Combustor nozzle
US7836699B2 · kind B2 · utility
7Cited by
22References
9Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 20, 2005 |
| Grant date | Nov 23, 2010 |
| Priority date | — |
| Expiry date | May 25, 2029 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R2900/00016
- WIPO fieldThermal processes and apparatus
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine swirler/nozzle apparatus has a swirler having a central axis and a nozzle. The nozzle has an outlet end with a plurality of outlets about the central axis and having an asymmetry about the central axis. The apparatus may be formed as a reengineering of a baseline apparatus having a symmetric nozzle.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.