Patent · US Active

Method of assisting piloting a hybrid rotorcraft provided with a lift rotor and with at least one propeller propulsive rotor that generates thrust

US11449057B2 · kind B2 · utility

0Cited by
9References
12Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMay 7, 2020
Grant dateSep 20, 2022
Priority date
Expiry dateFeb 10, 2041

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01D2207/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A method of facilitating piloting a hybrid rotorcraft having at least one propulsive rotor provided with a plurality of first blades and a lift rotor provided with a plurality of second blades, the hybrid rotorcraft having a power plant. The method includes a step of displaying on a single indicator a first pointer, the position of which along a movement path varies as a function of a first power from the power plant that is consumed by the propulsive system, and of displaying a second pointer, the position of which varies as a function of a second power of the power plant that is consumed by the lift rotor, a variable space between the first pointer and the second pointer representing a power margin from the power plant that is not used so long as the first pointer is situated between the first end and the second pointer.

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