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HYDROGEN ENRICHED COMBUSTION TESTING OF SIEMENS SGT-400 AT HIGH PRESSURE CONDITIONS

机译:西门子SGT-400高压条件下的富氢燃烧测试

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Following successful testing of the SGT-400 combustion system at atmospheric conditions with hydrogen enriched natural gas, a high pressure combustion test campaign was carried out at the Siemens test facility in Lincoln UK. Combustion performance at full engine operating conditions was studied, with the aim of demonstrating the capability of the standard SGT-400 combustion hardware to fire fuels with increased hydrogen content. Measurements consisted of: a pilot tip thermocouple to monitor the risk of flashback; pressure sensors to capture the combustion dynamics signature; and emissions instrumentation measuring NO_x and CO. The combustor was also instrumented with thermocouples to monitor both the distribution of wall temperatures and potential locations of flashback when utilizing the highly reactive hydrogen enriched gas. The current paper reports the findings of the high pressure tests and compares with the atmospheric results that had been documented previously. Combustion behavior at full engine pressure and temperature was found to be consistent with atmospheric conditions. Pilot tip temperature increased with the hydrogen gas content due to the higher flame speed. Combustion dynamics shifted to a higher frequency for the hydrogen enriched gas, and heat release fluctuations increased. NO_x emission also increased with the hydrogen blending due to the enhanced fuel reactivity. The high pressure tests demonstrated that the SGT-400 standard DLE combustion system can operate without risk of flashback for up to 20% vol hydrogen content. The next phase of the hydrogen program is to test a production engine using enriched gas and confirm its full operational characteristics. Extending the operational envelope of the standard DLE combustion system to hydrogen contents above 20% vol is also of interest.
机译:在大气压下使用富氢天然气成功测试了SGT-400燃烧系统之后,在英国林肯的西门子测试设施进行了高压燃烧测试。研究了在全发动机工况下的燃烧性能,目的是证明标准SGT-400燃烧硬件燃烧含氢量更高的燃料的能力。测量包括:引燃尖端热电偶,用于监控回火的风险;压力传感器捕获燃烧动力学特征;燃烧室还装有热电偶,以在利用高反应性富氢气体时监测壁温的分布和回火的潜在位置。本论文报告了高压测试的结果,并与先前记录的大气结果进行了比较。发现在全发动机压力和温度下的燃烧行为与大气条件一致。由于较高的火焰速度,飞行员的尖端温度随氢气含量的升高而升高。富氢气体的燃烧动力学转移到更高的频率,并且放热波动增加。由于增强的燃料反应性,NO_x排放也随着氢混合而增加。高压测试表明,SGT-400标准DLE燃烧系统可以在最高20%的体积氢含量无闪回风险的情况下运行。氢计划的下一阶段是测试使用富气的生产发动机,并确认其全部运行特性。将标准DLE燃烧系统的运行范围扩展到氢含量超过20%vol也是令人感兴趣的。

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