Patent · US Active

Method and system for controlling thrust of an engine

US10946972B2 · kind B2 · utility

0Cited by
4References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 21, 2018
Grant dateMar 16, 2021
Priority date
Expiry dateDec 18, 2038

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D31/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Systems and methods for controlling thrust of an engine for an aircraft are described herein. A position of a thrust lever for controlling the engine is obtained from one or more sensors. Air data is obtained from one or more air data inputs. An air temperature data input is detected as compromised from the air data. In response to detecting the air temperature data input is compromised, a target engine rotational speed is determined based on the position of the thrust lever and at least one of altitude data and Mach number data from the air data. A rotational speed of the engine is adjusted to the target engine rotational speed to control thrust of the engine.

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