摘要:
An overfiring air port (100) of the present invention is to supply an incomplete combustion region with air making up for combustion-shortage, in a furnace in which the incomplete combustion region less than stoichiometric ratio is formed by a burner. Furthermore, the airport is characterized by comprising: a nozzle mechanism for injecting air including an axial velocity component of an air flow and a radial velocity component directed to a center line of the air port (100) ; and a control mechanism for controlling a ratio of these velocity components.
摘要:
An overfiring air port (100) of the present invention is to supply an incomplete combustion region with air making up for combustion-shortage, in a furnace in which the incomplete combustion region less than stoichiometric ratio is formed by a burner. Furthermore, the airport is characterized by comprising: a nozzle mechanism for injecting air including an axial velocity component of an air flow and a radial velocity component directed to a center line of the air port (100) ; and a control mechanism for controlling a ratio of these velocity components.
摘要:
The invention relates to a method, a storage medium and a computer system for calculating radiation. Conventionally, a coarse mesh having the same size, i.e., a calculation cell, was used regardless to whether the location is near or remote from radiation elements such as calculation cells and wall face elements. Therefore, it took very long calculation time to calculate an energy exchange between a remote location covered by a coarse mesh and a noted cell. Further, there were many non-influential cells for calculation in a location remote from a noted radiation element for radiation calculation, thus making the calculation accuracy low. The present invention provides a method of calculating radiation comprising a measure for completing the calculation rapidly while keeping the calculation accuracy high. Near at a calculation cell from which radiation energy is emitted or at a calculation cell P into which radiation energy is absorbed, a small (level 0) cell is used, and at a remote location from the calculation cell P, a large (level n) cell formed by combining plural small cells is used. Further, a largest calculation cell which comes into the field of view angle ΔΩ covered by a ray is selected. As a result, the accuracy of the radiation calculation is enhanced, the calculation time is shortened and the amount of memory necessary for the calculation can be reduced.
摘要:
A solid fuel burner using a low oxygen concentration gas as a transporting gas of a low grade solid fuel such as brown coal or the like and a combustion method using the solid fuel burner are provided. The solid fuel burner comprises a means for accelerating ignition of the fuel and a means for preventing slugging caused by combustion ash from occurring. Mixing of fuel and air inside a fuel nozzle (11) is accelerated by that an additional air nozzle (12) and a separator (35) for separating a flow passage are arranged in the fuel nozzle (11), and the exit of the additional air nozzle (12) is set at a position so as to overlap with the separator (35) when seeing from a direction perpendicular to a burner axis, and additional air is ejected in a direction nearly perpendicular to a flow direction of a fuel jet flowing through the fuel nozzle 11. An amount of air from the additional air nozzle (12) is varied corresponding to a combustion load. By increasing the amount of air from the additional air nozzle (12) at a low load operation, an oxygen concentration of a circulation flow (19) formed in a downstream portion outside the exit of the fuel nozzle (11) is increased to stably burn the fuel. By decreasing the amount of air from the additional air nozzle (12) at a high load operation, a flame is formed at a position distant from the fuel nozzle (11) to suppress radiant heat received by structures of the solid fuel burner and walls of the furnace.