Aircraft with thrust vectoring propulsion assemblies
US10457390B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Mar 21, 2019 |
| Grant date | Oct 29, 2019 |
| Priority date | — |
| Expiry date | Mar 21, 2039 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/40
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft includes an airframe and a distributed propulsion system including a plurality of propulsion assemblies coupled to the airframe. Each of the propulsion assemblies includes a nacelle, an engine disposed within the nacelle, a proprotor coupled to the engine and a thrust vectoring system. Each thrust vectoring system includes a pivoting plate, a rotary actuator operable to rotate the pivoting plate about a propulsion assembly centerline axis and a linear actuator operable to pivot the pivoting plate about a pivot axis that is normal to the propulsion assembly centerline axis. The engine is mounted on the pivoting plate such that operation of the pivoting plate enables resolution of a thrust vector within a thrust vector cone.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.