U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Super capacitor battery clone

Patent 5850113 Issued on December 15, 1998. Estimated Expiration Date: Icon_subject April 15, 2017. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

System for producing and distributing electrical energy for vehicles particularly aircraft, as well as an electrical power center for such a system
Patent #: 4551632
Issued on: 11/05/1985
Inventor: Jourdan ,   et al.

Boost/buck DC/DC converter
Patent #: 4801859
Issued on: 01/31/1989
Inventor: Dishner

Cross-start bus configuration for a variable speed constant frequency electric power system
Patent #: 4967096
Issued on: 10/30/1990
Inventor: Diemer, et al.

Electric power supply apparatus
Patent #: 5256907
Issued on: 10/26/1993
Inventor: Shimada, et al.

Low distortion alternating current output active power factor correction circuit using bi-directional bridge rectifier and bi-directional switching regulator
Patent #: 5359277
Issued on: 10/25/1994
Inventor: Cowett, Jr.

Bidirectional power converter modules, and power system using paralleled modules
Patent #: 5602464
Issued on: 02/11/1997
Inventor: Linkowsky, et al.

Power distribution center
Patent #: 5612579
Issued on: 03/18/1997
Inventor: Wisbey, et al.

Neutral base for disconnect switch and method of assembling same Patent #: 5737195
Issued on: 04/07/1998
Inventor: Cassity, et al.

Inventors

Assignee

Application

No. 843408 filed on 04/15/1997

US 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 regulator

Examiners

Primary: Gaffin, Jeffrey
Assistant: Kaplan, Jonathan S.

Attorney, Agent or Firm

International Class

H01H 047/00

Abstract

An 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.

PatentsPlus Images
Enhanced PDF formats
loading...
PatentsPlus: add to cart
PatentsPlus: add to cartSearch-enhanced full patent PDF image
$9.95more info
PatentsPlus: add to cart
PatentsPlus: add to cartIntelligent turbocharged patent PDFs with marked up images
$16.95more info
 
Sign InRegister
Username  
Password   
forgot password?