotating parts, low cost, and easy maintenance. They can be installed in various places without perpendicular [3, 4]. Nowadays, many research centers are working on the hydrocyclone units’ use for the various liquids purification.

A hydrocyclone (Fig. 1) is an apparatus consisting of a cylindrical part 1, to which a conical part 7 adjoins the bottom with a wide base, and an intermediate drain chamber 3 with a branch pipe for discharging the top product. The diaphragm 6 is installed between the cylindrical part and the drain chamber, and replaceable nozzles 8 are fixed in the lower part of the cone.

Hydrocyclone for the purification of the emerged motor oil works as follows. Polluted oil under pressure enters through a device for admission 3 of cleaning oil tangentially into the cylindrical part of the body 1 and, acquiring a rotational motion, moves into the conical part of the body 1. This causes significant centrifugal forces exceeding gravity.

The heavier fractions of the purified oil under centrifugal forces move from the hydrocyclone axis to the walls of its body 1 in a spiral trajectory downward. Then the heavy fractions are removed from the hydrocyclone through the drain pipe 7. The lighter fractions move in the inner spiral flow, directed upwards, inside the diaphragm 2. Then they enter to the internal part of the lid 5 and are removed through the device for draining cleaned oil 4 outside.

thumbnail Fig. 1.

Hydrocyclone diagram (explanations are in the text)

2 Particle settling diameter determination

2.1 Theoretical investigations

The separation process of emerged oils into fractions in a hydrocyclone can be represented as follows. The following forces act on a particle that is in a fluid flow in a hydrocyclone (fig. 2): the centrifugal force Pz, throwing the particle to the periphery; the radial force Pr, arising the particle from the action of the radial fluid flow and directed to the apparatus axis; Coriolis force Pk, which moves a particle in a circumferential direction relative to the flow; the resistance force of the environment Pc, preventing the particle settling deposition; inertial force Pu, which appears as a result of a particle settling speed change.

If the particle is small and carries along by the flow into rotational motion with an angular velocity ω, then the main force acting on it is centrifugal one (Shestov, 1967)Pz=m·ω2·r=π·δ2·ρ·ω2·r6=π·δ2·ρ·v26r,$$ {P_z} = m \cdot {\omega ^2} \cdot r = \frac{{\pi \cdot {\delta ^2} \cdot \rho \cdot {\omega ^2} \cdot r}}{6} = \frac{{\pi \cdot {\delta ^2} \cdot \rho \cdot {v^2}}}{{6r}}, $$(1)

where m – is the particle mass, kg; ω – is the angular velocity of rotation, s−1; r – is the particle rotation radius, m; δ – is the particle diameter, m; ρ – is the particle density, kg/m3; v – is the linear local flow velocity, m/s.

We can observe the Stock-Soviet (laminar) mode of particles sedimentation in the oil flow, ensuring their separation into phases by a spiral-like movement of the fluid flow in a hydrocyclone. If we take into account the centrifugal force Rz action and the medium resistance force Pc, then from expression (1) with consideration for the medium resistance force, we get:π·δp2·ρp·v26r=24μvs·δp·ρl·π·δp24·ρl·vs22$$ \frac{{\pi \cdot \delta _p^2 \cdot {\rho _p} \cdot {v^2}}}{{6r}} = \frac{{24\mu }}{{{v_s} \cdot {\delta _p} \cdot {\rho _l}}} \cdot \frac{{\pi \cdot \delta _p^2}}{4} \cdot \frac{{{\rho _l} \cdot v_s^2}}{2} $$(2)

where ρl is the liquid density, kg/m3; vs – is the separation rate (solid particles of insoluble impurities release from the oil), m/c; μ is the kinematic viscosity of the oil being cleaned, m2/s.

Thenv2r=18·vs·μδp2·ρp$$ \frac{{{v^2}}}{r} = \frac{{18 \cdot {v_s} \cdot \mu }}{{\delta _p^2 \cdot {\rho _p}}} $$(3)

The inertial force Pu is due to a change in the relative particle velocity in the medium flow when the particle velocity profile is rearranged at the entrance to the cylindrical part of the hydrocyclone. The fluid flow enters the cyclone with the initial velocity vH (the fluid velocity in the inlet nozzle of the cyclone); then the velocity profile changes along line 1-1 (Fig. 2). The velocity profile vH (Fig. 2. line 2-2) is changed by a fluid transition into a curving duct of the inlet nozzle and its distribution over the inlet channel cross section corresponds to the law (Shestov, 1967) of variation the tangential velocity from radius.vrn=const,$$ v{r^n} = const, $$(4)

where n is a freedom indicator.

