| 摘要 |
PROBLEM TO BE SOLVED: To provide a method to solve a problem regarding an afterburner system for a turbojet in a simple, inexpensive, and effective manner. SOLUTION: A device to feed air and fuel to a burner ring in an afterburner chamber is provided with: a plurality of flame stabilizers radially extending from an outside casing to the surroundings of the axis of the afterburner chamber; a burner ring consisting of a ring sector mounted such that the one end is substantially attached to the other end by a flame stabilizer arm; and a means to feed air and fuel to the burner ring sector. The means is extended between the burner ring and the outside casing of the afterburner chamber situated at the inside of the flame stabilizer arm. COPYRIGHT: (C)2006,JPO&NCIPI
|
