Analysis of progressive cavity pumps specific wear processes using Finnie models

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IOP Conference Series: Materials Science and Engineering PAPER OPEN ACCESS Analysis of progressive cavity pumps specific wear processes using innie models To cite this article: M Popescu et al 217 IOP Conf. Ser.: Mater. Sci. Eng. 174 122 View the article online for updates and enhancements. Related content - Analysis of progressive cavity pumps specific wear processes using Bitter and Hutchings models A I Popovici, M Popescu, N N Antonescu et al. - A NEW EXTENSION O THE HELIX NEBULA G. Araya, V. M. Blanco and M. G. Smith - Accessing commercial cloud resources within the European Helix Nebula cloud marketplace C Cordeiro, A De Salvo, A Di Girolamo et al. This content was downloaded from IP address 4.3.194.15 on /2/218 at 1:4

IOP Conf. Series: Materials Science and Engineering 174 (217) 122 doi:1.188/1757-899x/174/1/122 Analysis of progressive cavity pumps specific wear processes using innie models M Popescu 1, A I Popovici 2, N Petrescu 2 and N N Antonescu 1 1 Petroleum-Gas University of Ploiesti, Blvd. Bucureşti no. 39, code 18, Ploiesti, Romania 2 Department of Mechanical Technology, Technical University of Civil Engineering Bucharest, 59 Plevnei Way, code 1223, Bucharest, Romania E-mail: arys_jo@yahoo.com Abstract. Progressive cavitation pumps are designed to work in aggressive environments thus their wear is inevitable. The specific tribological coupling of these pumps is composed of a helical rotor with a single outward helix and a stator with a double inside helix. These elements are in relative motion and direct contact to each other and also in direct contact with the pumped oil. Therefore the main forms of wear of rotor-stator coupling elements are the abrasive wear and the erosion wear. In this paper is presented the analysis of erosion with innie models. The results are useful for estimation of progressive cavity pumps specific abrasive-erosive wear. 1. Introduction The specific tribological coupling of progressive cavitation pump is composed of a helical rotor with a single outward helix and a stator with a double inside helix. The rotor-stator coupling wear resistance and working life are ensured by high-performance solutions concerning the design and manufacture of progressive cavity pumps. The pumps are designed to work in aggressive environments so their wear is inevitable. Specific tribological processes of progressive cavity pumps can be studied considering the followings: rotor and stator materials; the characteristics of pumped fluid; contamination of oil pumped under pressure. The rotor is made of steel (alloy steel or stainless steel with high hardness) and the stator is made of an elastomer with well-defined properties. The specific couplings components are in relative motion and direct contact with each other and in direct contact with the pumped oil. The wear of the specific tribological coupling of the progressive cavitation pumps (rotor-stator) must be approach in this context. The manner in which is acchived the sealing between the helix of the rotor and the stator in order to ensure the high presure of the fluid in the cavities formed, thus avoiding the reverse flow of discharge chamber to the aspiration chamber is of great tribological interest. Content from this work may be used under the terms of the Creative Commons Attribution 3. licence. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI. Published under licence by Ltd 1

