Patent · US Active

Rotorcraft engine and rotor speed synchronization

US7866598B2 · kind B2 · utility

39Cited by
20References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 6, 2009
Grant dateJan 11, 2011
Priority date
Expiry dateMar 6, 2029

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T74/19242
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Systems and methods are provided in which an electrical control system independently effects acceleration of both driven and driving elements of a clutch to engage each other. In preferred embodiments the clutch is not a friction clutch, but a dog clutch, and forms part of a drive drain of a rotorcraft. A second clutch can be used, along with a mechanical interlock to prevent simultaneous engagement of the clutches. Speeds of the driven and driving elements can be sensed, and altered using at least one of a rotor, a brake, a generator, an electric motor, and a combustion motor. In rotorcraft embodiments, the gearbox can have a neutral condition in which no power is transmitted from the engine to the rotor

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