ANNULAR COMBUSTION CHAMBER OF A LOWPOWER GAS TURBINE ENGINE,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Pagination or Media Count:
An annular combustion chamber of a low-power gas turbine engine is described which contains a fire tube, a system of fuel supply, and a vaporizing element which has the distinguishing feature that for the purpose of simplifying the design and the operation of the engine the system fuel supply is designed in the form of a single jet located in the body of an antechamber provided with an ignition plug and joined by means of a tube with vaporizing element. A chamber is described which has the distinguishing feature that the vaporizing element is designed in the form of a vaporizing collector located inside of the fire tube.