34results about How to "Safe and reliable ignition" patented technology

The invention relates to an ignition method of a boiling furnace. The method comprises the following steps of: laying hot furnace slag on an air distribution plate; laying bamboo charcoal on the hot furnace slag, and igniting the bamboo charcoal to form a charcoal fire layer; forming a micro negative pressure of minus 10 to 50Pa in a hearth; starting an air blower, so as to enable the charcoal fire layer to slightly jump and not to be buried by the furnace slag; uniformly spreading slack coal on the charcoal fire layer, and gradually increasing air quantity so as to raise the temperature of a material layer; when air output reaches the minimum air speed during normal operation, maintaining the temperature-rise speed of the material layer according to the quantity of the spread slack coal; when the temperature of the material layer reaches 600 to 700 DEG C, increasing the quantity of the slack coal and the air output to enable the air speed to exceed the minimum air speed within 5s; when the temperature of the material layer reaches 750 to 800 DEG C, remaining the addition amount of the slack coal and the air output unchanged so as to steadily raise the temperature; when the temperature of the material layer reaches 800 to 850 DEG C, starting a coal feeder to normally feed coal, remaining the air output unchanged, and adjusting a combustion situation until a flame is stabilized to be golden yellow. According to the ignition method, the ignition time is short and the one-time ignition success rate is high.

The invention discloses a solid-liquid power sounding rocket land launching sequential control system which comprises a main control computer, a ground sequential control system and a rocket-mounted single chip computer control system, wherein the main control computer sends a control command to the ground, sequential control of a rocket-mounted engine igniter is achieved through the ground sequential control system which is further used for conducting the sequential control on a rocket-mounted engine liquid path valve and the rocket-mounted single chip computer control system, and meanwhile opening and closing condition information of the rocket-mounted engine igniter and the liquid path valve is obtained and sent to the main control computer. The sequential control of a rocket-mounted engine pressurized valve is achieved by the rocket-mounted single chip computer control system, and meanwhile the closing and opening condition information of the rocket-mounted engine pressurized valve is obtained and sent to the main control computer through the ground sequential control system. The solid-liquid power sounding rocket land launching sequential control system has the advantages of solving the key problems of matching the solid-liquid power sounding rocket ground sequential control with a rocket-mounted sequential control circuit and meeting millisecond level requirements of launching sequential errors.

The invention relates to an ignition electrode suitable for multiple radiant tube burners. An electrode wire passes through an ignition head and is fixed with the ignition head, an ignition tripod is fixedly arranged at the right end of an electrode tube, and an insulated ceramic tube passes through a circular through hole in the center of the ignition tripod and is positioned and fixed; an electrode catheter is arranged outside the electrode tube, and the right end of the electrode catheter is connected with an electrode mounting hole in a burner combustion chamber; the right end of an electrode mounting joint is connected with a connector, and an electrode head is arranged at the left end of the electrode mounting joint; the left end of the electrode catheter is connected with one horizontal end of a cooling air sleeve of a three-way structure; and the other horizontal end of the cooling air sleeve is connected with the connector, and the cooling air port of the cooling air sleeve in the vertical direction is communicated with a ring seam between the electrode catheter and the electrode tube. The single electrode realizes automatic ignition and flame monitoring functions, and is suitable for multiple radiant tube burners; the ignition electrode wire is insulated and encircled in the whole travel, so that ignition of side walls and surface oxidation of the electrode wire are effectively avoided; and the cooling air effectively reduces the temperatures of the electrode ignition head and the tripod, so that the service life of the electrode is greatly prolonged.

The invention provides a method for preparing nano conductive carbon by cracking an organic compound through a hybrid plasma technology. The method is characterized in that a first cracking reaction zone formed by a direct current arc plasma and a second cracking reaction zone formed by a hybrid plasma consisting of a high-frequency plasma are comprised; and the first cracking reaction zone and the second cracking reaction zone are partitioned by a cylindrical graphite wall surface, the direct current arc plasma is positioned at the inner side of the cylindrical graphite wall surface, and the high-frequency plasma is positioned at the outer side of the cylindrical graphite wall surface. According to the method, the pure nano conductive carbon can be obtained with high efficiency, and valuable combustible gas side products can also be obtained; and meanwhile, the device has good running stability and continuity, and can be used for treating large particle and block solid materials.