28VDC Transformer Rectifier Assembly
2Pages

28VDC Transformer 28VDC Transformer 28VDC Transformer Rectifier Assembly Rectifier Assembly Rectifier Assembly Introduction Introduction The Transformer-Rectifier provides 28.5- volts DC (nominal) The Transformer-Rectifier provides 28.5Introductionto supply necessary energy for aircraft withto supply necessary volts DC (nominal) 28-volt DC power The Transformer-Rectifier provides 28.5requirements. The DC voltage isDC power energy for aircraft with 28-volt derived volts DC (nominal) to (furnished is derived from a 400 Hz source supply necessary requirements. The DC voltage by othenergywhich is Hz source28-volt DC by of ers), for400 connected(furnished power from a aircraft with to the input othrequirements. is connected to A is derived the Transformer-Rectifier unit. the input of ers), which The DC voltage massive from pulse, silicon rectifier/heat sink as12 aTransformer-Rectifier unit. A massive the 400 Hz source (furnished by othsembly with aconnected to the input of sophisticated, controlled ers), which issilicon rectifier/heat sink as12 pulse, step downwith a sophisticated,Acontrolled transformer provides smooth thesembly Transformer-Rectifier unit. massive DCpulse, load. rectifier/heat sink asfor down transformer provides fans 12 step the siliconFour highly reliablesmooth provide with load. forced highly controlled DC the a Four cooling for all semblyfor efficientsophisticated,reliable fans components withinforced cooling smooth the Transformerprovide efficient step down transformer provides for all Rectifier unit. components within highly reliable fans DC for the load. Four the TransformerRectifier unit. provide efficient forced cooling for all components within the may be connected to the external 400 Hz source via a standard aircraft receptacle TransformerThe Transformer-Rectifier Rectifier unit.the rear of the Transformer-Rectifier to the external via hard wired conduit connection in place of the mounted on The Transformer-Rectifier may be connected or, alternately, 400 Hz source via a standard aircraft receptacle receptacle. on the rear of the Transformer-Rectifier or, alternately, via hard wired portableconnection in place of the mounted The Transformer-Rectifier could be mounted on a portable generator, conduit cart, or upon a passenger loading bridge. Transformer-Rectifier could be mounted on aunit allows mounting portable cart, or upon passenreceptacle. The The low profile of the Transformer-Rectifier portable generator, to the underside of a a passenThe loading bridge cab next to a point of the Transformer-Rectifier unit allows mounting to thestandard aircraft receptacle ger Transformer-Rectifier may be of use converterthe external 400 Hz source via a underside of a passenger loading bridge. The low profile connected to without causing ground mounted on the rearcab the Transformer-Rectifier or, without causing groundwired conduit connection in place of the alternately, via hard ger loading bridge of addition, if the Transformer-Rectifier is mounted under the passenger loading bridge, it clearance problems. In next to a point of use converter receptacle. The Transformer-Rectifier couldsource by means of portable generator, portable cart, or upon a passenbe mounted on may be conveniently connected to the 400 Transformer-Rectifier a the existing 400 Hz aircraft ground powerbridge, it clearance problems. In addition, if the Hz is mounted under the passenger loading cable. germay be convenientlyflexibility at bridges servicing aircraft with different power requirements. the underside of a passenloading bridge. The low profile of the Transformer-Rectifier unit allows mounting to ground power cable. This allows maximum connected to the 400 Hz source by means of the existing 400 Hz aircraft gerThis allows maximumnext to a at bridges servicing aircraft with different power requirements. loading bridge cab flexibility point of use converter without causing ground clearance problems. In addition, if the Transformer-Rectifier is mounted under the passenger loading bridge, it may be conveniently connected to the 400 Hz source by means of the existing 400 Hz aircraft ground power cable. This allows maximum flexibility Standard Features at bridges servicing aircraft with different power requirements.   Standard Features AC Input 204Y/118 volts, 3 phase-4 wire, 400Hz  DC Output 28.5 volts nominal, in accordance with MIL-STD-704E voltage AC Input 204Y/118 volts, 3 phase-4 wire, 400Hz limits Output 28.5 volts nominal, in accordance with MIL-STD-704E voltage  DC limits Control panel with Digital Voltmeter, Digital Ammeter, Output ON/OFF Buttons, Output withIndicator, 400Hz Input Indicator, Current Limit (Soft  Control panel ON Digital Voltmeter, Digital Ammeter, Output ON/OFF start) Adjustment, Current 3 phase-4 wire, 400Hz AC Buttons,204Y/118 volts, Limit Disabled Indicator, Current Limit ON/OFF Input Output ON Indicator, 400Hz Input Indicator, Current Limit (Soft Control Adjustment, Current Limit Disabled Indicator, Current Limit ON/OFF start) DC Output 28.5 volts nominal, in accordance with MIL-STD-704E voltage Control Four limits Fans in high performance push-pull configuration  Over Temperature Protection Self-resetting configuration Four Fans in high performance push-pull thermal switches on Control panel with Digital Voltmeter, Digital Ammeter, Outputrectifier ON/OFF  heat sinks Over Output ON Protection Self-resetting thermal switches Limit (Soft Buttons,Temperature Indicator, 400Hz Input Indicator, Currenton rectifier heat Bus start) Adjustment, Current unit, Plated Copper with Bolted Connections Output sinksBars at rear of Limit Disabled Indicator, Current Limit ON/OFF Control Bus Bars at rear of unit, Output   Weather Resistant Construction Plated Copper with Bolted Connections   Four Fans in high performance push-pullPAGE Green Weather Resistant Construction Powder Coat Finish in High Gloss White or configuration  Over Temperature Protection Self-resetting thermal switches on rectifier  Powder Coat Finish in High Gloss White or PAGE Green heat sinks Output Bus Bars at rear of unit, Plated Copper with Bolted Connections www.pageindustries.com www.pageindustries.com Toll Free 1-855-465-PAGE Toll F(1-855-465-7243) ree 1-855-465-PAGE (1-855-465-7243) Phone 1-707-469-7243 P 1-707-469-7243 Fax honewww.pageindustries.com 1-707-469-7244 Fax 1-707-469-7244 Email Toll Free 1-855-465-PAGE Email GSE sales@pageindustries.com PAGE sales@pageindustries.com PAGE GSE 2050 Cessna Drive Phone 1-707-469-7243 ax 1-707-469-7244 FVacaville, CA 95688 USA Email USA 2050 Cessna Drive Vacaville, CA 95688