SMC Corporation of America
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Search Results "LQ1L23-MN-1"

Type SS3YJ7-40 1/8 1/8 1/8 1/8 C6 C8 Type SS3YJ7-41 Base mounted for internal pilot Type SS3YJ7-42-01 SYJ74 1/4 1/4 Type SS3YJ7-42-C6 Type SS3YJ7-42-C8 1/4 Body ported for external pilot SYJ72R 1/4 1/8 2.2 0.34 0.55 2.4 0.32 0.62 Type SS3YJ7-21R Type SS3YJ7-41R 2.2 2.0 1.6 2.1 0.35 0.27 0.32 0.24 0.59 0.47 0.39 0.51 2.4 2.2 2.2 2.3 0.36 0.32 0.27 0.31 0.66 0.56 0.54 0.59 1/8 1/8 C6 1/4 1

M5 6 4 8 (1) M5 X 0.8 SYJ300 Top (2) SY Body ported Base mounted Rc(PT)1/8 SYJ SYJ500 Top Rc(PT)1/8 VK (1) Rc(PT)1/8 SYJ700 Top VZ Rc(PT)1/4 VT (1) M5 X 0.8 SYJ300 Side VT Rc(PT)1/8 Bottom VP SYJ500 Rc(PT)1/8 Side VG Rc(PT)1/8 (1) SYJ700 Bottom Rc(PT)1/4 VP Rc(PT)1/4 Side Note 1) Only internal pilot style Note 2) Only external pilot style VQ VQZ VZ VS Series SYJ300 Series SYJ500 Series SYJ700

1.6 2.1 0.34 0.39 0.35 0.35 0.27 0.32 0.24 0.55 0.59 0.59 0.59 0.47 0.39 0.51 2.3 2.4 2.3 2.4 2.2 2.2 2.3 0.27 0.32 0.27 0.36 0.32 0.27 0.31 Body ported for internal pilot 0.59 0.62 0.54 0.66 0.56 0.54 0.59 1/8 1/4 1/8 1/4 10-SYJ72M 1/8 1/8 1/8 1/8 C6 C8 Type 10-SS3YJ7-40 Type 10-SS3YJ7-41 Base mounted for internal pilot 10-SYJ74M 1/4 1/4 Type 10-SS3YJ7-42-01 Type 10-SS3YJ7-42-C6 1/4 Type

Composite Center of Gravity Calculation m1 = mn = 0.88 + 4.35 + 0.795 + 0.5 = 6.525 kg 1 m1 X = x (mn x xn) 1 6.525 = (0.88 x 65 + 4.35 x 150 + 0.795 x 150 + 0.5 x 150) = 138.5 mm 1 m1 Y = x (mn x yn) 1 6.525 = (0.88 x 0 + 4.35 x 0 + 0.795 x 111 + 0.5 x 210) = 29.6 mm 1 m1 Z = x (mn x zn) 1 6.525 = (0.88 x 5 + 4.35 x 42.5 + 0.795 x 42.5 + 0.5 x 42.5) = 37.4 mm 4.

Composite Center of Gravity Calculation m1 = mn = 0.88 + 4.35 + 0.795 + 0.5 = 6.525 kg 1 m1 X = x (mn x xn) 1 6.525 = (0.88 x 65 + 4.35 x 150 + 0.795 x 150 + 0.5 x 150) = 138.5 mm 1 m1 Y = x (mn x yn) 1 6.525 = (0.88 x 0 + 4.35 x 0 + 0.795 x 111 + 0.5 x 210) = 29.6 mm 1 m1 Z = x (mn x zn) 1 6.525 = (0.88 x 5 + 4.35 x 42.5 + 0.795 x 42.5 + 0.5 x 42.5) = 37.4 mm 4.

Wn Weight mn X-axis Xn Y-axis Yn Z-axis Zn Z X Wa 0.88kg 65mm 0mm 5mm 111 Wb 4.35kg 150mm 0mm 42.5mm Y 210 Y Wc 0.795kg 150mm 111mm 42.5mm Wd 1.5kg 150mm 210mm 42.5mm n = a, b, c, d 3 Composite center of gravity calculation m3 = mn = 0.88 + 4.35 + 0.795 + 1.5 = 7.525kg 1 m3 X = x (mn x xn) 1 7.525 = (0.88 x 65 + 4.35 x 150 + 0.795 x 150 + 1.5 x 150) = 140.1mm 1 m3 Y = x (mn x yn) 1 7.525

Mass mn Y Y-axis Yn Z-axis Zn X-axis Xn X Wa 5mm 0mm 65mm 0.88kg 210 65 111 Z Wb 42.5mm 0mm 150mm 4.35kg 150 Wc 42.5mm 111mm 150mm 0.795kg Wd 42.5mm 210mm 150mm 0.5kg Y 42.5 5 n = a, b, c, d 3 Composite center of gravity calculation m = mn = 0.88 + 4.35 + 0.795 + 0.5 = 6.525kg 1 m X = x (mn x Xn) 1 6.525 = (0.88 x 65 + 4.35 x 150 + 0.795 x 150 + 0.5 x 150) = 138.5mm 1 m Y = x (mn x

Composite Center of Gravity Calculation m3 = mn = 0.88 + 4.35 + 0.795 + 1.5 = 7.525 kg 1 m3 X = x (mn x xn) 1 7.525 = (0.88 x 65 + 4.35 x 150 + 0.795 x 150 + 1.5 x 150) = 140.1 mm 1 m3 Y = x (mn x yn) 1 7.525 = (0.88 x 0 + 4.35 x 0 + 0.795 x 111 + 1.5 x 210) = 53.6 mm 1 m3 Z = x (mn x zn) 1 7.525 = (0.88 x 5 + 4.35 x 42.5 + 0.795 x 42.5 + 1.5 x 42.5) = 38.1 mm 4.

m3 Y = x (mn x yn) 1 7.025 = (0.88 x 0 + 4.35 x 0 + 0.795 x 111 + 1.0 x 210) = 42.5 mm 1 m3 Z = x (mn x zn) 1 7.025 = (0.88 x 5 + 4.35 x 42.5 + 0.795 x 42.5 + 1.0 x 42.5) = 37.8 mm 4 Calculation of load factor for static load m3: Weight m3 max (from 1 of graph MY2H / m3) = 22.5 (kg) .