IOP Conf. Series: Materials Science and Engineering 174 (217) 122 doi:1.188/1757-899x/174/1/122 The fluids circulated by progressive cavitation pumps are characterized by the followings: viscosity and specific weight differentiated in a range of relatively high values; the content of solid particles (in some cases can reach up to % sand); water content which can reach up to 9%; the temperature of the pumped liquid that can be relatively high: 12 C for fluids without sand and 4 9 C for fluids containing sand; the existence of corrosive agents in the pumped oil (CO 2, H 2 S or O 2 ). Abrasive wear and erosion wear are the main forms of wear of the coupling components (rotor and stator). Essentially, abrasion and erosion are caused by the impact of the rigid particle on the active surfaces of the pump. The impact is mainly differentiated by the nature of the material subjected to stress: elastic impact and plastic impact. According to Johnson [1] the elastic impact occurs at a speed nearly.1 m/s, and the full plastic penetration occurs at a speed of 5 m/s in progressive cavitation pumps case. or plastic materials the plastic deformation of the target surface occurs at a very low speed (for hard steel with σ c = 1 N/mm 2, the impact speed is.14 m/s [2]). Pumped oil contains abrasive solid particles in suspention. The particles entrained by the rotor spiral are pressed on the surface of the stator which is made of an elastomer (synthetic rubber) that deforms and fixes the particles during the contact. In this way, it is achived an efficient sealing of pumping chambers and thus the effects of abrasion are reduced. After the removal of the rotor from the stator the particle of sand that was interposed falls under its own weight into the pumping chamber (cavity). In this case the particles circulated by the fluid with certain speeds are directed to the surface of the rotor and the stator and become active in terms of abrasion and erosion. The arguments previous presented underline the requirement of studying wear processes specific to progressive cavity pumps. 2. Analytical models of abrasive erosion Theoretical and experimental research of erosive wear processes have been and are currently a constant concern of many experts in the field of tribology [3-8]. The research results of erosion were materialized by the development of mathematical models specific to these tribological process. In his study, Meng [9] presented and analyzed 28 such models. Essentially the mathematical models of erosion suggest calculation equations for the intensity of erosive wear. Development of abrasive erosion models is obviously marked by technical level of theoretical and experimental investigation resources which are currently in an accelerated dynamic of improvement. It is an unanimous assessment of experts in the field that 199 marks an important milestone in the research development history of erosive wear [1-11]. The pioneering stage in development of erosion mathematical models is marked by classic models foundation, characterized as the "spine" of the research of erosive processes. Thus, the classical models of erosion, developed before 199 are those proposed by innie in 19 [12] and in 1972 [13], Bitter in 193 [14], Hutchings (in 1974, 1979 and 1981) [15], Johnson and Cook (in 1983 and 1985) [1], and Sundararajan and Shewmon in 1983 [17]. These models have been validated by research performed by specialists in the fiels and undeniably reflects the true image of the essence of erosion mechanism. Using the numerical calculation methods for describing the mechanism of erosion it opens a new stage of research in this field which is located between 199-1995 and continued up to present date [1]. Using finite element method bi- and tridimenional models of erosion caused by abrasive particles specified forms (spherical in most cases) and different sizes which interacts with the surfaces of ductile and brittle materials were developed. Thus, based on the finite element method, Wang and Yang [1] model describe the effect of impact angles, impact speed and penetration depth of the particle on the intensity of erosive wear process. 2

IOP Conf. Series: Materials Science and Engineering 174 (217) 122 doi:1.188/1757-899x/174/1/122 3. Results of the erosion wear analysis using innie models. Discutions innie models are applied for two erosion processes: the one in which the proportion of abrasive particles with microcutting effect (p a ) is 1% and the second one in which the percentage is 5%. The proposed equations for the first innie model [12] (developed in 19) are as following: E p 2 1 2 a m v cr 2 K sin 2 sin, for tg (1).9272 Hs K K E 2 2 a m r 2 cos. 9272 Hs K p v 1 c K, for K tg (2) where: E dimensionless wear rate; p a the percentage of abrasive particles with microcutting effects; ρ m target material density; v particle impact speed (m s -1 ); α the angle of incidence; c r restitution coefficient; H s static hardness; Ψ the ratio of the contact length (L) and cutting depth (δ) of impact area; K the ratio of the horizontal component ( ) and the vertical component ( v ) of the characteristic impact force. The equations are inferred by considering the following assumptions: abrasive particles are sharp; cutting and recoil effects of the particles are significant; the material is plastically deformed by the impact of the abrasive particle. The calculation formulas modified by innie (in 1972) [13] have the following structure: E p 2 1 2 a mv cr 8 2 K sin 2 sin 2K, for tg (3).9272 Hs K E pa mv 1. 9272 H 1 cr 2 cos 2 2 s, for K tg (4) The involved parameters in the calculation formulas, for both innie models, are listed in table 1, together with their associated values used in the analysis performed. Table 1. innie models parameters (for plastic deformation). parameter p a the percentage of abrasive particles with microcutting effects for a concentration of 3,3x1³ mg/l sand calculation value 5% - for the first model: p a =1.5 kg/m 3 ; 1% - for the second model: p a =.33 kg/m 3 ; ρ m density of the target area [kg/m 3 ] 1.19 α the angle of incidence [ ] 3 º v particle impact speed [m/s] 4.71 H s surface hardness [N/m 2 ] stator I: 8; stator II: 75; stator III: 7 c r restitution coefficient.5 ρ a density of the particle material [kg/m 3 ] 259-27 E e equivalent elastic modulus [N/m 2 ] stator I: 4.2; stator II: 3.; stator III: 1.7 Ψ the ratio of the contact length (L) and the cutting depth (δ) of the impact area µ friction coefficient between the particle and the material.7 15.1 1 3

