Engine and rotatable proprotor configurations for a tiltrotor aircraft
US11338916B2 · kind B2 · utility
0Cited by
13References
18Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 21, 2018 |
| Grant date | May 24, 2022 |
| Priority date | — |
| Expiry date | Jul 2, 2039 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D35/08
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A tiltrotor aircraft includes a propulsion system with a fixed engine and a rotatable proprotor. The engine is located below the wing of the tiltrotor aircraft, and the rotatable proprotor assembly is mounted on the top surface of the wing. The engine and proprotor assembly are connected via a series of one or more gearboxes that route the engine output from the engine to the proprotor.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.