Purdue University Purdue e-Pubs International Compressor Engineering Conference School of Mechanical Engineering 1996 A Fundamental Optimum Design for High Mechanical and Volumetric Efficiency of Compact Scroll Compressors N. Ishii Osaka Electro-Communication University M. Sakai Matsushita Electric Industrial Co. K. Sano Matsushita Electric Industrial Co. S. Yamamoto Matsushita Electric Industrial Co. T. Otokura Osaka Electro-Communication University Follow this and additional works at: http://docs.lib.purdue.edu/icec Ishii, N.; Sakai, M.; Sano, K.; Yamamoto, S.; and Otokura, T., "A Fundamental Optimum Design for High Mechanical and Volumetric Efficiency of Compact Scroll Compressors" (1996). International Compressor Engineering Conference. Paper 1176. http://docs.lib.purdue.edu/icec/1176 This document has been made available through Purdue e-Pubs, a service of the Purdue University Libraries. Please contact epubs@purdue.edu for additional information. Complete proceedings may be acquired in print and on CD-ROM directly from the Ray W. Herrick Laboratories at https://engineering.purdue.edu/ Herrick/Events/orderlit.html A FUNDAl\1ENTAL OPfiMU M DESIGN FOR HIGH MECHANICAL AND VOLUMETRIC EFFICIENCY OF COMPACT SCROLL COMPRESSORS by Noriaki Ishii I, Manabu Sakai2, K.iyoshi Sano3, Shuichi Yamamoto3 . and Takayuki Otokura4 1 Professor, Faculty of Engineering, Osaka Electro-Communication University, Neyagawa, Osaka 572, Japan Tel: +81-720-20-4561; Fax: +81-720-20-4577; E-mail: ishii@is c.osakac .ac.jp 2 Engineer, Compressor Division, 3 Senior Staff Engineer, Air Conditioning Research, Matsushita Electric Industrial Co., Ltd. (Panasonic), Noji-cho, Kusatsu-shi, Shiga 525, Japan Tel: +81-775-67-9801, Fax: +81-775-61-3201 4 Graduate Student, Faculty of Engineering, Osaka Electro-Communication University. ABSTRACT This paper presents a fundamental optimum design which yields a high compressor performance in mechanical and volumetric efficiency. The frictional power losses were calculated by an analytical method revealing the dynamic behavior of scroll compressors, and the refrigerant leakages were calculated by an incompressive and viscous theory assuming an entire turbulent leakage flow. Computer calculations were made for a number of combinations of the involute base circle radius and the scroll depth, where the scroll thickness and the cylinder diameter were fixed at a constant value. The calculated results for the mechanical and volumetric efficiency indicated that there is a definite optimum combination of major parameters. Additionally, the effects of the suction volumes and the clearance values upon the resultant efficiency were carefully examined to clarify a better fundamental optimum design in compact scroll compressors. 1. INTRODUCTION The suction volume of scroll compressors is determined by the major parameters, such as the involute base circle diameter, the scroll depth, the scroll thickness and the number of scroll turns, and, subsequently, there are many combinations of major parameters that result in a scroll compressor with the same suction volume. Therefore, one of basically significant designs in scroll compressor is to determine a combination of these major parameters for high compressor performance. This paper presents an optimum combination of the major parameters, which yields a high performance in mechanical and volumetric efficiency of scroll compressors. Depending upon the selected combination of major parameters, the frictional power loss at each pair of compressor elements changes, resulting in different mechanical efficiencies [1-3], and simultaneously, the refrigerant leakage from each clearance also changes, resulting in different volumetric efficiencies. Thus, careful selection of the optimum combination of major parameters is necessary to ensure a high mechanical and volumetric efficiency of the scroll compressor. In the present study, the mechanical and volumetric efficiencies were computer simulated for a number of combinations of the involute base circle radius and the scroll depth, where the scroll thickness and the cylinder diameter were fixed at a constant value. For mechanical efficiency, the frictional power losses were calculated by an anlytical method for the dynamic behavior of scroll compressors [4-7]. For volumetric efficiency, the refrigerant leakages through the axial and radial clearances were calculated by an incompressive and viscous theory assuming an entire turbulent 639 small suction leakage flow [8]. Additionally computer simulations were made for a number of design for optimum ntal fundame a of volumes and clearance values, in order to examine a possibility sors. high mechanical and volumetric efficiency in compact scroll compres 2. CALCU LATION FOR VOLUM ETRIC EFFICIE NCY -shaped A scroll compressor configuration is shown in Figure 1, in which one crescent