Deflagration To Detonation Supersonic Igniter
Patent No: 201941026005
Dr. Aldin Justin Sundararaj, Assistant Professor, Aerospace Engineering
Ms. Vinitha M Samuel PR16AE002, M.Tech batch 2016-18
In deflagration to detonation supersonic igniter the fuel and oxidizer is ignited with a conventional spark plug. The flame thus developed is made to travel through a Shchelkin spiral placed inside the tube. The spiral acted as a blockage and the subsonic flame gets converted to detonation wave. A introduction of secondary source of fuel in the detonating tube results in an effective enhancement of ignition in detonation engines. The supersonic igniter can be used to initiate supersonic /detonating wave in high enthalpy engines like Pulse Detonation Engines (PDE), Continuous Rotating Detonation Engines (CRDE).