Options - Panasonic MINAS A4P Series Instruction Manual

Options

Specifications of for Motor Connector
• Pin disposition for encoder connector
MSMA
MDMA
MFMA
MHMA
MGMA
A
M B
N
C
L
P
T
D
K
S R
J E
H F
G
N/MS3102A20-29P
• Specifications of 2500P/r
incremental encoder
Pin No. Content Pin No. Content
PS
A NC K
B NC L
PS
C NC M NC
D NC N NC
E NC P NC
F R
NC NC
G EOV S NC
H E5V T
NC
Frame
J
GND
• Pin disposition for motor/brake connector (without brake)
MSMA 1kW, 1.5kW, 2kW
MDMA 1kW, 1.5kW, 2kW
MHMA 500W, 1kW, 1.5kW
MGMA 900W
D A
C B
JL04V-2E20-4PE-B-R
(by Japan Aviation
Electronics or equivalent)
Content
PIN No.
A U-phase
B V-phase
C W-phase
D Earth
Do not connect anything to NC pins.
180
MSMA
MDMA
MFMA
MHMA
MGMA
A
M B
N
C
L
P
T
D
K
S R
J E
H F
G
N/MS3102A20-29P
• Specifications of 17bit
absolute/incremental
encoder
Pin No. Content Pin No. Content
PS
A NC K
B NC L
PS
C NC M NC
D NC N NC
E NC P NC
F R
NC NC
G EOV S BAT–*
H E5V T
BAT+*
Frame
J
GND
*Connection to Pin-S and T are not
required when used in incremental.
MSMA 3kW, 4kW, 5kW
MDMA 3kW, 4kW, 5kW
MHMA 2kW,3kW,4kW,5kW
MGMA 2kW, 3kW, 4.5kW
D A
C B
JL04V-2E22-22PE-B-R
(by Japan Aviation
Electronics or equivalent)
Content
PIN No.
A U-phase
B V-phase
C W-phase
D Earth
• Pin disposition for motor/brake connector (with brake)
MSMA 1kW, 1.5kW, 2kW
MDMA 1kW, 1.5kW, 2kW
MFMA 400W, 1.5kW
MHMA 500W, 1kW, 1.5kW
MGMA 900W
G H A
B
F I
E D C
JL04V-2E20-18PE-B-R
(by Japan Aviation
Electronics or equivalent)
Content
Pin No.
G Brake
H Brake
A NC
F U-phase
I V-phase
B W-phase
E Earth
D Earth
C NC
MFMA 400W, 1.5kW
G H A
B
F I
E D C
JL04V-2E20-18PE-B-R
(by Japan Aviation
Electronics or equivalent)
Content
PIN No.
G NC
H NC
A NC
F U-phase
I V -phase
B W-phase
E Earth
D Earth
C NC
MSMA 3kW, 4kW, 5kW
MDMA 3kW, 4kW, 5kW
MFMA 2.5kW, 4.5kW
MHMA 2kW,3kW,4kW,5kW
MGMA 2kW, 3kW, 4.5kW
A B C
D E F
G H I
JL04V-2E24-11PE-B-R
(by Japan Aviation
Electronics or equivalent)
Content
Pin No.
A Brake
B Brake
C NC
D U-phase
E V-phase
F W-phase
G Earth
H Earth
NC
I
MFMA 2.5kW, 4.5kW
A B C
D E F
G H I
JL04V-2E24-11PE-B-R
(by Japan Aviation
Electronics or equivalent)
Content
PIN No.
A NC
B NC
C NC
D U-phase
E V -phase
F W-phase
G Earth
H Earth
I NC