IOP Conf. Series: Materials Science and Engineering 174 (217) 122 doi:1.188/1757-899x/174/1/122 Analysis of wear rate variation was achived for the following cases: E f - the variation depending on the incidence angle, for the three analyzed stators (the surface hardness H s is: for stator I: 8 N/m 2 ; stator II: 75 N/m 2 ; stator III: 7 N/m 2 ), for three values of the friction coefficient (. 1;. 5; 1). The results are shown in figure 1. 1. irst innie model Second innie model 81 3 1 3 41 3 21 3 µ=.1 - - - - - - µ=.5 2 4 8 1 1 3 41 3 21 3 µ=.1 - - - - - - µ=.5 2 4 8 1 (a) (b) 81 3 1 3 41 3 21 3.1 81 3 1 3 41 3 21 3 2 4 8 1 (c) µ=.1 - - - - - - µ=.5 µ=.1 - - - - - - µ=.5 2 4 8 1 1 3 41 3 21 3 81 3 1 3 41 3 21 3 2 4 8 1 (d) µ=.1 - - - - - - µ=.5 2 4 8 1 µ=.1 - - - - - - µ=.5 (e) igure 1. Wear rate variation depending on the angle of incidence for: (a) and (b) stator I; (c) and (d) stator II; (e) and (f) stator III. (f) 4

IOP Conf. Series: Materials Science and Engineering 174 (217) 122 doi:1.188/1757-899x/174/1/122 2. E f - the variation depending on the ratio of the contact lenght and the cutting depth of the impact area, for different values of the incidence angle ( 15 o ; 3 o ; o ), for the three analyzed stators (the surface hardness H s is: for stator I: 8 N/m 2 ; stator II: 75 N/m 2 ; stator III: 7 N/m 2 ), for the friction coefficient of µ =.5. The results are shown in figure 2. irst innie model Second innie model.2.15.1.5 5 1 15 2.1 α =15 - - - - - - 81 α =3 3 α = α =15 - - - 1 3 41 3 21 3 5 1 15 2 α =3 α = (a) (b).2.15.1.5 α =15 - - - - - - α =3 α = 5 1 15 2.1 81 3 1 3 41 3 21 3 5 1 15 2 α =15 - - - α =3 α = (c) (d).2.15.1.5 α =15 - - - - - - α =3 α = 5 1 15 2.1 81 3 1 3 41 3 21 3 5 1 15 2 α =15 - - - α =3 α = (e) igure 2. Wear rate variation depending on the ratio of the contact lenght and the cutting depth of the impact area for: (a) and (b) stator I; (c) and (d) stator II; (e) and (f) stator III. (f) 5

IOP Conf. Series: Materials Science and Engineering 174 (217) 122 doi:1.188/1757-899x/174/1/122 3. E f v - the variation depending on the impact speed, for the three analyzed stators (the surface hardness H s is: for stator I: 8 N/m 2 ; stator II: 75 N/m 2 ; stator III: 7 N/m 2 ), for the friction coefficient of µ =.5.The results are shown in figure 3. Dimensionless wear rate (E).2.15.1 51 3 Stator I - - - - - - Stator II Stator III 2 4 8 Impact speed (v) [m/s].3.2.1 Stator I - - - - - - Stator II Stator III 2 4 8 1 Impact speed (v) [m/s] (a) (b) igure 3. Wear rate variation depending on the impact speed for: (a) irst innie model; (b) Second innie model. In table 2 are shown the calculated values of the wear rate with innie models, for the angle of incidence α = 2 and the speed of v = 4.71 [m/s], and the values experimentally determined for the three analyzed stators. Stator I II III Table 2. Wear rate calculated for the working conditions. The calculation model of the rate of wear Rate of wear Experimentally Calculated value determined value [18] innie I.454 1-3 innie II 4.841 1-3 5.35 1-3 innie I.885 1-3 innie II 5.13 1-3 5.783 1-3 innie I 7.37 1-3 innie II 5.532 1-3.175 1-3 The analysis of the obtained results for the two innie models leads to the following findings: the shape of wear rate variation curves with the angle of incidence is the same for different values of the friction coefficient and the same value of the impact speed; is distinguished an incidence angle at which the wear rate has a maximum value; this is considered the critical angle of incidence in relation to the erosive effects it can produces; wear rate variation depending on the angle of incidence is different in relation to the critical angle of incidence: from zero to the critical angle the wear rate increases rapidly, then decreases slowly becoming zero at incidence angle of 9º; the maximum value rate of the wear rate and the angle of incidence at which is recorded this value it is changing depending on the friction coefficient: the increase of the friction coefficient leads to decreasing of the wear rate and to increasing of the critical angle of incidence; for angles of incidence higher than the critical value, erosive wear rate is not influenced by the friction coefficient; the wear rate decreases exponentially with the ψ coefficient (the ratio between the contact length and the depth of the cut) for angles of incidence smaller than 45 - for the first model, and is maintained constant for any value of the ψ coefficient for the second model;