M3 1 3 mn x g M1E mn x g M3E x FE x Y M3E FE FE Note) Regardless of the mounting orientation, dynamic moment is calculated using the formulas above.

Wn Mass mn X-axis Xn Y-axis Yn Z-axis Zn Z X Wa 0.88kg 65mm 0mm 5mm 111 Wb 4.35kg 150mm 0mm 42.5mm Y 210 Y Wc 0.795kg 150mm 111mm 42.5mm Wd 1.5kg 150mm 210mm 42.5mm n = a, b, c, d 3 Composite center of gravity calculation m = mn = 0.88 + 4.35 + 0.795 + 1.5 = 7.525kg 1 m X = x (mn x xn) 1 7.525 = (0.88 x 65 + 4.35 x 150 + 0.795 x 150 + 1.5 x 150) = 140.1mm 1 m Y = x (mn x yn) 1 7.525

Wn Mass mn X-axis Xn Y-axis Yn Z-axis Zn Z X Wa 0.88kg 65mm 0mm 5mm 111 Wb 4.35kg 150mm 0mm 42.5mm Y 210 Y Wc 0.795kg 150mm 111mm 42.5mm Wd 0.5kg 150mm 210mm 42.5mm n = a, b, c, d 3 Calculation of composite center of gravity m = mn = 0.88 + 4.35 + 0.795 + 0.5 = 6.525kg 1 m X = x (mn x xn) 1 6.525 = (0.88 x 65 + 4.35 x 150 + 0.795 x 150 + 0.5 x 150) = 138.5mm 1 m Y = x (mn x yn) 1 6.525

1/8 1/8 1/8 1/8 C6 Base mounted For internal pilot VZ54 VV3Z5-41-1 1/4 1/4 C8 Body ported For external pilot VV3Z5-21R-1 VZ52R 2.2 0.34 0.55 2.4 0.32 0.62 1/4 1/8 Courtesy of Steven Engineering, Inc.-230 Ryan Way, South San Francisco, CA 94080-6370-Main Office: (650) 588-9200-Outside Local Area: (800) 258-9200-www.stevenengineering.com VV3Z5-41R-2 1/4 1/4 1/8 1/8 C6 C8 2.2 2.0 1.6 2.1 0.35

Intermediate strokes (1 to 99 mm) are available in 1 mm increments.

VJ100M1.7 x 15 VJ300M1.7 x 22 Note) In the case of ZX1VJ114, M, MN and MO cannot be used. 13-2-7 7 Series ZX Ejector Unit Specifications 1 2 ZX1-W07 1 2 ZX1-W10 1 2 Unit no. ZX1-W05 0.5 5 13 Nozzle dia.

16 3/8 3/8 3/4 5/8 1.57 1 1/2 3 3/4 1 1/4 1 3/8-24 325 (3.25) 1 1/8 3.9 1/2 0 7 1/2 1 1 1/4 1.18 2.34 4 1/4 1 3/8 3/4 5/8 2.72 8 1/4 3/4-16 3/4 7/8 1/2 5/8 1.57 1 1/8 1 1/2 3/8-24 4 1/2 1 1/4 1 400 (4) 4.7 1/2 0 7 1/2 1 1 1/4 1.18 2.34 4 1/4 1 3/8 3/4 5/8 2.72 8 1/4 3/4-16 3/4 7/8 1/2 5/8 Courtesy of Steven Engineering, Inc. !

4 VXD2130-02 10 1.9 34 0.5 0.4 0.9 0.7 0.02 0.7 0.5 3/8 VXD2130-03 10 2.4 43 0.5 0.4 0.9 0.7 0.02 1 1 3/8 VXD2140-03 15 4.5 80 1.5 0.7 0.7 1 1 0.02 0.02 0.5 1/2 VXD2130-04 10 2.4 43 0.5 0.4 0.9 0.7 0.02 1 1 1/2 VXD2140-04 15 5.5 100 0.7 0.7 1 1 0.02 1 1 3/4 VXD2150-06 20 9.5 170 0.7 0.7 1 1 T E C H N I C A L SPECIFICATIONS E N E R G I Z E D C L O S E D T Y P E S E R I E S VXD 1MPa = 145PSI

Calculation of Composite Center of Gravity m3 = mn = 0.88 + 4.35 + 0.795 + 0.5 = 6.525 kg 1 m3 X = x (mn x xn) 1 6.525 = (0.88 x 65 + 4.35 x 150 + 0.795 x 150 + 0.5 x 150) = 138.5 mm 1 m3 Y = x (mn x yn) 1 6.525 = (0.88 x 0 + 4.35 x 0 + 0.795 x 111 + 0.5 x 210) = 29.6 mm 1 m3 Z = x (mn x zn) 1 6.525 = (0.88 x 5 + 4.35 x 42.5 + 0.795 x 42.5 + 0.5 x 42.5) = 37.4 mm 4.