(Page 11) fR: Lateral load applied to rod end Ft: Maximum force of cylinder Lateral load applied to rod Bushing (bearing) Cylinder stroke Fig. 1 Allowable lateral load applied to rod end Calculation for excessive lateral load: Minimum operating pressure value after the device is mounted (MPa) = Cylinder's minimum operating pressure(MPa) + {Load weight(kg) Guide friction coefficient / Cylinder's
AF AR 4 - 1) 5 2) 3) 5 4) 1 ISO VG-32 2-2. 1) 2) 3) 4) 5) 6 7) 5 - 8 9) , 10) 11) 3 1) P10 [2-6.] 2) 3) 4) 5) 6) 7) (40) 6 - 2-3. 1) 1 P10 [2-6.] fR Ft N () mm 1. (MPa)=(MPa)+{(kg) 2)} X /(mm ,, 2) 3) 4) 7 - 5) 6) 7) 8) 9) 24. 1) 2) 3) 8 - 1) 2) 1.52 2 2. 2-5. ,AS 9 - 2-6. P7.1. 1.
FR/L COMBO MODULAR. 1.76000 lb. P29.
FR/L COMBO MODULAR. 1.76 lb. P29.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 1/2 MODULAR (NPT). 3.55923 lb. FC.
FR/L COMBO MODULAR. 1.76000 lb. P29.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 1/2 MODULAR (NPT). 4.7477 lb. FC.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 3/8 MODULAR (NPT). 3.55189 lb. EC.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 3/8 MODULAR (NPT). 3.55189 lb. EC.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 3/8 MODULAR (NPT). 3.55189 lb. EC.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 3/8 MODULAR (NPT). 3.55189 lb. EC.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 3/8 MODULAR (NPT). 3.55189 lb. EC.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 1/2 MODULAR (NPT). 2.88805 lb. FC.
FR/L COMBO MODULAR. 1.104 lb.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 1/2 MODULAR (NPT). 2.88805 lb. FC.
FR/L COMBO MODULAR. 1.65 lb. P29.
FR/L COMBO MODULAR. 2.27 lb. P29.
FR/L COMBO MODULAR. AIRLINE EQUIPMENT. AC MASS PRO 1/2 MODULAR (NPT). 3.55923 lb. FC.
FR/L COMBO MODULAR. 1.194 lb. 11.
FR/L COMBO MODULAR. 2.49 lb. P29.