Patent · US Active

Quiet climb crew interface

US8131410B2 · kind B2 · utility

3Cited by
10References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 15, 2007
Grant dateMar 6, 2012
Priority date—
Expiry dateNov 29, 2029

Classification

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

Abstract

In accordance with an embodiment, a method includes displaying information corresponding to automatically controlled engine thrust levels during a reduced engine thrust period of flight of an aircraft. The information corresponds to one or more parameters associated with a flight control computer of the aircraft. In an alternate aspect, the displayed information includes alphanumeric information formatted in accordance with a sequential order of the automatically controlled engine thrust levels. In a further aspect, the alphanumeric information corresponds to first, second and third engine thrust levels.

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