Flow modifier for combustor fuel nozzle tip
US9400104B2 · kind B2 · utility
12Cited by
59References
27Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Sep 28, 2012 |
| Grant date | Jul 26, 2016 |
| Priority date | — |
| Expiry date | Feb 20, 2033 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R2900/00004
- WIPO fieldThermal processes and apparatus
- WIPO sectorMechanical engineering
Abstract
A fuel injector nozzle assembly includes a body extending along an axis and a core swirl plug positioned at least partially within the body. The core swirl plug has a flow modifying structure configured to swirl fuel at a location upstream from a distal end of the nozzle assembly.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.