Thermally compliant combustion cap device and system
A technology of combustion cover and combustion chamber, which is applied in the direction of combustion chamber, combustion method, combustion equipment, etc., and can solve problems such as high cost, multiple parts, and complexity
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[0040] see figure 1 , a gas turbine assembly constructed in accordance with an exemplary embodiment of the present invention is indicated generally at 10 . Gas turbine 10 includes a compressor assembly 12 , a combustor assembly 14 , a turbine assembly 16 in fluid communication with combustor assembly 14 and compressor assembly 12 , and a rotor shaft 18 attached to compressor assembly 12 and turbine assembly 16 . In operation, air flows through compressor assembly 12 and is discharged into combustor assembly 14 which injects fuel into the airflow and ignites the fuel / air mixture to produce a high temperature combustion airflow. The combustion airflow is discharged toward turbine assembly 16 , which rotates turbine assembly 16 .
[0041] see figure 2 , illustrates an exemplary embodiment of the combustor assembly 14 including a generally circular shroud assembly 38 that provides at least partial support for the plurality of fuel nozzles 22 . The shroud assembly 38 is coupled...
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