Variable volume combustor with aerodynamic fuel flanges for nozzle mounting
The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles and a fuel injection system for providing a flow of fuel to the micro-mixer fuel nozzles. The fuel injection system may include a number of support struts su...
Saved in:
Main Authors | , , , |
---|---|
Format | Patent |
Language | English |
Published |
20.09.2016
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles and a fuel injection system for providing a flow of fuel to the micro-mixer fuel nozzles. The fuel injection system may include a number of support struts supporting the fuel nozzles and for providing the flow of fuel therethrough. The fuel injection system also may include a number of aerodynamic fuel flanges connecting the micro-mixer fuel nozzles and the support struts. |
---|---|
Bibliography: | Application Number: US201313760094 |