Patent · US Active

Power demand anticipation systems for rotorcraft

US10287026B2 · kind B2 · utility

4Cited by
11References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 4, 2017
Grant dateMay 14, 2019
Priority date
Expiry dateAug 5, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/313
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A power demand anticipation system for a rotorcraft includes an engine subsystem having an engine with a power output. The power demand anticipation system also includes one or more sensors including a cyclic control sensor. The one or more sensors are operable to detect one or more flight parameters of the rotorcraft to form sensor data including a cyclic control position. A power demand anticipation module is in data communication with the engine subsystem and the one or more sensors. The power demand anticipation module is operable to anticipate a power demand of the engine using the sensor data to form a power demand anticipation signal. The engine subsystem is operable to adjust the power output of the engine based on the power demand anticipation signal received from the power demand anticipation module.

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