by affected greatly is P, r, chambe compression chambe r is meshed. The pressure in this compression pressure lower the to outflow the leakage inflow from the higher pressure chamber and the leakage axial clearance chamber. The leakage inflow is induced by the radial flow velocity Uai through the by Ti. The denoted e denoted by Ai, and by the tangential flow velocity uri through the radial clearanc by Ao, denoted e leakage outflow is induced by the radial flow velocity Uao through the axial clearanc inflow The • T by 0 and by the tangential flow velocity uro through the radial clearance denoteq outflow the and r, velocities are caused by the pressure difference from the higher compression chambe velocities are by the pressure difference from the lower compression chamber. by the For given pressure differences, these inflow and outflow velocities can be calculated for valid be to incompressive and viscous flow theory which was ensured in the former study [3] the through refrigerant leakage flows in scroll compressors. Therewith the outflow and inflow rates ed by calculat be can Qrj, and Qe, clearanc radial the through 0 those axial clearance, Qao and Qru, and the followin g expressions: Oao :::: P <>aSoUao, Qm :::: poaSillai•} = (1) <1-o p OrBUr0 , <1-i :::: pbrBuri, B is the height, where pis the specific mass, 6a is the axial clearance height, 6r is the radial clearance 1, Figure in Ai scroll height, and S 0 and Si are the length of the axial clearances denoted by Ao and the in mass respectively. Using the leakage mass flow rates calculated by (1), the refrigerant on: crescent-shaped compression chamber, G, can be calculated by the following integral expressi G:::: Gs + !. 1 { <2ai + <1-i- (Qa0 +Q.o)} dt, where the time after the instant when the suction chamber was just closed at the periphery of the scrolls is represented by t, and the refrigerant mass in the suction chambe r at t :::: 0 is by G 8 • Since the inflow mass from the higher compression chambe r is normally larger than the outflow mass to the lower pressure chambe r, the refrigerant mass in the compression chamber, G, increase s as the time elapses, thus inducin g a pressure non-leakage in than higher compression. Assumi ng the adiabatic compression with the specific heat ratio K , pressure P in the compres sion chamber with volume V can be calculated by ¢>, ¢>. (2) ¢> ;-2 rr ' ' .G.)lC P -- ps (~(3) Gs V ' clearances. where Ps and Vs are the initial values Figure 1. Leakage flow velocities at axial and radial 640 of pressure and volume at t=O, respectively. If the pressure changes are initially given by the adiabatic change for non-leakage compression, the refrigerant mass and pressure in the compression chamber can be calculated for one compression process from suction to discharge, by expressions (2) and (3). Using the calculated pressures, furthermore, the refrigerant mass and pressure can be newly calculated, and such repeated calculations can be made to obtain the correct pressure changes and refrigerant gas leakage flow rates. The resultant refrigerant mass of leakage from the outer two compression chambers to the suction chamber, llG, can be calculated by AG = 2 { 0< ( Oao + Q.0 ) dt, lo (4) 0 where tr is one period for orbiting motion. Finally the volumetric efficiency l'Jm can be calculated by the following expression: _ Gs -AG . Gs l']v = (5) 3. CALCULATED RESULTS YQlumetrk.EfficieiJC~ In numerical calculation, the specific heat ratio was assumed to be 1.32, the suction pressure to be 0.62 MPa, the suction temperature to be 18 °C, the specific mass of refrigerant in the suction chamber to be 24.71 kg/m3 and the discharge pressure to be 2.17 MPa. The cylinder diameter and the scroll thickness were fixed at the values of75.7 mm and 4 nun, respectively, and the combinations of the involute base circle radius rb and the scroll height B were adjusted at various values. Calculated results for refrigerant leakage at a suction volume of 10.3 cm3 and an involute base circle radius of 2.0 mm are shown in Figure 2, where both the axial and radial clearances were fixed at 10 ~tm. The abscissa is the orbiting angle e, and its zero value corresponds to the angle when the suction chamber was closed. One compression cycle is about 79Qo. The leakage flow velocities are less than about 74 m/s at the axial clearance, and less than about 117 m/s at the radial clearances, as shown in diagram (b). The leakage flow velocities at the axial clearances are less than the radial clearance, but the leakage mass flow rates from the axial clearance is larger than the radial clearance, as shown in diagram (c). By integrating the calculated mass flow rates for one cycle of orbiting motion, as given by (4), the resultant refrigerant mass of leakage from the outer two compression chambers to the suction chamber, L1G, can be calculated, thus resulting in the volumetric efficiency given by (5). Similar calculations were made for various 72D e (deg] values of the involute base circle radius from 1.3 nun to 3.6 nun, and the calculated results were obtained, as Figure 2. Refrigerant leakage in scroll shown in Figure 3, where the suction volume Vs was compressor with involute base circle fixed at 4 different values from 10.3 cm3 to 2.5 cm3. radius of 2.0 mm and axial and radial Figure 3a shows the scroll height over the suction clearances of 10 ~tm: (a) pressure in volume, B/Vs, which increases with decreasing the compression chamber; (b) leakage ininvolute base circle radius fb. The refrigerant mass of flow and outflow velocities; (c) leakage mass inflow and outflow rates. 