Ramjet engine equipped with a plurality of carburated air supply nozzles and a missile equipped with such a ramjet engine

摘要

A ramjet engine of the type including a combustion chamber into which n air ducts open, each air duct being equipped with a fuel injector device. A total fuel flow quantity D is introduced into the combustion chamber so that a relationship D/n would generally be provided for individual fuel flow by a respective injector device. A distributor is provided which regulates the individual fuel flow of at least one of the injector devices to be at a value different from the D/n relationship.