Then the fluid velocity distribution in the curvilinear channel (line 2–2 in Figure 2) will be determined by the dependence:v=vH(R2-R1)rlnR2R1,$$ v = \frac{{{v_H}\left( {{R_2} - {R_1}} \right)}}{{r\;\ln \;\frac{{{R_2}}}{{{R_1}}}}}, $$(5)

where R2 is the fluid flow outer radius, equal to the hydrocyclone radius R2 = Rz, m; R1 is the fluid flow internal radius in a hydrocyclone, m

Substituting (5) in (3) we get:υi(R2-R1)2r3(lnR2R1)2=18·vs·μδp2·ρp.$$ \frac{{{\upsilon _i}{{\left( {{R_2} - {R_1}} \right)}^2}}}{{{r^3}\left( {\ln \frac{{{R_2}}}{{{R_1}}}} \right)^2}} = \frac{{18 \cdot {v_s} \cdot \mu }}{{\delta _p^2 \cdot {\rho _p}}}. $$(6)

Taking as a current radius r its average value:ra=R2+R12,$$ {r_a} = \frac{{{R_2} + {R_1}}}{2}, $$(7)

We get a generalized dependence characterizing the minimum diameter of the deposited particles:δp.min=18·vs·μ·D2,5·vi2·ρp,$$ {\delta _{p.\min }} = \sqrt {\frac{{18 \cdot {v_s} \cdot \mu \cdot D}}{{2,5 \cdot v_i^2 \cdot {\rho _p}}},} $$(8)

where D is cyclone diameter D=2R2, m

However, the use of the average value radius allows determining only the particles diameter locating at a given radius, and does not allow obtaining the real diameter of the deposited particle. To solve this problem, it is necessary to use the radius value of zero vertical velocity. If we assume that there is no vertical effect on the particle in the cyclone flow, then each particle will be suspended at a certain distance from the center of rotation, that is, at a distance where the centrifugal force will be equal to the radial force Pz = Pr.

Heavier particles will be located closer to the hydrocyclone periphery, and light ones will be located at its center. Each group of particles in the oil flow in the inner conical hydrocyclone cavity will create a curved-linear surface (Fig. 3) when they are moving.

Zero vertical velocity points (that is, the boundaries of the vertical velocity signs change) also create a curved surface. The intersection or coincidence of the vertical velocity plane with the plane of any group particles will give the value of the boundary grain, with the larger grain going to the drain and the smaller grain to the cleaned stream.

It is necessary to determine the axial velocity of a particle moving in a hydrocyclone flow to define the radius of the zero surface.

We use the formula to calculate the axial velocity [4]:υz=G4πcosα120H+H1dh02π(R0-htgα12)[(h-z)2+(R0-htgα12)2-(R0-htgα12)Rcosβ+R2-2Rcosβ(R0-htgα12)]3/2dβ,$$ \begin{aligned}{\upsilon _z} = \frac{G}{{4\pi \cos \frac{{{\alpha _1}}}{2}}}\int\limits_0^{H + {H_1}} {dh\int\limits_0^{2\pi } {\frac{{\left( {{R_0} - htg\frac{{{\alpha _1}}}{2}} \right)}}{{\left[ {{{\left( {h - z} \right)}^2} + {{\left( {{R_0} - htg\frac{{{\alpha _1}}}{2}} \right)}^2}} \right.}}} }\cr \frac{{ - \left( {{R_0} - htg\frac{{{\alpha _1}}}{2}} \right)R\cos \beta }}{{{{\left. { + {R^2} - 2R\cos \beta \left( {{R_0} - htg\frac{{{\alpha _1}}}{2}} \right)} \right]}^{{3/2}}}}}d\beta, \end{aligned} $$(9)

where G=const is the velocity circulation per unit of the toroid heightG=2πrvt;$$ G = 2\;\pi \;r\;{v_t}; $$(10)

