Nozzle for jet engines
US10378477B2 · kind B2 · utility
2Cited by
19References
14Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Feb 26, 2016 |
| Grant date | Aug 13, 2019 |
| Priority date | — |
| Expiry date | Feb 28, 2038 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2240/128
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
An exhaust system or nozzle for use in a gas turbine engine is disclosed herein. The exhaust system is adapted to adjust various streams of pressurized air produced by the gas turbine engine to control operation of the gas turbine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.