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

Dynamic, multi-attribute hazard prioritization system for aircraft

Patent 6043757 Issued on March 28, 2000. Estimated Expiration Date: Icon_subject June 12, 2018. 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

3582949

3668403

Multiple parameter monitoring and readout system with sampling of parameters of higher priority than the highest parameter which is out of tolerance
Patent #: 3988730
Issued on: 10/26/1976
Inventor: Valker

Alarm filtering in a ground proximity warning system
Patent #: 4121287
Issued on: 10/17/1978
Inventor: Leal ,   et al.

Alarm device for a vehicle including priority control for plural alarm conditions
Patent #: 4401971
Issued on: 08/30/1983
Inventor: Saito ,   et al.

Adaptive collision threat assessor
Patent #: 4417248
Issued on: 11/22/1983
Inventor: Mathews

Status display system
Patent #: 4635030
Issued on: 01/06/1987
Inventor: Rauch

Device of suppressing incorrect alarms for use in a collision avoidance system installed in an airplane
Patent #: 5029092
Issued on: 07/02/1991
Inventor: Funatsu

Multiple input warning system for a motor vehicle
Patent #: 5241295
Issued on: 08/31/1993
Inventor: Madau

Integrated time/limit exceedance cue system
Patent #: 5339244
Issued on: 08/16/1994
Inventor: Stiles, Jr., et al.

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Inventor

Assignee

Application

No. 096543 filed on 06/12/1998

US Classes:

340/963, Flight alarm340/945, AIRCRAFT ALARM OR INDICATING SYSTEMS701/9, Warning signal or alarm701/14Flight condition indicating system

Examiners

Primary: Swarthout, Brent A.

Attorney, Agent or Firm

International Class

G08B 023/00

Abstract

Signals from warning systems are passed to a hazard prioritization computer. The prioritization computer also receives inputs from the aircraft's air data and inertial reference system. The alert prioritization computer includes three functional modules: (1) hazard detection, identification and monitoring, (2) threat assessment and (3) display and alert prioritization logic. The hazard prioritization computer processes the warning system signals, along with stored data from a hazard database to compute a severity component of threat and a proximity component of threat. These two components are processed to produce an overall threat value for each hazard. This overall threat value is then processed to provide alert and display generation and prioritization for the flight crew and/or the aircraft's auto-flight system.

Other References

  • "Smart Alerting", compiled by Paul Proctor, Aviation Week & Space Technology, Feb. 24, 1997, p. 1
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