Patent · US Active

Aircraft propeller drive system

US9745074B2 · kind B2 · utility

0Cited by
15References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 30, 2015
Grant dateAug 29, 2017
Priority date
Expiry dateMar 1, 2036

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16D7/027
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft propeller drive system has a gear to be driven by an engine and having a first plurality of teeth. A torsion bar has a first end driven by the gear and a second end rotatable relative to the first end about a torsion axis by a torsion angle. An output shaft is driven by the second end and is adapted for connection to a propeller. A clutch has a driven member rotationally fixed to the output shaft and a driving member having a second plurality of teeth. The first and second pluralities of teeth engage each other when a variation in the torsion angle from a mean torsion angle is greater than a predetermined angle. Torque is transferred between the gear and the output shaft via the clutch when the first and second pluralities of teeth engage each other.

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