The bleed air discharge opening has a covering that is designed as aerodynamic casing element (3) and is elongated, particularly oval or saucer-type and extends in longitudinal direction of a bypass duct (2).A base (10) with convex bending is provided in l...

A pulse detonation system (202) for a turbofan engine (200) including a fan assembly (212) and a turbine sub-system (230), which includes at least one turbine (232), is configured to create a temperature rise and a pressure rise within the turbofan engine ...

A pulse detonation system (12) for a gas turbine engine (10) includes a core engine (30). The pulse detonation system is downstream from the core engine and is configured to create a temperature rise and a pressure rise within the gas turbine engine and to...

A turbofan engine (200) includes a pulse detonation system (202) to create a temperature rise and a pressure rise within the engine to generate thrust from the engine. The system includes a pulse detonation augmentor (240) including a shock tube sub-system...