Non-Standard Motor Compatible Drivers Matsushita Electric Industrial Co., Ltd. Drivers for LJ1, LG1, LX

Signal description Symbol Digital output power supply Failure Positioning complete Z phase pulse Interface power supply common Reverse pulse line Reverse pulse line Normal pulse line Normal pulse line 1 2 3 4 5 7 8 9 10 V+ ALM PF OP SG NP NG PP PG 11 12 13 14 15 16 17 19 20 Shield SD SG CR LSN LSP V5 SON OPC V24 Driver model MR-C10A MR-C20A MR-C10A1 MR-C20A1 Interface power supply common

Precision Air Slide Table Series MXP ø6, ø10, ø12, ø16, (ø8: new addition, see 8-8-23 ) 1

Examine Mr. [As Mp and My does not arise, examination is not needed.] Mr = 0.2 x 9.8 (20 + 6.8)/1000 = 0.053 Ma = Mmax Find the allowable static moment Ma (Nm).

Series MXP Precision Air Slide Table

Examine for Mr [As Mp and My does not arise, Examination is not needed.] Mr=2(20+6.8)/1000=0.054 A2=6.8 Calculate allowable static moment Ma(Nm). Mar=14.2=4.2 =1 Mr max.=4.2 2=0.054/4.2=0.013 Calculate load rate (2) of static moment. 2=M/Ma 3-3 Load rate of kinetic moment Calculate kinetic moment Me(Nm).

Battery-less

Mr: Roll moment H H, L: Distance to the point at which the load is applied [mm] Model Allowable vertical load Fv [N] Static allowable moment Pitch moment: Mp [Nm] Yaw moment: My [Nm] Roll moment: Mr [Nm] LEHF32EK2-l 176 1.4 1.4 2.8 LEHF40EK2-l 294 2 2 4 * Values for load in the table indicate static values.

240

MXH10 0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04 0.045 0.05 0 0.5 1 1.5 2 2.5 3 3.5 Roll moment Mr (Nm) MXH16 0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 0 1 2 3 4 5 6 7 Roll moment Mr (Nm) MXH20 0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0 2 4 6 8 10 12 Roll moment Mr (Nm) 22 Compact Slide MXH Series Construction MXH MXH !2 !3 !1 t y u i !4 w q !

This is a legacy product, and replaced byAW40-04-12R-A, AW MASS PRO 1/2 MODULAR (PT), AIRLINE EQUIPMENT, AW MASS PRO, FA, AW MASS PRO 1/2 MODULAR (PT), 1.79431 lb

1 Blow Gun Series VMG K
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MS 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 T
VMG Pressure loss is less than 1%. (nozz

Ryan Way, South San Francisco, CA 94080-6370-Main Office: (650) 588-9200-Outside Local Area: (800) 258-9200-www.stevenengineering.com Type Nozzle model Without nozzle KN-R02-100 KN-R02-150 KN-R02-200 KN-R02-250 KNH-R02-100 KNH-R02-150 KNH-R02-200 KNS-R02-075-4 KNS-R02-090-8 KNS-R02-100-4 KNS-R02-110-8 KNL3-06-150 KNL3-06-200 KNL6-06-150 KNL6-06-200 Nozzle size Standard type Nil 01 02 03 04

Cylinder with Lock

Single clevis: CP96NC Double clevis: CP96ND CD EB UB CB EW MR L XD + Stroke Double clevis Single clevis [mm] Bore size CBH14 CDH9 EB EW L MR UBh14 XD 32 26 10 65 26 0.2 0.6 12 9.5 45 200 40 28 12 75 28 0.2 0.6 15 12 52 226 50 32 12 80 32 0.2 0.6 15 12 60 245 63 40 16 90 40 0.2 0.6 20 16 70 269.5 80 50 16 110 50 0.2 0.6 20 16 90 320 100 60 20 140 60 0.2 0.6 25 20 110 353.5 Pivot Bracket: Double

MXH

CX 0.005 0 D0 0.20 0.39 0.59 Roll moment Mr (Nm) -X MXH10 200.09 0.08 0.07 Data 0.06 0.05 0.04 0.03 0.02 0.01 0 0 0.20 0.98 1.18 1.37 0.78 0.59 0.39 Roll moment Mr (Nm) MXH16 0.06 0.05 Displacement (mm) Displacement (mm) 0.04 0.03 0.02 0.01 0 0 0.78 1.18 1.57 1.96 2.35 2.75 Roll moment Mr (Nm) MXH20 0.1 0.09 0.08 0.07 0.06 0.05 0.04 0.03 0.02 0.01 0 0 0.78 1.57 2.35 3.14 3.92 4.71 5.49 Roll

