Continuous Detonation Wave Combustion Chamber

摘要

Domain: Gas turbine and rocket motor combustion chamber. Object of invention: Low loss fuel-oxidiser efficient combustion in a continuous detonation wave engine, especially in the case of liquid hydrogen and air. Problem 1, Methods of mixing fuel and oxidizing agents for continuous detonation wave combustion chambers do exist, but the method proposed involves a significant restriction of the airflow (oxidizer) and so a loss of performance of the combustion chamber.