Supercapacitor-Based Automatic Energy-Saving System of Direct-Current High-Voltage Beam Pumping Unit
US-2024405679-A1 · Dec 5, 2024 · US
US10014790B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10014790-B2 |
| Application number | US-201213450562-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 19, 2012 |
| Priority date | Apr 19, 2012 |
| Publication date | Jul 3, 2018 |
| Grant date | Jul 3, 2018 |
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A dual function solid state power converter operable from a three phase AC input current simultaneously provides; an AC or DC output current on an aircraft power cable to provide ground power to a parked aircraft, and a low voltage DC current on a battery charging power cable to charge batteries in nearby service vehicles. The power converter includes an AC to DC converter which converts the current on an internal DC bus, a DC to AC converter which converts the DC bus current to an AC current at a higher voltage and frequency, or a DC to DC converter which converts the DC bus current to a lower voltage DC, for supplying ground power to a parked aircraft, and a DC to DC converter for converting the DC bus current to a lower voltage battery charging current on the battery charging cable.
Opening claim text (preview).
I claim: 1. A dual purpose power converter, comprising: an airport terminal applied alternating current supply input; a rectifier circuit for converting the applied alternating current supply to a direct current; an inverter circuit for converting said direct current from said rectifier circuit to primary AC output current, said primary AC output current coupled to a parked aircraft connector; a direct current conversion circuit for converting said direct current from said rectifier circuit to the secondary DC output current, said secondary DC output current coupled to a ground support vehicle connector; and a control circuit for controlling operation of said rectifier circuit, said inverter circuit and said conversion circuit in response to control signals whereby said power converter simultaneously provides power to a parked aircraft coupled to said aircraft connector and to a ground support vehicle coupled to said vehicle connector. 2. A dual purpose power converter as defined in claim 1 wherein said rectifier circuit comprises a thyristor bridge circuit. 3. A dual purpose power converter as defined in claim 2 wherein said thyristor bridge circuit includes a direct current filter. 4. A dual purpose power converter as defined in claim 1 wherein said inverter circuit comprises a three phase DC to AC inverter circuit. 5. A dual purpose power converter as defined in claim 4 wherein said DC to AC inverter circuit includes an output filter. 6. A dual purpose power converter as defined in claim 5 wherein said DC to AC inverter circuit further includes an output transformer. 7. A dual purpose power converter as defined in claim 1 wherein said DC to DC converter includes a regulation circuit responsive to output load voltage and load temperature.
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