Patent ReferencesSystem for producing and distributing electrical energy for vehicles particularly aircraft, as well as an electrical power center for such a system Boost/buck DC/DC converter Cross-start bus configuration for a variable speed constant frequency electric power system Electric power supply apparatus Low distortion alternating current output active power factor correction circuit using bi-directional bridge rectifier and bi-directional switching regulator Bidirectional power converter modules, and power system using paralleled modules Power distribution center Neutral base for disconnect switch and method of assembling same Patent #: 5737195 InventorsAssigneeApplicationNo. 843408 filed on 04/15/1997US Classes:307/125, Electrical307/23, Substitute or alternate source307/43, PLURAL SUPPLY CIRCUITS OR SOURCES307/64, Substitute or emergency source307/82, Plural converters307/85, Connecting or disconnecting323/222, Using choke and switch across source323/224With additional series regulatorExaminersPrimary: Gaffin, JeffreyAssistant: Kaplan, Jonathan S. Attorney, Agent or FirmInternational ClassH01H 047/00AbstractAn aircraft electrical supply bus supplementing arrangement in which electrical energy is stored in a large capacitor and energy flow between the capacitor and the bus is controlled by a bi-directional electrical converter circuit of the switched inductance type. The varying terminal voltage of the energy storing capacitor, a super capacitor, is coupled to the relatively fixed voltage of the aircraft supply bus by way of the voltage changing capability of the converter circuit switched inductance. Current flow levels in this inductance are controlled with a negative feedback regulator circuit. Energy storage efficiency in the converter is enhanced with respect to weight and physical size of the capacitor element by ability of the converter circuit to accept a widely varying input voltage while generating a relatively constant output voltage. Suppression of electrical transients and improved regulation of voltage on the aircraft energy supply bus especially at distal and bus impedance-isolated locations are achieved.Field of SearchPLURAL SUPPLY CIRCUITS OR SOURCESOne source floats across or compensates for other source With intervening converter Storage battery or accumulator-type source Substitute or emergency source Plural substitute sources Storage battery or accumulator Load transfer without paralleling sources Selective or optional sources Plural converters Plural generators Connecting or disconnecting Condition responsive Attainment of voltage, frequency or phase relationship Plural sources of supply Substitute or alternate source Using choke and switch across source Using a three or more terminal semiconductive device With additional series regulator Switched (e.g., switching regulators) Digitally controlled With threshold detection With plural condition sensing | |