Patent · US Active

Tiltrotor aircraft with inboard wing mounted fixed engine arrangement

US9376206B2 · kind B2 · utility

28Cited by
26References
25Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 12, 2013
Grant dateJun 28, 2016
Priority date
Expiry dateJul 12, 2033

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D35/04
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A rotor system for tilt rotor aircraft comprises an engine disposed at a first fixed position on a wing member, and a prop-rotor pylon mechanically coupled to the engine along a drive path extending through the wing member. The engine is disposed adjacent a fuselage of the tilt rotor aircraft, and the prop-rotor pylon is configured to selectively rotate between a vertical position and a horizontal position. The prop-rotor pylon is coupled to a plurality of rotor blades.

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