The invention discloses a miniature gas
turbine combustion chamber, which has an annular structure and mainly comprises a
flame tube, an outer casing, an inner casing, a swirler and a
fuel oil supply
system. The
flame tube is formed by
welding an outer
flame tube, a head end wall and an inner flame tube; the rear end of the flame tube is connected with a rear
flange of the casing of the
combustion chamber through a screw; the rear end of the outer casing is connected with the rear
flange of the casing through a bolt; and a front
flange of the casing is connected with the front end of the casing through a bolt. An inlet of the
combustion chamber is welded on the front flange of the casing; air radially enters the inlet of the
combustion chamber; the front end of the inner casing is fixed in a hole of the inlet of the
combustion chamber; the swirler is welded on the head end wall; the
fuel oil supply
system is fixed on an outer ring of the inlet of the
combustion chamber; a main combustion hole, a mixing hole and an air film cooling hole are formed on the flame tube; and an air film slot tongue is welded on the lower part of the air film cooling hole for guiding cooling
airflow. A high-energy DC igniter is inserted into the flame tube for realizing ignition starting of the totally annular combustion chamber; and gas is discharged out of the combustion chamber radially under the guiding of a slope of the outer flame tube and a vertical section of the outer flame tube. The miniature gas
turbine combustion chamber is applied to a miniature gas
turbine. Because the gas at the outlet directly impacts a centripetal turbine, the
axial distance of the miniature gas turbine can be shortened, and the space is fully utilized.