gas turbine combustor design
C47702
concept
Gas turbine combustor design is the engineering process of configuring the combustion chamber’s geometry, fuel–air mixing, cooling, and materials to achieve stable, efficient, low-emission burning of fuel within a gas turbine engine.
Instances (1)
| Instance | Via concept surface |
|---|---|
| TAPS (Twin Annular Pre-mixing Swirler) | — |