System and method for purging a fuel manifold of a gas turbine engine through a flow divider valve
US11732653B2 · kind B2 · utility
0Cited by
23References
8Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 17, 2022 |
| Grant date | Aug 22, 2023 |
| Priority date | — |
| Expiry date | Nov 17, 2042 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
Methods and systems of operating a gas turbine engine in a low-power condition are provided. In one embodiment, the method includes supplying fuel to a combustor by supplying fuel to a first fuel manifold and a second fuel manifold of the gas turbine engine. The method also includes, while supplying fuel to the combustor by supplying fuel to the first fuel manifold: stopping supplying fuel to the second fuel manifold; and supplying pressurized air to the second fuel manifold to flush fuel in the second fuel manifold into the combustor and hinder coking in the second fuel manifold and associated fuel nozzles.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.