Patent · US Active

Power control for propeller-driven aircraft

US10112722B2 · kind B2 · utility

0Cited by
25References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 11, 2016
Grant dateOct 30, 2018
Priority date
Expiry dateJul 16, 2036

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D43/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A method of controlling an engine for a propeller-driven aircraft, including setting an initial maximum power limit, wherein the initial maximum power limit is associated with a maximum allowable thrust for an aircraft, receiving an indication that a predetermined aircraft condition is satisfied, and setting an updated maximum power limit.

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