36v prolynx, 5a: non-isolated dc-dc power modules, Data sheet – GE Industrial Solutions 9-36V ProLynx 5A User Manual

Page 16

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GE

Data Sheet

9-36V ProLynx

TM

5A: Non-Isolated DC-DC Power Modules

9Vdc –36Vdc input; 3Vdc to 18Vdc output; 5A to 2.5A Scaled output current

9Vdc –24Vdc input; -3.3Vdc to -18Vdc output; 5A to 0.7A Scaled output current

July 23, 2013

©2012 General Electric Company. All rights reserved.

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Shock and Vibration

The ruggedized (-D version) of the modules are designed to withstand elevated levels of shock and vibration to be able to operate
in harsh environments. The ruggedized modules have been successfully tested to the following conditions:

Non operating random vibration:
Random vibration tests conducted at 25C, 10 to 2000Hz, for 30 minutes each level, starting from 30Grms (Z axis) and up to
50Grms (Z axis). The units were then subjected to two more tests of 50Grms at 30 minutes each for a total of 90 minutes.

Operating shock to 40G per Mil Std. 810F, Method 516.4 Procedure I:
The modules were tested in opposing directions along each of three orthogonal axes, with waveform and amplitude of the shock
impulse characteristics as follows:

All shocks were half sine pulses, 11 milliseconds (ms) in duration in all 3 axes.

Units were tested to the Functional Shock Test of MIL-STD-810, Method 516.4, Procedure I - Figure 516.4-4. A shock magnitude of

40G was utilized. The operational units were subjected to three shocks in each direction along three axes for a total of eighteen
shocks.

Operating vibration per Mil Std 810F, Method 514.5 Procedure I:

The ruggedized (-D version) modules are designed and tested to vibration levels as outlined in MIL-STD-810F, Method 514.5, and
Procedure 1, using the Power Spectral Density (PSD) profiles as shown in Table 1 and Table 2 for all axes. Full compliance with
performance specifications was required during the performance test. No damage was allowed to the module and full
compliance to performance specifications was required when the endurance environment was removed. The module was tested
per MIL-STD-810, Method 514.5, Procedure I, for functional (performance) and endurance random vibration using the performance

and endurance levels shown in Table 5 and Table 6 for all axes. The performance test has been split, with one half accomplished
before the endurance test and one half after the endurance test (in each axis). The duration of the performance test was at least
16 minutes total per axis and at least 120 minutes total per axis for the endurance test. The endurance test period was 2 hours

minimum per axis.

Table 5: Performance Vibration Qualification - All Axes

Frequency

(Hz)

PSD Level

(G2/Hz)

Frequency

(Hz)

PSD Level

(G2/Hz)

Frequency

(Hz)

PSD Level

(G2/Hz)

10 1.14E-03 170 2.54E-03 690 1.03E-03
30 5.96E-03 230 3.70E-03 800 7.29E-03
40 9.53E-04 290 7.99E-04 890 1.00E-03
50 2.08E-03 340 1.12E-02 1070 2.67E-03
90 2.08E-03 370 1.12E-02 1240 1.08E-03

110 7.05E-04 430 8.84E-04 1550 2.54E-03
130 5.00E-03 490 1.54E-03 1780 2.88E-03
140 8.20E-04 560 5.62E-04 2000 5.62E-04

Table 6: Endurance Vibration Qualification - All Axes

Frequency

(Hz)

PSD Level

(G2/Hz)

Frequency

(Hz)

PSD Level

(G2/Hz)

Frequency

(Hz)

PSD Level

(G2/Hz)

10 0.00803 170 0.01795 690 0.00727
30 0.04216 230 0.02616 800 0.05155
40 0.00674 290 0.00565 890 0.00709
50 0.01468 340

0.07901

1070

0.01887

90 0.01468 370 0.07901 1240

0.00764

110 0.00498 430 0.00625 1550 0.01795
130 0.03536 490 0.01086 1780 0.02035
140 0.0058 560 0.00398 2000

0.00398

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