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

Automatic load shed control for spacecraft power system

Patent 4575679 Issued on March 11, 1986. Estimated Expiration Date: Icon_subject May 10, 2003. 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

3600599

3617850

3740636

Battery testing apparatus
Patent #: 3971980
Issued on: 07/27/1976
Inventor: Jungfer ,   et al.

Device for controlling the charging and discharging of a storage battery
Patent #: 4194146
Issued on: 03/18/1980
Inventor: Patry ,   et al.

Method of controlling the recharging of storage cells, and monitoring their state of charge
Patent #: 4247812
Issued on: 01/27/1981
Inventor: Patry ,   et al.

Redundant battery protection system
Patent #: 4281278
Issued on: 07/28/1981
Inventor: Bilsky ,   et al.

Method and device for monitoring the state of charge of a storage battery
Patent #: 4307330
Issued on: 12/22/1981
Inventor: Belot

Video preamplifier for laser systems
Patent #: 4376267
Issued on: 03/08/1983
Inventor: Chu ,   et al.

Electrical charging and discharging control apparatus and method, and solar to electrical energy conversion apparatus incorporating such apparatus Patent #: 4383211
Issued on: 05/10/1983
Inventor: Staler

Inventors

Assignee

Application

No. 06/493227 filed on 05/10/1983

US Classes:

324/427, To determine ampere-hour charge capacity307/39, Condition responsive320/136, With battery or cell condition monitoring (e.g., for protection from overcharging, heating, etc.)323/906SOLAR CELL SYSTEMS

Examiners

Primary: Karlsen, Ernest F.
Assistant: O'Shea, Kevin D.

Attorney, Agent or Firm

International Classes

G01R 31/36 (20060101)
H02J 7/00 (20060101)
H02J 7/35 (20060101)
H02J 7/34 (20060101)
H02J 1/14 (20060101)

Abstract

An automatic load shed control for a spacecraft power system employs a selectable one of a plurality of charging gains to approximate a state of charge in a secondary battery system. An ampere hour meter is initialized when the battery system is known to be fully charged and the inefficiencies of the charging system are lumped into a charging gain parameter. An output of the ampere hour meter is compared with a load shed threshold to determine the time for load shedding. The charging gain can be remotely changed as required to a value which causes the output of the ampere hour meter to track the true state of charge of the battery system closely enough for system satisfactory operation of load shedding. The charging gain may be a constant or may be a variable in dependence on the state of charge of the battery system. Charge which is delivered at a rate below a predetermined threshold is ignored by the ampere hour meter.

Other References

  • Hayden, "An Electrical Power System for the Defense Satellite Communications System--Phase III", Proceedings of the 13th Intersociety Energy Conversion Conference, Aug. 1978
  • Kichak, "Standard Power Regulator for the Multi-Mission Modular Spacecraft", American Chemical Society, 1979
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