NAVWEPS 00-80T-80  AIRPLANE PERFORMANCE  112  Figure 2.8. Combustion Chamber and Turbine Components  PRIMARY  COMBUSTION  AIR7  TYPICAL COMBUSTION CHAMBER  SECONDARY Al R  OR COOLING FLOW  FUEL  SPRAY  NOZZLE  DISCHARGE  TO TURBINE  NOZZLES  COMBUsTlON  NUCLEUS  TURBINE SECTION  TUR ’ BINE NOZZLE VANES  r  /  11  TmaiNt  BLADES  TURBINE WHEEL  SHAFT  TURBIhE BLADING  (STATIONARY)  (ROTATING)  TURBINE BLADES 