The combustion chamber burns a mixture of air and fuel inside jet engines, maintaining stable combustion over a wide range of operating conditions while minimizing pressure loss and distributing the heated exhaust gases uniformly to the turbine. Different combustion chamber designs are used depending on requirements, employing features like recirculation zones, cooling air, and multiple fuel injectors to efficiently combust the air-fuel mixture under varying operating conditions.

2. INTRODUCTION

8. COMBUSTION CHAMBERS JET ENGINES EMPLOY VARIOUS TYPES OF COMBUSTION CHAMBERS FOR BURNING OF AIR/FUEL MIXTURE AND GENERATING LARGE AMOUNT OF HEAT DEPENDING UPON DESIGN REQUIREMENTS.

10. COMBUSTION CHAMBERS VARIOUS DESIGN FEATURES ARE INCORPORATED IN THE COMBUSTION CHAMBERS FROM SHAPE, SIZE TO THE MATERIAL AND HEAT TREATMENT SO THAT THEY MEET THEIR REQUIREMENTS.

11. TYPES OF COMBUSTION CHAMBER MULTIPLE OR CAN TYPE

12. TYPES OF COMBUSTION CHAMBERS ANNULAR TYPE

13. TYPES OF COMBUSTION CHAMBER CAN-ANNULAR TYPE