Patent · US Active

Methods and systems for controlling thrust produced by a plurality of engines on an aircraft for assisting with certain flight conditions

US10759544B2 · kind B2 · utility

1Cited by
0References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 6, 2018
Grant dateSep 1, 2020
Priority date
Expiry dateJul 14, 2038

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/50
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

In an example, method of controlling thrust produced by a plurality of engines on an aircraft for assisting with nose-down recovery of the aircraft is described. The method includes selecting a maximum value of an aircraft parameter, measuring a value of the aircraft parameter while the aircraft is in flight, based on a comparison of the maximum value and the measured value determining that the measured value exceeds the maximum value, and reducing a thrust produced by each of the engines of the plurality of engines to bring the measured value of the aircraft parameter below the maximum value of the aircraft parameter.

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