AMETEK MX15 Series - Manual (Page 21)

User Manual – Rev M California Instruments
MX15 21
Displays:
LCD display: A two-line LCD display with backlight provides easy to read guidance
through all setup operations. An adjustable viewing angle makes it easy
to read from all practical locations.
Status indicators: Bright status indicators inform the user of important power source
conditions. The Remote lamp informs the user that the unit is under
remote control. The Overload lamp indicates that excessive current is
being drawn at the output. The Over temperature lamp illuminates when
internal heat sink temperatures are too high. The Hi Range indicator is
lit any time the unit is switched to the high voltage range. The Output
On/Off indicator is on when the power source output relays are closed.
2.6 Special Features and Options
Controller Features
Mode: This option is not available for the MX15.
Parallel Operation: Up to three units can be paralleled in a single-phase configuration (with
one master controller and one or two auxiliary units). (MX30/2 and
MX45/3). Only the master unit requires a controller in this setup. The
auxiliary units are controlled through the system interface.
Clock and Lock Mode:
(Option -LKM and -LKS
required). Up to three units (all with controllers) can be connected in a one, two, or
three-phase configuration using CLOCK and LOCK connections. Each
unit requires its own controller in this configuration. One unit acts as the
master and provides the reference clock to the auxiliary units.
Controller: Programmable controller front panel assembly.
Output Relay: Standard output relay feature to isolate power source from the load.
Output On/Off: The output relay can be used to quickly disconnect the load. An amber
status indicator displays the status of the output relay.
Firmware Options
- 704 Mil Std 704D & E test firmware.
Mil Std 704A, B, C, & F test software (refer to Avionics Software Manual
P/N 4994-971 for details).
Note: Requires use of MXGui Windows application software provided on
CD ROM CIC496.
- 160 RTCA/DO-160D test firmware
RTCA/DO-160E test software (refer to Avionics Software Manual P/N
4994-971 for details)..
Note: Requires use of MXGui Windows application software provided on
CD ROM CIC496.
-411 IEC 61000-4-11 Voltage Dips and Interruptions Test firmware. Supported
over remote control interface only.
-413 IEC 61000-4-13 Interharmonics Test Firmware. Supported over remote
control interface only.
787 Boeing 787 Test software (refer to Avionics Software Manual P/N 4994-
971 for details)..
Note: Requires use of MXGui Windows application software provided on
CD ROM CIC496.
-ABD Airbus ABD0100.1.8 Test software (refer to Avionics Software Manual
P/N 4994-971 for details).
Note: Requires use of MXGui Windows application software provided on