The turbomachine (1) has a continuous detonation wave engine (6) provided with an annular detonation chamber (7), and a fuel injection system (8) and a priming unit (9) for continuous production of hot gas (F3) from a detonation mixture of fuel and air. A ...

A damping device (122; 222; 322; 422; 522) for damping pressure oscillations within a combustion chamber (106; 206; 306; 406; 506) of a turbine (102; 202; 302; 402; 402; 502) comprises a radially extending damping device body (123; 223; 323; 423; 523), whe...

A turbine containing system (10) is disclosed. The system includes an intake section (14), a compressor section (16) downstream from the intake section (14), a combustor section (20) having a primary combustion system (22) downstream from the intake sectio...