Patent · US Expired

Method and system for autoflight information display

US6745113B2 · kind B2 · utility

62Cited by
12References
90Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 7, 2002
Grant dateJun 1, 2004
Priority date
Expiry dateJun 12, 2022

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01D7/04
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

A method and system for autoflight information display. A method in accordance with one embodiment of the invention includes determining if an automatic aircraft controller is controlling an aircraft function based at least in part on a target aircraft speed. If so, the method further includes displaying alphanumeric information corresponding to the operation of the automatic aircraft controller at a first location of a display medium. If not, the method further includes displaying the alphanumeric information at a second location of the display medium different than the first location. The first location can be aligned with a display of the aircraft speed, and the second location can be aligned with a display of the aircraft altitude. In another embodiment of the invention, engine control information can be integrated with a display of aircraft autopilot and/or autothrottle information.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.