Ro is the surface radius of zero axial velocities at the boundary of the cylindrical and conical parts of the hydrocyclone, mRI^=rorc+rn(RG+Htgα2)$$ {R_{\widehat I}} = \frac{{{r_o}}}{{{r_c} + {r_n}}}\left( {{R_G} + Htg\frac{\alpha }{2}} \right) $$(11)

where RΓ is the radius of the hydrocyclone, m; ro is the radius of the air column (ro = 0,606rc), m; rc is the radius of cleaned oil discharging, m; rn is the radius of the drain pipe, m; α1 is the taper angle of the hydrocyclone, deg.; β is the angle of inclination or the offset angle of a point when moving in a vortex layer to a height (h-z), deg.; h is the distance of the considered annular section from the beginning of the vortex layer (i.e, from the top lid of the hydrocyclone cylindrical part), m; H is the height of the hydrocyclone conical part, m; H1 is the height of the hydrocyclone cylindrical part, m.

Tangential velocity of the particleυt=C·r00H+H1dh02πR[(h-z)2+rn+R2-2rncosβ]-rncosβ(rn2+R2-2R0cosβ)dβ,$$ \begin{gathered}{\upsilon _t} = C \cdot {r_0}\int\limits_0^{H + {H_1}} {dh\int\limits_0^{2\pi } {\frac{R}{{\left[ {{{\left( {h - z} \right)}^2} + {r_n} + {R^2} - 2{r_n}\cos \beta } \right]}}} } \hfill \\ \frac{{ - {r_n}\cos \beta }}{{\left( {r_n^2 + {R^2} - 2{R_0}\cos \beta } \right)}}d\beta, \end{gathered} $$(12)

where C is a constant value characterizing the dependence of productivity on the hydrocyclone height; rH is the outer diameter of the considered annular section, m; R and z are the coordinates of the point for which the velocity is determined, m; vt — tangential velocity of the particle, m/s; dh is the height of the considered ring, m;tgα12=rorc+rntgα2,$$ tg\frac{{{\alpha _1}}}{2} = \frac{{{r_o}}}{{{r_c} + {r_n}}}tg\frac{\alpha }{2}, $$(13)

Axial velocity of a particleυz=2πrCr04πcosα120H+H102πR[(h-z)2+rn+R2-2rncosβ]-r0cosβ(r02+R2-2R0cosβ)××0H+H1dh02π[(R0-htgα12)2[(h-z)2+(R0-htgα12)-(R0-htgα12)Rcosβ]+R2-2Rcosβ(R0-htgα12)]32dβdh$$ \begin{gathered}{\upsilon _z} = \frac{{2\pi rC{r_0}}}{{4\pi \cos \frac{{{\alpha _1}}}{2}}}\int\limits_0^{H + {H_1}} {\int\limits_0^{2\pi } {\frac{R}{{\left[ {{{\left( {h - z} \right)}^2} + {r_n} + {R^2} - 2{r_n}\cos \beta } \right]}}} } \hfill \\ \frac{{ - {r_0}\cos \beta }}{{\left( {r_0^2 + {R^2} - 2{R_0}\cos \beta } \right)}} \times \hfill \\ \times \int\limits_0^{H + {H_1}} {dh\int\limits_0^{2\pi } {\frac{{\left[ {{{\left( {{R_0} - htg\frac{{{\alpha _1}}}{2}} \right)}^2}} \right.}}{{\left[ {{{\left( {h - z} \right)}^2} + \left( {{R_0} - htg\frac{{{\alpha _1}}}{2}} \right)} \right.}}} } \hfill \\ \frac{{\left. { - \left( {{R_0} - htg\frac{{{\alpha _1}}}{2}} \right)R\cos \beta } \right]}}{{{{\left. { + {R^2} - 2R\cos \beta \left( {{R_0} - htg\frac{{{\alpha _1}}}{2}} \right)} \right]}^{\frac{3}{2}}}}}d\beta dh \hfill \\ \end{gathered} $$(14)

In order to establish a criterial form communication in the form of a regression model of the zero surface radius dependence Ro on the hydrocyclone parameters, we compose a matrix, taking as predictors: the height of the hydrocyclone working part H+H1, the particle coordinate according to the hydrocyclone radius R, the particle coordinate according to the hydrocyclone height H+H1, distance to the considered section h of the hydrocyclone conical part, diameter of the section d, axial velocity vz (Table 1).

