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            Steel Lamina Coupling

            RLAF Diaphragm Coupling

            Home>Coupling Products>Steel Lamina Coupling > RLAF Diaphragm Coupling

            RLAF Diaphragm Coupling

            Large and Small Axis Installation

            The size difference design of the bilateral shaft sleeve is suitable for situations where the diameter difference between the two ends of the shaft is significant.

            RLAF Diaphragm Coupling
            ModelD/DAD1/D2D3d1(max)d2(max)L1/L2SMaximum Allowable SpeedNominal TorqueMaximum Instantaneous Torque
            (mm)(mm)(mm)(mm)(mm)(mm)(mm)n max(r/min)T(N.m)Tmax(N.m)
            RLAF125-6125/15570/10568507055/7511140006501300
            RLAF135-6135/16892/11982658570/90111180011802478
            RLAF156-6160/190105/140967510080/105151000021002780
            RLAF178-6180/218119/1611178511590/12015850035805600
            RLAF210-6210/258140/182122100130105/13520780050007800
            RLAF225-6230/276154/217144110155115/165226500850013200
            RLAF255-6260/295168/238158120170125/180245800900014040
            RLAF280-6280/320196/259171140185150/1953052001350021060
            RLAF305-6310/356210/273193150195160/2053243502025031500
            RLAF340-6340/400238/308230170220180/2303438803050047500
            RLAF365-6370/425258/350228190250200/2603435003250078500
            RLAF420-6420/495278/406269200290210/2903631004200095800
            ModelMass Point
            G/GA
            Angular DeviationAxial DeviationIntermediate Joint Sleeve
            H
            Intermediate Sleeve Weight
            Intermediate Sleeve Rotational Inertia
            Torsional stiffness of diaphragm groupWeightTorsional StiffnessRotational Inertia
            (mm)(±△o)(±△mm)min(mm)kgJh(Kg.m2)Ct+10E6(N.m/rad)(Kg)Ct+10E6(N.m/rad)J(Kg.m2)
            RLAF125-652.1/69.1211651.570.006440.347.80.170.01708
            RLAF135-662.2/83.9711651.820.00780.2911.20.1450.0225
            RLAF156-664.5/87.07511.4852.70.01630.8416.10.420.05
            RLAF178-677.6/100.8811.4853.30.02241.123.20.550.0768
            RLAF210-680.6/10411.41056.160.06821.9733.580.9850.1974
            RLAF225-696.9/121.1250.751.61057.170.08733.4547.021.7250.2806
            RLAF255-6103.2/1280.751.615013.640.2235.1367.922.5650.646
            RLAF280-6118.1/147.6250.75216014.770.2427.9489.723.970.814
            RLAF305-6122/152.50.75218524.430.5359.35118.544.6751.58
            RLAF340-6141.3/162.4950.75219030.230.80712.58164.546.292.464
            RLAF365-6145/166.6750.75221037.41.1715.95195.757.9753.55
            RLAF420-6167.8/192.970.75222049.52.03623.95272.87511.9756.222
            ModelDA/DD1/D2D3d1(max)d2(max)L1/L2SMaximum Allowable SpeedNominal TorqueMaximum Instantaneous Torque
            (mm)(mm)(mm)(mm)(mm)(mm)(mm)n max(r/min)T(N.m)Tmax(N.m)
            RLAF255-8260/295168/238158120170125/180245800900014040
            RLAF280-8280/320196/259196140185150/1953052001350021060
            RLAF310-8310/356210/273210150195160/2053243502025031500
            RLAF340-8340/400238/308238170220180/2303438803050047500
            RLAF370-8370/425258/350258190250200/2603435003250078500
            RLAF420-8420/495278/406273200290210/2903631004200095800
            RLAF445-8450/518330/450340220320282/3303818506000093600
            RLAF500-8500/575360/546434240390330/33044180072000112500
            ModelMass Point
            G/GA
            Angular DeviationAxial DeviationIntermediate Joint Sleeve
            H
            Intermediate Sleeve Weight
            Intermediate Sleeve Rotational Inertia
            Torsional stiffness of diaphragm groupWeightTorsional StiffnessRotational Inertia
            (mm)(±△o)(±△mm)min(mm)kgJh(Kg.m2)Ct10E6(N.m/rad)(Kg)Ct+10E6(N.m/rad)J(Kg.m2)
            RLAF255-8103.2/1280.53.615013.644 0.22310.2567.925.1250.629
            RLAF280-8118.1/147.6250.53.616014.769 0.24216.1589.728.0750.902
            RLAF310-8122/152.50.53.818524.437 0.53518.69118.549.3451.589
            RLAF340-8141.3/162.4950.53.819030.234 0.80725.15164.5412.5752.613
            RLAF370-8145/166.6750.5421037.400 1.1731.91195.7515.9553.668
            RLAF420-8167.8/192.970.54.622049.497 2.03647.89272.87523.9456.458
            RLAF445-8160.6523/184.750.54.622055.760 2.04358.46364.500 29.2310.191
            RLAF500-8187.2418/215.3280.55.523073.668 3.50971.67499.030 35.83517.063
            ModelDA/DD1/D2D3d1(max)d2(max)L1/L2SMaximum Allowable SpeedNominal TorqueMaximum Instantaneous Torque
            (mm)(mm)(mm)(mm)(mm)(mm)(mm)n max(r/min)T(N.m)Tmax(N.m)
            RLAF370-10370/425258/350258190250200/2603435003250078500
            RLF420-10420/495278/406273200290210/2903631004200095800
            RLAF445-10450/518330/420321220300282/33038185075000117000
            RLAF500-10500/575360/448346240320330/330441800105000163800
            RLAF630-10630/710405/462398280350330/450441420210000327600
            RLAF700-10700/785460/546448320390330/520501280288000449280
            RLAF60-10760/850493/645478340460450/580601180365000569400
            ModelMass Point
            G/GA
            Angular DeviationAxial DeviationIntermediate Joint Sleeve
            H
            Intermediate Sleeve Weight
            Intermediate Sleeve Rotational Inertia
            Torsional stiffness of diaphragm groupWeightTorsional StiffnessRotational Inertia
            (mm)(±△o)(±△mm)min(mm)kgJh(Kg.m2)Ct10E6(N.m/rad)(Kg)Ct+10E6(N.m/rad)J(Kg.m2)
            RLAF370-10145/166.6750.32421037.400 1.1731.91195.7515.9553.668
            RLF420-10167.8/192.970.324.622049.497 2.03647.89272.87523.9456.458
            RLAF445-10160.6523/184.750.324.522055.760 2.04371.35364.500 35.67510.191
            RLAF500-10187.2418/215.3280.32523073.668 3.50991.95499.030 45.97517.063
            RLAF630-10197.3536/226.950.326245130.080 12.453193.1694.250 96.5539.181
            RLAF700-10198.6369/228.450.327250217.214 20.778260.46939.340 130.2362.154
            RLAF60-10261.44407/300.660.328265197.708 26.842331.341260.120 165.6796.662
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