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

Computer imaging system and method for remote in-flight aircraft refueling

Patent 5530650 Issued on June 25, 1996. Estimated Expiration Date: Icon_subject November 21, 2014. 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

3910533

Real-time simulation of point system having multidirectional points as viewed by a moving observer
Patent #: 4027403
Issued on: 06/07/1977
Inventor: Marsh ,   et al.

Remote refueling station
Patent #: 4298176
Issued on: 11/03/1981
Inventor: Kendall

Satellite servicing
Patent #: 4349837
Issued on: 09/14/1982
Inventor: Hinds

Apparatus for remotely indicating alignment of male and female members
Patent #: 4395005
Issued on: 07/26/1983
Inventor: Ganssle

Aerial day/night refueling stations
Patent #: 4398685
Issued on: 08/16/1983
Inventor: Task ,   et al.

Ship-to-ship fluid transfer system
Patent #: 4408943
Issued on: 10/11/1983
Inventor: McTamaney ,   et al.

Terrain advisory system
Patent #: 4646244
Issued on: 02/24/1987
Inventor: Bateman ,   et al.

Docking alignment system
Patent #: 4890918
Issued on: 01/02/1990
Inventor: Monford

Real-time flight and destination display for aircraft passengers
Patent #: 4975696
Issued on: 12/04/1990
Inventor: Salter, Jr., et al.

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Inventors

Assignee

Application

No. 344412 filed on 11/21/1994

US Classes:

701/300, RELATIVE LOCATION244/135A, Aircraft refueling340/958, Docking guidance348/117Aircraft or spacecraft

Examiners

Primary: Teska, Kevin J.
Assistant: Walker, Tyrone V.

International Class

B64D 039/00

Abstract

A visual guidance system and method includes a subsystem which both locates the aircraft and mating structures thereof and also determines their motion and their rate of change of motion. The locating subsystem has an electrical output which feeds the location and motion data to a guidance system computer which utilizes software which combines the data with other data in a database containing the dimensional size and configuration of the aircraft and mating structures. The combined data is converted to a suitable form and fed to the computer monitor which displays the aircraft and mating structures thereof in real time during the refueling operation. The computer and computer monitor are provided with image controls which allow the operator to select the perspective viewing angle as well as the image contrast and color in order to enhance the visual cues provided by the image and facilitate the refueling operation.

Other References

  • NASA Tech Briefs, Official Publication of NASA, Mar. 1991, pp. 26, etc
  • McDonnell Douglas publication, author, date and pages unknow
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