The regression equation will beRo=ao+a1X1+a2X2++anXn=0;$$ {R_o} = {a_o} + {a_1}{X_1} + {a_2}{X_2} + \ldots + {a_n}{X_n} = {\text{ }}0; $$(15)

where ao, a1,...aп are regression coefficients with selected parameters of a hydrocyclone; X1, X2, … Xn are the parameters of the hydrocyclone.

Having preliminary information about the influence of the hydrocyclone listed parameters on the radius of the surface of zero axial velocity, we present the functional dependence in general formRo=f(α,R,h,z,d).$$ {R_o} = f{\text{ }}(\alpha ,{\text{ }}R,{\text{ }}h,{\text{ }}z,{\text{ }}d). $$(16)

To calculate the coefficients, we determine the change in the axial velocity and the coordinates of a particle moving in a vortex flow of a hydrocyclone at three points of the section along the height and ten points along the radius of the hydrocyclone [5, 6, 7]. In this case, the particle coordinate z will take certain numerical values depending on the diameter of the section, and accordingly, on its position along the height of the hydrocyclone. Given the condition that the z coordinate is a numerical variable value, we will get:

ro,Ro,a,p,r,h=const;$$ {r_o},{\text{ }}{R_o},{\text{ }}a,{\text{ }}p,{\text{ }}r,{\text{ }}h = const; $$(17)

that is, only the coordinate of the point being examined will change R. After calculating the position of the point, we will obtain a series of numerical values of the main parameters.

thumbnail Fig. 2.

Forces, acting on a particle in a spiral flow in a hydrocyclone

thumbnail Fig. 3.

Diagram of particle surfaces in a hydrocyclone flow

Table 1.

Matrix for the establishment of communication in the criterial form

3 Research results

A quadratic equation of the axial velocity of the particle in the flow is obtained after determining the coordinates of changing the position of a particle in a hydrocyclone flow and calculating the regression coefficients. After substituting into it the boundary values of the predictors defined for these specific conditions (h = 0,01–0,18 m, R0 = 0,02 m, ro = 0,017 m, α = 5o2′, H+Ho = 0,302 m, β = 100–1200, R = 0,018–0,046 m), and transformations, a theoretical dependence of the axial velocity of a particle in a flow, on the design and technological parameters of a hydrocyclone depending on the required values of the quality of oil cleaning is obtained.υz=Y=(-244,524-30)-19769,382r-+138.852z+31610,804C+1373,869r2++227914.938r2-17399,748z2+158265,452C2-88475,75R2.$$ \begin{gathered}{\upsilon _z} = Y = \left( { - 244,524 - 30} \right) - 19769,382\,r - \hfill \\ + 138.852\,z + 31610,804\,C + 1373,869\,{r^2} + \hfill \\ + 227914.938\,{r^2} - 17399,748\,{z^2} + \hfill \\ 158265,452\,{C^2} - 88475,75\,{R^2} \hfill \\ \end{gathered}. $$(18)

For the calculations of the boundary layer radius (zero surface), the dependence of the hydrocyclone parameters is obtained: radius R, height (as a function of performance) C on the particle coordinate in the cleaning flow z:R=0,0385-0,833r-0,0072z-0,347C,$$ R = 0,0385 - 0,833\,r - 0,0072\,z - 0,347\,C, $$(19)

Substitute zero surface radius equation (17) of the axial velocity in expression (6), replacing the value of the diameter of the hydrocyclone D by the radius of the zero surface 2Ro. Then we will get the size of the particles separated at a certain radius of the cyclone:δp.min=36υcμRo2,5υn2ρp$$ {\delta _{p.\min }} = \sqrt {\frac{{36{\upsilon _c}\mu {R_o}}}{{2,5\upsilon _n^2{\rho _p}}}} $$(20)

The obtained dependence clearly shows the relationship of each quantity in the radicand with the size of the particles separated in the spiral flow of the hydrocyclone. At the same time, the size of separated particles will increase with the increase in the radius of the zero surface. Therefore, reduced diameters hydrocyclones should be used to trap fine particles [5, 6]. Increasing of the initial flow velocity of the cleaned oil vH (in the cyclone inlet) also contributes to the separation of smaller particles.

