SMC Corporation of America
Elite Part Number Search
Search Results "CXSL25-10-Y59AL"

Model CYP15 CYP32 Series Throttle valve 10-AS2200-01-X214 Elbow type 10-AS1200-M5-X216 Metal body piping type 10-AS2000-01-X209 In-line type 10-AS1000-M5-X214 10-AS2201F-01-04-X214 10-AS1201F-M5-04-X214 Elbow type (throttle valve) 10-AS2201F-01-06-X214 10-AS1201F-M5-06-X214 10-AS2201F-01-06-X214 Operation 10-AS2301F-01-04-X214 10-AS1301F-M5-04-X214 Resin body with One-touch fitting Caution

10 15 15 20 20 2 pcs. 5 10 15 10 20 15 Auto Switch Mounting Bracket Part Nos.

2.7 X 10-6 Calculation of weight m2 = d X e X f X Specific gravity = 0.002(kg) Iz2 = {0.002 X (52 + 102)/12} X 10-6 Moment of inertia around Z2 axis = 0.02 X 10-6 (kgm 2) IB = 0.02 X 10-6 + 0.002 X 472 X 10-6 Iz2 = {m2(d 2 + e2)/12} x 10-6 Moment of inertia around Z axis IB = IZ2 + m2r22 x 10-6 = 4.4 X 10-6 (kgm2) I = 9.0 X 10-6 + 4.4 X 10-6 Total moment of inertia I = IA + IB = 13.4 X

G46-10-01 2 pcs. G46-10-01 2 pcs. G27-10-R1-X209 2 pcs. G27-10-R1-X209 2 pcs.

REAL40 REAL25 REAL32 Model 10 (2.48 1.3 x 10-3 x ST) 30 10 (1.98 1.3 x 10-3 x ST) 10 (2.26 1.3 x 10-3 x ST) = 50 20 2.

Load weight (kg) Load weight (kg) Load weight (kg) 10 10 10 MY1H40 MY1H40 MY1H40 MY1H40 MY1H40 MY1H40 MY1H40 2. Reference formula [Dynamic moment at impact] Use the following formulae to calculate dynamic moment when taking stopper impact into consideration.

10.5 20 9.5 6 10 35.5 72 19 17.5 CY1R10 9 38 3.5 4 M3 x 0.5 4.5 M5 x 0.8 68 14 14 20 13 8 15 39.5 76 26 17.5 CY1R50 25 110 8.6 10 M8 x 1.25 15 Rc 1/4 159 48 42 60 41 10 50 113 176 82 30 CY1R63 24 118 8.6 10 M8 x 1.25 16 Rc 1/4 171 60 48 70 47 10 60 121 188 94 32 8-15-42 42 Series CY1R Magnetically Coupled Rodless Cylinder Direct Mount Type Centralized Piping Type: 10, 50, 63 CY1RG Bore size

-6 = 9.0 x 10-6 (kgm2) Moment of inertia around Z axis IA = IZ1 + m1r12 X 10-6 z r2 Z2 B part r2 = 47(mm) Calculation of weight m2 = d x e x f x Specific gravity m2 = 5 x 10 x 12 x 2.7 x 10-6 = 0.002 (kg) Moment of inertia around Z2 axis IZ2 = {m2 (d2 + e2)/12} x 10-6 IZ2 = {0.002 x (52 + 102)/12} x 10-6 = 0.02 x 10-6 (kgm2) IB = 0.02 x 10-6 + 0.002 x 472 x 10-6 = 4.4 x 10-6 (kgm2) I =

-6 = 9.0 x 10-6 (kgm2) Moment of inertia around Z axis IA = IZ1 + m1r12 X 10-6 z r2 Z2 B part r2 = 47(mm) Calculation of weight m2 = d x e x f x Specific gravity m2 = 5 x 10 x 12 x 2.7 x 10-6 = 0.002 (kg) Moment of inertia around Z2 axis IZ2 = {m2 (d2 + e2)/12} x 10-6 IZ2 = {0.002 x (52 + 102)/12} x 10-6 = 0.02 x 10-6 (kgm2) IB = 0.02 x 10-6 + 0.002 x 472 x 10-6 = 4.4 x 10-6 (kgm2) I =

A part z1 m1 = 20 x 3 x 4 x 2.7 x 10-6 = 6.48 x 10-4 (kg) Weight calculation m1 = a x b x c x Relative density IZ1 Inertial moment around Z1 axis IZ1 = {m1 (a2 + b2) / 12} x 10-6 = {6.48 x 10-4 x (202 + 32)/12} x 10-6 = 2.21 x 10-8 (kg.m2) = 2.21 x 10-8 + 6.48 x 10-4 x 16.42 x 10-6 = 0.20 x 10-6 (kg.m2) IA Inertial moment around Z axis IA =IZ1 + m1r12 x 10-6 z f2 z2 B part r2 = 23.5(mm)

A part z1 m1 = 20 x 3 x 4 x 2.7 x 10-6 = 6.48 x 10-4 (kg) Weight calculation m1 = a x b x c x Relative density IZ1 Inertial moment around Z1 axis IZ1 = {m1 (a2 + b2) / 12} x 10-6 = {6.48 x 10-4 x (202 + 32)/12} x 10-6 = 2.21 x 10-8 (kg.m2) = 2.21 x 10-8 + 6.48 x 10-4 x 16.42 x 10-6 = 0.20 x 10-6 (kg.m2) IA Inertial moment around Z axis IA =IZ1 + m1r12 x 10-6 z f2 z2 B part r2 = 23.5(mm)

For details, refer to 3 point preset counter/CEU1 on page 10-12-30, and Multi counter/CEU5 on page 10-12-27 respectively.

For details, refer to 3 point preset counter/CEU1 on page 10-12-30, and Multi counter/CEU5 on page 10-12-27 respectively.

49 1/8 17 8 32 M12 x 1.75 11 depth 6.5 61 51 10 18 14 15 7 47 6.6 63 1/4 19.5 10 40 M16 x 2 14 depth 8.6 65 55 10 22.4 19 20 7 52 9 71 1/4 20.5 10 50 M20 x 2.5 17.5 depth 10.8 71 60 11 28 24 24 8 58 11 81 1/4 22 10 63 M27 x 3 20 depth 13 80 67 13 35.5 30 33 9 69 13 97 1/4 25.5 10 80 M30 x 3.5 23 depth 15.2 95 78 17 45 41 36 14 86 15 117 3/8 30 15 100 M39 x 4 26 depth 17.5 122 96 26 56 50

For details, refer to 3 point preset counter/CEU1 on page 10-12-30, and Multi counter/CEU5 on page 10-12-27 respectively.