Two-axis thrust vectoring nozzle
US7216476B2 · kind B2 · utility
10Cited by
18References
26Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 9, 2003 |
| Grant date | May 15, 2007 |
| Priority date | — |
| Expiry date | Feb 22, 2024 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2250/42
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A nozzle for a jet engine generally includes a nozzle rim and a bendable duct for communicating an exhaust flow generated by the engine to the nozzle rim. A gimbal joint pivotably couples the nozzle rim to supporting structure. The gimbal joint allows the nozzle rim to be pivoted about a first axis and a second axis, thereby allowing changes to the vector at which the exhaust flow is discharged from the nozzle rim.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.