Tiltrotor aircraft with inboard wing mounted fixed engine arrangement
US9376206B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Mar 12, 2013 |
| Grant date | Jun 28, 2016 |
| Priority date | — |
| Expiry date | Jul 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.