15

Dimensions: Motor Top/Parallel LEY25, 32, 63 ZZ Y2 Motor flange Motor LEF Rod operating range Note 1) (Stroke + G mm) H thread depth C LEJ T U M LEL EV J LEM D 4 x O1 thread depth R K Note 2) LEY Y1 B + Stroke L S M 4 x O1 M EH thread depth R LES XA H9 depth XA 6 x MO thread depth MR LEPY LEPS Section XX details MH LER LEH MD MC ML + Stroke Section XX XB XA H9 XA LEY -X5 L MA 11LEFS IP65

Table of Contents

.-230 Ryan Way, South San Francisco, CA 94080-6370-Main Office: (650) 588-9200-Outside Local Area: (800) 258-9200-www.stevenengineering.com Mr Mp MHS Fv L MHC MHT MHY L: Distance to the point at which the load is applied (mm) Maximum allowable moment MHW Allowable vertical load Fv (N) Model Pitch moment: Mp (Nm) Yaw moment: My (Nm) Roll moment: Mr (Nm) MRHQ MHZ2-6 0.08 0.04 0.04 10 Misc.

MXH Series Compact Slide

Allowable moment N m (ft lb) Pitch moment Yaw moment Roll moment Model Mp My Mr MXH6 MXH10 MXH16 MXH20 0.47 (0.35) 0.39 (0.29) 0.59 (0.44) MXH6 0.96 (0.71) 0.82 (0.60) 1.37 (1.01) 1.88 (1.34) 1.59 (1.17) 2.75 (2.03) 0.04 3.14 (2.03) 2.75 (4.05) 5.49 (4.05) 0.035 0.03 Displacement (mm) Displacement (mm) 0.025 0.02 0.015 0.01 0.005 0 0 0.20 0.39 0.59 Roll moment Mr(Nm) 1 N m = 0.7375 ft

C95

.-230 Ryan Way, South San Francisco, CA 94080-6370-Main Office: (650) 588-9200-Outside Local Area: (800) 258-9200-www.stevenengineering.com Flange style (F, G) Head side mounting (G) Rod side mounting (F) Rear double clevis D Head side single clevis style (C) Head side double clevis style (D) Bore size (mm) EW -0.2 -0.6 MR FB CD H9 XV Z TD e8 E1 R W MF ZF EB L XD UB h14 CB H14 TR AO AT XA

MXF

My = 0.5 x 9.8 (10 + 11)/1000 = 0.11 A3 = 11 May = 1 x 1 x 9.14 = 9.14 Mymax = 9.14 K = 1 = 1 2 = 0.11/9.14 = 0.012 Examine Mr.

CRQ2

Linear motion E m V Rotary actuator I = mr m: Mass (kg) (However, the weight of the L section is ignored) E= I Formula (2) 2 1 = mr 2 1 This indicates the moment of inertia with respect to the rotation axis of a mass "m" which is a distance "r" from the rotational axis. The formula for finding the moment of inertia differs depending on the shape of the object.

Air Slide Table Long Stroke Type Series MXY ø6, ø8, ø12 1

M = W x 9.8 (Ln + An)/1000 Corrected value of moment center position distance An: Table (1) Examine Mr. Mr = 0.2 x 9.8 (40 + 15.5)/1000 = 0.1 A2 = 15.5 Obtain Mar = 13 from Va = 300 in Graph (3). Find the allowable static moment Ma (Nm). Pitch, Yaw moment: Graph (2) Roll moment: Graph (3) 13 Find the load factor 1 of the static moment.

Compact Rotary Actuator Rack-and-Pinion Type/Sizes: 10, 15, 20, 30, 40 Series CRQ2

Linear motion E m V Rotary actuator I = mr m: Mass (kg) (However, the weight of the L section is ignored) E= I Formula (2) 2 1 = mr 2 1 This indicates the moment of inertia with respect to the rotation axis of a mass "m" which is a distance "r" from the rotational axis. The formula for finding the moment of inertia differs depending on the shape of the object.

Air Slide Table Series MXQ

= W/Wa 3-2 Load factor of static moment Rolling Yawing Examine Mr. Mr = 1 x 9.8 (30 + 10.5)/1000 = 0.39 A = 10.5 Examine My. My = 1 x 9.8 (10 + 30)/1000 = 0.39 A3 = 30 Find the static moment M (Nm). M = W x 9.8 (Ln + An)/1000 Corrected value of moment center position distance An: Table 3 Find the allowable static moment Ma (Nm).

MXQ

Wa = 1 x 1 x 4 = 4 K = 1 = 1 Wmax = 4 1 = 1/4 = 0.25 3-2 Load Factor of the Static Moment Rolling Yawing Examine Mr. Mr = 1 x 9.8 (30 + 10.5)/1000 = 0.39 A6 = 10.5 Mar = 36 Mrmax = 36 K = 1 = 1 '2 = 0.39/36 = 0.011 Examine My.

This is a legacy product, and replaced byAW40-04-B, FILTER REGULATOR, MODULAR, AIRLINE EQUIPMENT, AW MASS PRO, FA, AW MASS PRO 1/2 MODULAR (PT), 1.77868 lb