Systems and method for cooling a staged airblast fuel injector
US-9383097-B2 · Jul 5, 2016 · US
US2016290291A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016290291-A1 |
| Application number | US-201514674709-A |
| Country | US |
| Kind code | A1 |
| Filing date | Mar 31, 2015 |
| Priority date | Mar 31, 2015 |
| Publication date | Oct 6, 2016 |
| Grant date | — |
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A nozzle includes a nozzle body defining a longitudinal axis. The nozzle body has an air passage, a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, and a cooling circuit. The fuel circuit extends from a fuel circuit inlet to a fuel circuit annular outlet. The fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall. At least a portion of the fuel circuit outer wall is radially outboard from the fuel circuit inner wall with respect to the longitudinal axis. A cooling circuit is defined within at least one of the fuel circuit inner wall or the fuel circuit outer wall. The cooling circuit extends from an axial position proximate the fuel circuit inlet to an axial position proximate the fuel circuit outlet.
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What is claimed is: 1 . A nozzle, comprising: a nozzle body defining a longitudinal axis including: an air passage; a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, the fuel circuit extending from a fuel circuit inlet to a fuel circuit annular outlet, wherein the fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall, wherein at least a portion of the fuel circuit outer wall is radially outboard fro…
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