IOP Conf. Series: Materials Science and Engineering 174 (217) 122 doi:1.188/1757-899x/174/1/122 erosive wear rate increases exponentially with speed impact at the same angle of incidence (for the second analyzed model); the increase is not influenced by the friction coefficient; for the erosion developed at the same speed and angle of incidence, the wear rate is not influenced by the friction coefficient between the erodent particle and the target area. 4. Conclusion in all analyzed cases, the estimated erosive wear rate with second innie model is less than the one assessed with the first innie model, which is explained by the fact that the percentage of abrasive particles with microcutting effects is 1% for the second model, versus 5% for the first model (the basic assumptions for the two models); the presented graphical results highlights the influence on the eroded surface hardness on the erosion wear: the increas hardness leads to a lower rate of erosion wear; the results acchived with the second innie model are the closest to the experimentally determined values of wear rate. It is therefore reccomanded to use the second model for the evaluation of erosive process of progression cavitation pumps. References [1] Johnson K L 1985 Contact Mechanics (Cambridge: Cambridge University Press) [2] Tudor A 22 recarea şi uzarea materialelor (Bucharest: Editura Bren) [3] Ashrafizadeh H and Ashrafizadeh 212 A numerical 3D simulation for prediction of wear caused by solid particle impact Wear 27-277 75-84 [4] Arabnejad H, Mansouri A, Shirazi S A and McLaury B S 215 Development of mechanistic erosion equation for solid particles Wear 332-333 144-15 [5] Mansouri A, Arabnejad H, Shirazi S A and McLaury B S 215 A combined CD/experimental methodology for erosion prediction Wear 332-333 19-197 [] Hadavi V, Moreno C E and Papini M 21 Numerical and experimental analysis of particle fracture during solid particle erosion, Part II: Effect of incident angle, velocity and abrasive size Wear 35-357 14-157 [7] Zhu H, Lin Y, Zeng D, Zhou Y, Xie J and Wu Y 212 Numerical analysis of flow erosion on drill pipe in gas drilling Eng. ail. Anal. 22 83-91 [8] Zhu X, Liu S, Tong H, Huang X and Li J 212 Experimental and numerical study of drill pipe erosion wear in gas drilling Eng. ail. Anal. 2 37-38 [9] Meng H C and Ludema K C 1995 Wear models and predictive equations: their form and content Wear 181-183 443-457 [1] Wang Y-, Yang Z-G 28 inite element model of erosion wear on ductile and brittle materials Wear 15 871-878 [11] Popovici A I 212 Contribuţii la studiul efectelor uzării asupra performanţelor sistemelor hidraulice de reglare automată (Bucharest: PhD Thessis, Technical University of Civil Engineering Bucharest) [12] innie I 19 Erosion of surface by solid particles Wear 3 (2) 87-13 [13] innie I 1972 Some observations on the erosion of ductile metals Wear 19 (1) 81-9 [14a] Bitter J G A 193 A study of erosion phenomena: Part I Wear (1) 5-21 [14b] Bitter J G A 193 A study of erosion phenomena: Part I and Part II Wear (1) 5-21, 19-19 [15] Hutchings I M 1981 A model for the erosion of metals by spherical particles at normal incidence Wear 7 29-281 [1] Johnson G R and Cook W H 1985 Eng. ract. Mech. 21 31-48 [17] Sundararajan G and Shewmon P G 1983 Wear 84 237-258 [18] Popescu M 21 Contribuţii la realizarea constructivă şi tehnologică a pompelor cu şurub pentru industria petrolieră PhD Thesis, Petroleum-Gas University of Ploieşti 7