Hydrogen combustion treating system

• Main Authors: GAO YANFENG, ZHANG JIE, WANG LI, CAO LING, YU HUIJIE, HUANG LINGYAN, LYU YAN, HE YI, HE JIANHUA, TIAN QINGYA
• Format: Patent
• Language: English
• Published: 13.01.2016
• Subjects: AIR; BLASTING; COMBUSTION APPARATUS; COMBUSTION PROCESSES; EXTINGUISHING-DEVICES; HEATING; IGNITION; LIGHTING; MECHANICAL ENGINEERING; METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN; WEAPONS

The invention relates to a hydrogen combustion treating system used for treating low-temperature hydrogen at a launching site of a carrier rocket. The hydrogen combustion treating system comprises a first igniting system and a plurality of first electric igniting pins. The first igniting system comprises a first igniting control cabinet and a first high voltage generator. The first igniting control cabinet is used for supplying power to the first high voltage generator. The first high voltage generator is used for generating and transferring high voltage to the two ends of an electrode of each first electric igniting pin. The hydrogen combustion treating system further comprises a combustion cell, a plurality of bubble caps, a hydrogen discharge pipeline and a low-temperature check valve. The combustion cell is filled with water. The multiple bulb caps are all arranged inside the combustion cell, and the lower ends of the multiple bulb caps are all immersed in the water. The multiple first electric igniting pins are uniformly distributed on the inner wall of the combustion cell. A hydrogen inlet is formed in the side wall of the combustion cell. One end of the hydrogen discharge pipeline penetrates through the hydrogen inlet and is communicated with the multiple bulb caps. The low-temperature check valve is arranged on the hydrogen discharge pipeline and located outside the combustion cell.