| 摘要 |
Combustion chamber consists of the entrance part (4) with the back splay (5) advantageously provided with burner (7), and of transitional part (8) with the burner plane (90), where a system of stabilizing burners (9) is placed, and of vertical part (10) of the advantageously circular section, with burner planes (110, 120) in which first, eventually second, additional burners (11, 12) are placed. The burner (7) in splay (5) of the entrance part (4) is placed in the way that its aperture lies in the burner plane (70), which is parallel with the axis (200) of the rotary combustion furnace (2) and with distance most of half of its diameter (D). Burner planes (110, 120) of the additional burners (11, 12) are situated in the way that the first burner plane (110) is placed in distance from the base (112) of the vertical part (10) of 0.1 to 1.5 of diameter (D) of the rotary combustion furnace (2) and the second burner plane (120) from the first one (110) in distance of 0.5 to 1.5 of diameter (D).
|
