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| | | Thrust and Dynamic Load Mass | | |
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| | | ■What is a thrust? | | ■What is a dynamic load mass? | | |
| | | Table 6 Specifications of I/O connector (CN5) | | |
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| | | | | | | | | | | | | | Pin No. | Signal name | Function | Pin No. | Signal name | Function | | | | 1 | inOi | GENERAL INPUT |l | 26 | OUTO1 | GENERAL OUTPUTO1 | | | | 2 | InO2 | GENERAL INPUT |2 | 27 | OUTO2 | GENERAL OUTPUTO2 | | | | 3 | inO3 | GENERAL INPUT |3 | 28 | OUtO3 | GENERAL OUTPUtO3 | | | | 4 | InO4 | GENERAL INPUT |4 | 29 | OUtO4 | GENERAL OUTPUTO4 | | | | 5 | InO5 | GENERAL INPUT |5 | 30 | OUtO5 | GENERAL OUTPU^5 | | | | 6 | InO6 | GENERAL INPUT |6 | 31 | OUT06 | GENERAL OUTPUtO6 | | | | 7 | InO7 | GENERAL INPUT |7 | 32 | OUtO7 | GENERAL OUTPUTO7 | | | | 8 | InO8 | GENERAL INPUT |8 | 33 | OUT08 | GENERAL OUTPU^8 | | | | 9 | InO9 | GENERAL INPUT |9 | 34 | OUtO9 | GENERAL OUTPUtO9 | | | | 10 | IN10 | GENERAL INPUT 10 | 35 | OUT10 | GENERAL OUTPUT10 | | | | 11 | IN11 | GENERAL INPUT 11 | 36 | OUT11 | GENERAL OUTPUT11 | | | | 12 | IN12 | GENERAL INPUT 12 | 37 | OUT12 | GENERAL OUTPUT12 | | | | 13 | IN13 | GENERAL INPUT 13 | 38 | OUTC | General output common | | | | 14 | IN14 | GENERAL INPUT 14 | 39 | OUTC | General output common | | | | 15 | IN15 | GENERAL INPUT 15 | 40 | +24VI | +24V output supply | | | | 16 | IN16 | GENERAL INPUT 16 | 41 | +24VI | +24V output supply | | | | 17 | IN17 | GENERAL INPUT 17 | 42 | gndi | +24Voutput supply common | | | | 18 | IN18 | GENERAL INPUT 18 | 43 | gndi | +24Voutput supply common | | | | 19 | IN19 | GENERAL INPUT 19 | 44 | A+ | A phase +Output | | | | 20 | IN20 | GENERAL INPUT 20 | 45 | A— | A phase —Output | | | | 21 | inc | General input common | 46 | B+ | B phase +Output | | | | 22 | inc | General input common | 47 | B— | B phase — Output | | | | 23 | MON1 | Monitor output1 | 48 | Z+ | Z phase +Output | | | | 24 | MON2 | Monitor output2 | 49 | Z— | Z phase — Output | | | | 25 | GND | Monitor output common | 50 | GND | Encoder output common | | | | | | | | | | | | | |
| | | A thrust is a force in the moving direction exerted by the moving coil as shown in figure (page 4) illustrating Principle of Operation. The thrust becomes the maximum when the table is at rest, and decreases as the table speed increases. The thrust required for acceleration or deceleration must be examined referring to the graphs of thrust characteristics on page 10 to 12. | | |
| | | A dynamic load mass is the maximum mass that can be placed on the table with required acceleration or deceleration. When examining an operation pattern, the relationship between the mass of load and acceleration/deceleration must be considered because if the mass is larger, acceleration and deceleration have to be lower. The graphs showing the relationship between the dynamic load mass and acceleration on page 10 to 12 are given for the thrust of Linear Motor Table LT at a speed of 1000 mm/s. For example, the acceleration/deceleration under the load of 10kg is about 24m/s2 in maximum in the case of LT150CG. | | |
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| | | ■What is an effective thrust? An effective thrust is the effective value of the thrust required in a given operation pattern. When this value exceeds the rated thrust of Linear Motor Table LT, the motor may overheat or seize. Therefore, make sure that, in principle, the calculated effective thrust does not exceed the rated thrust. Also, note that the operation limit may depend on the operation environment, etc. In general, the effective thrust (Frms) is obtained as follows. (For a calculation example, see page 17.) | | |
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| | | F P2 X t a +( F P - 2 X F l) 2 X 2 a + F l2 X 2c t | | |
| | | F rms — | | |
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| | | •General circuit | | where, Fp is the force required for acceleration/deceleration. Fl is the force due to running resistance consists of the friction of liner motion rolling guide incorporated in Linear Motor Table LT, the pulling resistance of electrical cord, etc. | | |
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| | | In case of internal power supply | | | |
| | | In case of outside power supply | | |
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| | | | | | | | | | | | | InO1 | 1 | -c | | | | InO2 | 2 | -c | | | | inO3 | 3 | | | | | InO4 | 4 | | | | | | | | | | | | IN20 | 20 | | | | inc | 21 | | r | | | | inc | 22 | | | | | | | | | outO1 | 26 | | | | outO2 | 27 | | | | | | outO3 | 28 | | | | | | | | | | r | | | | OUT12 | 37 | | | | OUTC | 38 | | | | | | OUTC | 39 | | | | +24VI | 40 | | | | +24VI | 41 | | | | gndi | 42 | | | | | gndi | 43 | | | | | | | | | | | | GND | 50 | | | | | | | | | | | | | | | | | | | | | | InO1 | 1 | | | | | InO2 | 2 | | | | | inO3 | 3 | | | | | InO4 | 4 | | | | | | | | | | | | IN20 | 20 | | | | inc | 21 | | | | | | inc | 22 | | r | | | | | | | | | outO1 | 26 | | | | outO2 | 27 | | | | | | outO3 | 28 | | | | | | | | | | r | | | | OUT12 | 37 | | | | OUTC | 38 | | | | | | OUTC | 39 | | | | +24VI | 40 | | | | | +24VI | 41 | | | | gndi | 42 | | | | gndi | 43 | | | | | | | | | | GND | 50 | | | | | | | | | | | | |
| | —0^0- | | —cT"o— | | |
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| | | V | | |
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| | | T3 CD 03 Q. CO | | |
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| | | L | | |
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| | | Time | | |
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| | | F? | | |
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| | -\4- | | |
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| | | CO | | |
| | F | a | | |
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| | | Fl | | |
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| | | Time | | |
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| | | fa | | fc | | fa | | |
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| | | 1N=0.102kgf=0.2248lbs. 1mm=0.03937inch 16 | | |
| | | 15 | | |
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