641 leakage for Vs=10.3 cm3 is shown in Figure 3c, where the leakage mass AGa from the axial clearance is larger than AG r from the radial clearance, corresponding well to the calculated data of the leakage mass flow rates shown in Figure 2c. The resultant refrigerant mass of leakage, AG, shows a minimum value around at rb=l.7 mm, thus resulting in the volumetric efficiency which shows its maximum value of 76.2 % for Vs=10.3 cm3. As the suction volume becomes smaller , the volumetric efficiency decreases wholly. When the suction volume takes on a small value of 2.5 cm3, the volumetric efficiency is less than about 20 %. o.a.---- -------- --. """ "'~0.6 >"' 0.4 I ~0.2 o:l ..,_-- VS=1 0.3cm3 7.5cm3 5.0cm 3 2.5cm3 0 L...:::=§§§~~_j (a) 90r-----------------~ 80 70 ,......., 60r £so '---' ~17"2 ~cm3 ~cm3 ~Ocrn3 > 40 I Mechanical Efficiency ~ I An analytical method for dynamic behavior of I 30 scroll compressors has been established with regard to the 20 fundamental dynamics of machinery, in the previous studies [4-7], where it was assumed that the frictional 10 I forces at any pair that is not well lubricated by a thick oil 0'-----'---.c....... ..J--'-----'---'---- --' (b) film are subject to Coulomb's law of friction. As for the frictional coefficient at each pair, it was quite difficult to evaluate each precise value for practically used scroll Thereupon, it was a quite rough compressors. assumption but the previous study made use of the frictional coefficient of 0.013 which were determined I '\l 4 I numerically in a study [9] for a compact rolling-piston I L1Gr r c!5 rotatory crankshaft the Therewith, rotary compressor. '\l 2 behavior, the constraint force and the frictional power loss at each pair could be calculated to reveal the (Vs==10.3cm3) (c) _L ~ 01 mechanical efficiency. 4 3 2 The mechanical efficiency calculated for 4 rb [mm] different values of suction volume are shown in Figure 4. for axial Some of the mechanical efficiencies were cited from the Figure 3 .. Volumetric efficiency and radial clearances of 10 !Am: (a) previous study [3]. In computer calculations, the motor scroll height; (b) volumetric efficiency; power was adjusted to keep the mean crankshaft speed at refrigerant mass of leakage from (c) .56.4 Hz, and an optimum intermediate pressure was led two compression chambers. outer to to the back surface of the orbiting scroll end plate [4bearing 95.------------~-----. minimize the frictional power loss at the thrust 7]. With decreasing the involute base circle radius, 90 the frictional power losses at the crankshaft and crank pin height. scroll in increase the of increases because Furthermore, with increasing involute base circle radius, a 85 the frictional power loss at the thrust bearing increases 1;:.::[2]. area chamber compression in because of the increase That is why the mechanical efficiency shows its highest 80 value at a moderate involute base circle radius. ~-' f:: \v----- Jr~ \LS----_l_ Mechanical and Volumetric Efficiency 751r-~--,2~_.--,3~~--~4 The product of the volumetric efficiency shown in lb[mm] Figure 3b and the mechanical efficiency shown in Figure 4, termed a mechanical and volumetric efficiency TJ, are Figure 4. Mechanical efficiency for fricshown in Figure Sa. The efficiency curves for the suction tional coefficient of 0.013. 642 volumes of 10.3 cm3 , 7.5 cm3 and 5.0 cm3 increase rapidly with increasing the involute base circle radius rb, showing each peak value at the involute base circle radius of 2.0 mm to 2.1 mm. These curves gradually decrease with increasing further the involute base circle radius. The decrease magnitude from each peak value is not so large .. As shown in Figure Sb, however, the crankshaft speed fluctuation ratio a increases rapidly, with increasing the involute base circle radius, and takes on a value more than 1% for Ib> about 2.5 rom. Conclusively, a fundamental optimum value for the involute base circle radius has to be determined around at 2.0 mm to 2.1 mm. The efficiency curve for the suction volume of 2.5 cm3 does not exhibit a peak value, since the volumetric efficiency took on too small values, as shown in Figure 3b. 80r----------..., 4. POSSIBILITY OF FUNDAMENTAL OPTIMUM DESIGN FOR COMPACT SCROLL COMPRESSORS ........., 70 ;:::] 66.6 60 59.1 Vs,10.3cw 3 ~Scw 3 £50 4ll "--" In order to examine the possibility of fundamental ~.Ocw 3 ~40 optimum design for compact scroll compressors, similar 30 calculations were made for various reduced values of the axial clearance. The leakage mass from the axial 20 15.7% clearance was far larger than from the radial clearance, as 10 shown in Figure 3c. That is why the axial clearance only ~.