FAB1204022 PST | Alldatasheet
Document overview
- Manufacturer or author: Provided By ALLDATASHEET.COM(FREE DATASHEET DOWNLOAD SITE)
- PDF pages: 3
Technical content
FEATURES
INPUT : 115Vac Comply with Airbus AC Power requirement 360-820Hz OUTPUT : 335Vdc 400W -55°C +100°C operating INPUT V oltage range : 90-132Vac Frequency : 360-820Hz comply with Airbus MP240300229, ABD100.1.8 PFC correction Input protection : fuse transient and surges protected MILSTD-704F inrush current limitation EMI : MIL STD-461E CE101, CE102 Power interruption : Ouptut voltage is maintained above 180Vdc during a 200ms input AC interruption at 300W. OUTPUT V oltage : 335Vdc Current : 1,2A max. Typ. Line regulation Load regulation Ripple and noise Current limit 2 % 7 % 5 % 135 % of I nominal Low line to high line ; full load No load to full load Peak to peak, nom. Input ; full load 5 % 10 % 8 % OUTPUT Conditions Max.
APPLICATIONS
Power factor corrected AC front end for avionic application. FAB1204022 1/3Rev. 02
Safety : built to meet EN60950 EMI : Built to meet MIL-STD461E CE101, CE102 PFC : Built to meet ABD100.1.8 No laboratory certification, certified in the customer equipment. ENVIRONMENTAL Storage temperature : -65°C to +125°C Operating temperature : -55°C to 100°C baseplate, chassis mounting ISOLATION Input to chassis : 1500 Vrms or 2121 Vdc Input to Output : None GENERAL FAB1204022 2/3Rev. 02 SIGNALS ON/OFF control : control of the DC/DC converter supplied by the front end Power Fail
DESCRIPTION
INPUT : SUBD 9 pts male PIN2 AC/N PIN 5 Ground CN2 PIN1 +HT OUTPUT : SUBD 9 pts female PIN2 -HT FAB1204022 3/3Rev. 02 PIN 3-4-6 to 9 Ground PIN3 Pow_fail_c PIN5 Ground PIN7 INH-G PIN8 Pow_fail_e PIN4-6-9 NC