Transducer dc bias is monitored on all signals, Important, Attention – Rockwell Automation 1440-VAD02-01RA XM-123 Aeroderivative Module User Manual

Page 45

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Publication GMSI10-UM003D-EN-P - May 2010

37

Connecting a Velocity Sensor and Two Non-Contact Sensors

Figure 2.27 shows the wiring of a velocity sensor and two non-contact sensors
to the terminal base unit of the XM-123. The velocity sensor is wired to
channel 1. The first non-contact sensor is wired to channel 2, and the other
non-contact sensor is wired to the tachometer input signal.

Figure 2.27 Velocity Sensor and Two Non-Contact Sensor Wiring

ATTENTION

You may ground the cable shield at either end of the cable.
Do not ground the shield at both ends. Recommended
practice is to ground the cable shield at the terminal base
and not at the transducer. Any convenient Chassis terminal
may be used (see Terminal Block Assignments on page 18).

IMPORTANT

Transducer DC bias is monitored on all signals.

IMPORTANT

A jumper from terminal 22 to terminal 21 is required for
channel 2 buffered output. Refer to Configuring Buffered
Output Input Range on page 27.

TYPICAL WIRING FOR COIL-BASED VELOCITY SENSOR

AND TWO NON-CONTACT SENSORS TO XM-123 AERODERIVATIVE MODULE

Pin A - Common
Pin B - Signal

Cable shield not
connected at this end

Shield

0

16

Channel 1 Input Signal

Signal Common

SIG

-24

COM

SIG

-24

COM

17

1

Signal Common

Channel 2 Input Signal

21

22

-24V DC

20

-24V DC

4

Signal Common

Tach Input Signal

36

13

31

Shield

Shield

*

* Note: Jumpering terminal 22 to
terminal 21 configures
CH 2 buffer (-24V to 9V)

18

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