____.._ _.__ _.___,______.__..J(a) was reduced and the radial clearance was kept at the same value of 10 !lm- The calculated results are shown in .........,3 Figure 6. As the axial clearance decreases, the efficiency ~2 curves for a larger suction volume of 10.3 cm3 increase (j 1 wholly, exhibiting each peak value at the involute base circle radius of about 2.2 to 2.4 mm, as shown in 1~~~~~~3~--'--~4.~) diagram (a). The efficiency curves for a smaller suction Ib(mm] volume of 2.5 cm3 also exhibit each peak value at the involute base circle radius of about 1.9 to 2.1 mm, which Figure 5. Mechanical and volumetric efficiency for axial and radial clearances of becomes higher with decreasing the axial clearance, as 10 !liD: (a) mechanical and volumetric shown in diagram (b). efficiency; (b) crankshaft speed fluctuation ratio. 5. CONCLUSIONS The present study performed computer simulations for the mechanical and volumetric efficiency, thus resulting in the following conclusions. The volumetric efficiency is more significantly affected by the refrigerant leakage from the axial clearance than from the radial clearance. A fundamental optimum design for higher mechanical and volumetric efficiency would be possible for compact scroll compressors, by reducing the axial clearance and by selecting the optimum combination of the major parameters. An extremely compact and high efficiency scroll compressor, for example, with a suction volume of2.5 cm3, would be ::r---~-~---0-2-..., 70 ........ ~60 90r-----------. 80 ~ 1!- o,dO!Lm ~ 70 ~60 ~ 50 50 40 40 301_......__'*2____..____*3___.---.J.4 (a) l"b[mm] ~ ~ ~ 3 ~--~*2~~3~~~4 (b) l'b[mm] Figure 6. Improvement of mechanical and volumetric efficiency:(a) for suction volume of 10.3 cru3; (b) for suction volume of 2.5 cm3. 643 highly possible, by utilizing the present optimum design simulations. ACKNOVVLEDGMlliNTS The authors would like to express their gratitude to Mr. Jirou Yuuda, Head of the Air Conditioning Research Laboratory, and Mr. Tomio Kawabe, Head of the Compressor Division, for their financial support in carrying out this work and their permission to publish these results. The authors also would like to express their sincere thanks to Mr. Hiraku Matsui and Mr. Noriyuki Morita for their energetic works for leakage tests and computer simulations. REFERENCES ( 1) Ishii, N. et al., Optimum Combination of Dimensions for High Mechanical Efficiency of a RollingPiston Rotary Compressor, Proc. International Compressor Engineering Conference at Purdue, July, 1990, pp.418-424. (2) Ishii, N. et al., Optimum Combination of Parameters for High Mechanical Efficiency of a Scroll Compressor, Proc. International Compressor Engineering Conference at Purdue, July, 1992, pp.l18al-118a8. (3) Ishii, N. et al., A Study on High Mechanical Efficiency of a Scroll Compressor with Fixed Cylinder Diameter, Proc. International Compressor Engineering Conference at Purdue, July, 1994, pp.677-682. (4) Ishii, N. et al., Mechanical Efficiency of Various Large Capacity Scroll Compressors, Proc.17th International Congress of Refrigeration, Wien, Aug., 1987, pp.468-474; Transactions of the Japan Society of Mechanical Engineers (in Japanese), Series C, Vol.53, No.495, 1987, pp.2295-2302. (5) Ishii, N. et al., Dynamic Behavior of a Scroll Compressor (Dynamic Analysis), JS.ME International Journal, Series 3, Vol.31, No.1, March, 1988, pp.58-67; Proc. International Compressor Engineering Conference at Purdue, Vol.3, Aug., 1986, pp.901-916. (6) Ishii, N. et al., On the Superior Dynamic Behavior of a Variable Rotating Speed Scroll Compressor, Proc. International Compressor Engineering Conference at Purdue, Vol.l, July, 1988, pp.75-82; Transactions of the Japan Society of Mechanical Engineers (in Japanese), Series C, Vol. 55, No.517, 1989, pp.2436-2445. (7) Ishii, N. et al., Mechanical Efficiency of a Variable Speed Scroll Compressor, Proc. International Compressor Engineering Conference at Purdue, Vol.l, July, 1990, pp.192-199. (8) Ishii, N. et al., Refrigerant Leakage Flow Evaluation for Scroll Compressors, Proc. International Compressor Engineering Conference at Purdue, July, 1996. (9) Ishii, N. et al., The High Mechanical Efficiency of Rolling-Piston Rotary Compressors, Proc. 2nd World Congress on Heating, Ventilating, Refrigerating and Air Conditioning (CLIMA2000) at Sarajevo, Yugoslavia, 1989, p.91. 644