Engine and rotatable proprotor configurations for a tiltrotor aircraft
US11148798B2 · kind B2 · utility
2Cited by
55References
15Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 22, 2018 |
| Grant date | Oct 19, 2021 |
| Priority date | — |
| Expiry date | Sep 29, 2039 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D35/00
- 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 on the top surface of the wing of the tiltrotor aircraft, and the rotatable proprotor assembly is also 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.