The using of expression (18) to determine the minimum size of a detachable particle for practical purposes is not always possible, since it contains an unknown quantity — the separation velocity vc.

To determine the separation velocity, we assume that the particle entering the cyclone near the inlet nozzle (radius R1) must settle on the wall of the cyclone during its passing through the cylindrical-conical part of the cyclone.τ=R2-R1υc=VhQh=πHR2-R1Qh,$$ \tau = \frac{{{R_2} - {R_1}}}{{{\upsilon _c}}} = \frac{{{V_h}}}{{{Q_h}}} = \pi H\frac{{{R_2} - {R_1}}}{{{Q_h}}}, $$(21)

where Vh is the volume of the hydrocyclone cylindrical-conical part, m3; Qh is the hydrocyclone productivity, m3/h; H is the height of the hydrocyclone cylindrical-conical part, m.

Whereas the separation of particles occurs at radius Ro, replacing R2-R1 with Ro, we getτ=πHRl^Qh$$ \tau = \pi H\frac{{{R_{\widehat l}}}}{{{Q_h}}} $$(22)

In this case, the particle settling rateυn=QhπHRo$$ {\upsilon _{\widetilde n}} = \frac{{{Q_h}}}{{\pi H{R_o}}} $$(23)

Three quantities are essential for separation of a particle in a hydrocyclone: the separation rate vc, the thickness of the deposition layer and the residence time of the particle in the hydrocyclone τ.

A parameter can be made up of these three quantities – a separation criterion that determines the amount of particles to be separated from the purified oil stream.Kc=υcτλ,$$ {K_c} = \frac{{{\upsilon _c}\tau }}{\lambda }, $$(24)

where λ is the thickness of the deposition layer, m.

Since the thickness of the deposition layer is determined by the boundary values of the radii RzRo, thenλ=Rz-Ro,$$ \lambda = {R_z} - {R_o}, $$(25)

Since the quality of cleaning determines the amount of deposited impurities, we replace the volume of supplied oil with the amount of impurities in the cleaned oil. Performing the replacement and substituting the value of vc in the formula (22), we getKc=GhτRzπH,$$ {K_c} = \frac{{{G_h}\tau {R_z}}}{{\pi H}}, $$(26)

where Gh is the amount of impurities in the cleaned oil, kg.

In this case, the quality of hydrocyclone cleaning can be defined as the particles entrainment through a drain hole, expressed as a percentage of the particles total number entering the hydrocyclone with the cleaned oil:ϕ=Gh-KcGh.$$ \phi = \frac{{{G_h} - {K_c}}}{{{G_h}}}. $$(27)

Thus, the quality of oil purification will be determined by the geometrical parameters of the hydrocyclone and the residence time of the particle in the hydrocyclone, depending on the separation mode.

The comparative laboratory studies of the efficiency of purification of spent mineral oil from insoluble impurities using experimental and controlling hydrocyclones were carried out to confirm the obtained theoretical calculations. A hydrocyclone made according to the calculating method of its geometrical parameters recommended by most researchers was used as a controlling [810].

In the process of research, it was found that an experimental cylindro-conical hydrocyclone, with geometrical parameters set in accordance with the theoretical calculations, provides the best degree of purification (88.4%) with a process productivity of 3...5 t/h, input flow pressure P = 0.04 MPa and the diaphragm seal immersion depth of a hydrocyclone H = 136.8 mm, contrary to 21.6% for a typical hydrocyclone.

4 Conclusion

The purification degree of oil from insoluble impurities will be determined by the geometrical parameters of the hydrocyclone: radius Rz, the height of the cylindrical-conical part H and the time the particle stays in the hydrocyclone, depending on the separation mode. The results of the comparative laboratory studies show that the calculations of the structural and technological parameters of the hydrocyclone according to the proposed method provides a higher degree of purification of spent mineral oils from insoluble impurities.

References

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All Tables

Table 1.

Matrix for the establishment of communication in the criterial form

All Figures

thumbnail Fig. 1.

Hydrocyclone diagram (explanations are in the text)

In the text
thumbnail Fig. 2.

Forces, acting on a particle in a spiral flow in a hydrocyclone

In the text
thumbnail Fig. 3.

Diagram of particle surfaces in a hydrocyclone flow

In the text

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