Patent · US Active

Supplemental engine power control

US12291326B2 · kind B2 · utility

0Cited by
41References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 14, 2023
Grant dateMay 6, 2025
Priority date
Expiry dateDec 14, 2043

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D31/12
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A rotorcraft has a drive system including a main rotor coupled to a main rotor gearbox to rotate the main rotor at a rotor speed, a main engine coupled to the drive system to provide a first power, a supplemental engine coupled, when a first clutch is engaged, to the drive system to provide a second power additive to the first power, and a control system operable to control the main engine and the supplemental engine to provide a total power demand, where the main engine is controlled based on variations in rotor speed and a power compensation command to produce the first power, and the supplemental engine is controlled to produce the second power in response to a supplemental power demand.

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