SMC Corporation of America
Elite Part Number Search
Search Results "25A-MXQ8-10-M9NL"

32 6 36.5 41.5 10 44 54 8.5 13.5 16 5,10 16 8 5.4 35.5 40.5 5, 10 38 8 39 44 10.5 46 56 9.5 14.5 20 5, 10 20 10 7 36.5 41.5 5, 10 47 7 41 46 11 47.5 57.5 10 15 25 5, 10 25 12 10 37.5 42.5 5, 10 52 12 42.5 47.5 10.5 50 50 12 17 32 5, 10 32 16 13.3 38 43 5, 10 45 13 45 50 11 56.5 66.5 12 17 40 5, 10 40 16 18.3 44.5 41.5 5, 10 52 13 51.5 56.5 10.5 68.5 88.5 18 28 50 10, 20 50 20 17.6 50.5 60.5

32 6 36.5 41.5 10 44 54 8.5 13.5 16 5,10 16 8 5.4 35.5 40.5 5, 10 38 8 39 44 10.5 46 56 9.5 14.5 20 5, 10 20 10 7 36.5 41.5 5, 10 47 7 41 46 11 47.5 57.5 10 15 25 5, 10 25 12 10 37.5 42.5 5, 10 52 12 42.5 47.5 10.5 50 50 12 17 32 5, 10 32 16 13.3 38 43 5, 10 45 13 45 50 11 56.5 66.5 12 17 40 5, 10 40 16 18.3 44.5 41.5 5, 10 52 13 51.5 56.5 10.5 68.5 88.5 18 28 50 10, 20 50 20 17.6 50.5 60.5

9 10 10 11 D-C7 D-C80 10 15 50 50 + 45 (n2) D-B5/B64 8 10 13 4 8.5 9 14 4.5 9 10 14 5 10 10 14 6 9.5 11 17 6.5 10.5 11 16 6.5 10.5 11 18 7 11 9 10 9 10 10 11 11 11 9 10 10 11 RZQ 15 + 45 ( ) n2 2 D-H7 D-H7W D-H7BAL D-H7NF D-B59W 13 (n = 2, 4, 6, ) D-H7/H7NF/H7W/H7BAL 4 10 15 60 60 + 45 (n2) MI W S D-H7C 7 D-A3/A44 D-G39/K39 8 CEP1 D-C73C D-C80C D-H7C 10 15 65 9 9 9 15 + 50 ( ) n2 2 65

CUJB6-4 -6 -8 -10 -15 CUJB8-4 -6 -8 -10 -15 -20 CUJB10-4 -6 -8 -10 -15 -20 Model Mounting bolt CUJB4-4 -6 -8 -10 CUJB6-4 -6 -8 -10 -15 CUJB8-4 -6 -8 -10 -15 -20 CUJB10-4 -6 -8 -10 -15 -20 C D A M2.5 x 21l M2.5 x 23l M2.5 x 25l M2.5 x 27l M3 x 22l M3 x 24l M3 x 26l M3 x 28l M3 x 33l M3 x 22l M3 x 24l M3 x 26l M3 x 28l M3 x 33l M3 x 38l M3 x 22l M3 x 24l M3 x 26l M3 x 28l M3 x 33l M3 x 38l

-15 -20 -30 -10 -15 -10 -15 -20 -30 -10 -15 -10 -15 -20 -30 -10 -15 1 9h9 M3 x 0.5 0.88 M3 x 0.5 0.88 M3 x 0.5 0.88 6 6 6 6 6 3 3 12h9 2 2 2 1.5 4 4 M4 x 0.7 2.1 M4 x 0.7 2.1 M4 x 0.7 2.1 8 8 8 8 8 14h9 5 5 M5 x 0.8 4.3 M5 x 0.8 4.3 M5 x 0.8 4.3 10 2 10 10 10 10 16h9 1 9h9 3 3 3 M3 x 0.5 0.88 1.5 6 M3 x 0.5 0.88 M3 x 0.5 0.88 6 6 6 6 3 3 12h9 How to Locate Finger and Attachment How to Mount

Area: (800) 258-9200-www.stevenengineering.com 0.03 0.04 0.03 0.02 0.03 0.02 0.02 0.01 0.01 0.01 0 10 20 30 40 Load (N) 0 10 20 30 40 Load (N) 0 10 20 30 50 Load (N) 40 10 10 10 L = 100 mm L = 100 mm L = 100 mm Table displacement amount (mm) Table displacement amount (mm) Table displacement amount (mm) MXP10-10 MXP10-20 MXP10-10 MXP10-20 0.04 0.03 0.08 MXP10-10 MXP10-20 MXP10-10 MXP10-20

MHR2-10/MDHR2-10 MHR2-10/MDHR2-10 20 20 Pressure 0.6 MPa Pressure Gripping force (N) Gripping force (N) 15 15 0.6 MPa 0.5 MPa MHZ 0.5 MPa 10 10 0.4 MPa 0.4 MPa MHF External grip 0.3 MPa 0.3 MPa 5 5 MHL 0.2 MPa 0.2 MPa MHR 0 10 20 30 40 50 0 10 20 30 40 50 Gripping point L (mm) Gripping point L (mm) MHK Courtesy of Steven Engineering, Inc.-230 Ryan Way, South San Francisco, CA 94080-6370-Main

10 H H 0 10 20 30 40 50 0 10 20 30 40 50 Gripping point L Gripping point L mm Gripping point L mm MRHQ16 MRHQ16 Internal gripping 60 60 50 50 Pressure 0.2MPa Pressure 0.2MPa Pressure 0.2MPa Pressure 0.2MPa 40 40 Overhang H mm Overhang H mm 0.3MPa 0.3MPa 0.3MPa 30 30 0.4MPa 0.4MPa 0.4MPa 0.3MPa 0.5MPa 0.5MPa 0.5MPa 0.4MPa 0.5MPa 0.6MPa, 0.7MPa 20 20 0.6MPa 0.6MPa 0.6MPa 10 MHZ 10 0 10 20

(FKM) 1.3 x 10-8 Internal 1.3 x 10-10 (FKM) 1.3 x 10-8 DNil A B C Seal material XSA Symbol Nil N1 1.3 x 10-8 1.3 x 10-10 (FKM) 1.3 x 10-8 Seal material FKM EPDM Barrel Perfluoro Compound no. 1349-80 2101-80 1.3 x 10-10 (FKM) XVD Note 1) Values at ambient temperatures, excluding gas permeation.

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

-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 =

-12-8 P . 10-12-30 P . 10-12-18 P . 10-12-27 10-12-1 2 Achieve rationalization of production lines with position feedback Stroke reading cylinder Measurement is possible throughout the full stroke range.

-12-8 P . 10-12-30 P . 10-12-18 P . 10-12-27 10-12-1 2 Achieve rationalization of production lines with position feedback Stroke reading cylinder Measurement is possible throughout the full stroke range.

-12-8 P . 10-12-30 P . 10-12-18 P . 10-12-27 10-12-1 Achieve rationalization Stroke reading cylinder Measurement is possible throughout the full stroke range.

A part z1 m1 = 20 x 3 x 4 x 2.7 x 10-6 = 6.48 x 10-4 (kg) Mass calculation m1 = a x b x c x Relative density Z1 Inertial moment around Z1 axis Z1 = {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) A Inertial moment around Z axis A = Z1 + m1r12 x 10-6 z f2 z2 B part r2 = 23.5(mm) Mass

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)

MI-A0801-10 MI-A0801-20 MI-A1201-10 MI-A1201-20 MI-A1201-30 MI-A2001-10 MI-A2001-20 MI-A2001-30 MI-A2501-30 MI-A2501-50 MI-A3201-30 MI-A3201-50 MI-A0802-10 MI-A0802-20 MI-A1202-10 MI-A1202-20 MI-A1202-30 MI-A2002-10 MI-A2002-20 MI-A2002-30 MI-A2502-30 MI-A2502-50 MI-A3202-30 MI-A3202-50 MI-A0803-10 MI-A0803-20 MI-A1203-10 MI-A1203-20 MI-A1203-30 MI-A2003-10 MI-A2003-20 MI-A2003-30 MI-A2503

MI-A0801-10 MI-A0801-20 MI-A1201-10 MI-A1201-20 MI-A1201-30 MI-A2001-10 MI-A2001-20 MI-A2001-30 MI-A2501-30 MI-A2501-50 MI-A3201-30 MI-A3201-50 MI-A0802-10 MI-A0802-20 MI-A1202-10 MI-A1202-20 MI-A1202-30 MI-A2002-10 MI-A2002-20 MI-A2002-30 MI-A2502-30 MI-A2502-50 MI-A3202-30 MI-A3202-50 MI-A0803-10 MI-A0803-20 MI-A1203-10 MI-A1203-20 MI-A1203-30 MI-A2003-10 MI-A2003-20 MI-A2003-30 MI-A2503