为有效解决青龙煤矿21602工作面采煤期间上隅角瓦斯浓度超限问题,利用定向钻进技术的轨迹可控、覆盖区域广等优势,在21602工作面布置高位定向长钻孔抽采采动卸压瓦斯。介绍了高位定向长钻孔瓦斯抽采技术原理,分析了钻孔布置层位及设计方...为有效解决青龙煤矿21602工作面采煤期间上隅角瓦斯浓度超限问题,利用定向钻进技术的轨迹可控、覆盖区域广等优势,在21602工作面布置高位定向长钻孔抽采采动卸压瓦斯。介绍了高位定向长钻孔瓦斯抽采技术原理,分析了钻孔布置层位及设计方案,通过现场实践确定了21602工作面高位定向长钻孔优先布置在顶板距离煤层16~28 m区域。实践表明,21602工作面采煤期间上隅角瓦斯浓度由抽采前的最高值0.72%降低到抽采期间的0.20%~0.40%,单孔抽采瓦斯纯流量达1.58 m 3/min,有效保证了工作面的高效安全回采,可为近距离煤层群上隅角瓦斯治理提供经验。展开更多
This study is aimed at using blade 3-D optimization to control corner flows in the high through-flow fan/booster of a high bypass ratio commercial turbofan engine. Two kinds of blade 3-D optimization, end-bending and ...This study is aimed at using blade 3-D optimization to control corner flows in the high through-flow fan/booster of a high bypass ratio commercial turbofan engine. Two kinds of blade 3-D optimization, end-bending and bow, are focused on. On account of the respective operation mode and environment, the approach to 3-D aerodynamic modeling of rotor blades is different from stator vanes. Based on the understanding of the mechanism of the corner flow and the consideration of intensity problem for rotors, this paper uses a variety of blade 3-D optimization approaches, such as loading distribution optimization, perturbation of departure angles and stacking-axis manipulation, which are suitable for rotors and stators respectively. The obtained 3-D blades and vanes can improve the corner flow features by end-bending and bow effects. The results of this study show that flows in corners of the fan/booster, such as the fan hub region, the tip and hub of the vanes of the booster, are very complex and dominated by 3-D effects. The secondary flows there are found to have a strong detrimental effect on the compressor performance. The effects of both end-bending and bow can improve the flow separation in corners, but the specific ways they work and application scope are somewhat different. Redesigning the blades via blade 3-D optimization to control the corner flow has effectively reduced the loss generation and improved the stall margin by a large amount.展开更多
文摘为有效解决青龙煤矿21602工作面采煤期间上隅角瓦斯浓度超限问题,利用定向钻进技术的轨迹可控、覆盖区域广等优势,在21602工作面布置高位定向长钻孔抽采采动卸压瓦斯。介绍了高位定向长钻孔瓦斯抽采技术原理,分析了钻孔布置层位及设计方案,通过现场实践确定了21602工作面高位定向长钻孔优先布置在顶板距离煤层16~28 m区域。实践表明,21602工作面采煤期间上隅角瓦斯浓度由抽采前的最高值0.72%降低到抽采期间的0.20%~0.40%,单孔抽采瓦斯纯流量达1.58 m 3/min,有效保证了工作面的高效安全回采,可为近距离煤层群上隅角瓦斯治理提供经验。
基金supported by National Natural Science Foundation of China (51006005,50736007)"Fan-Zhou" Youth Foundation(20100401)
文摘This study is aimed at using blade 3-D optimization to control corner flows in the high through-flow fan/booster of a high bypass ratio commercial turbofan engine. Two kinds of blade 3-D optimization, end-bending and bow, are focused on. On account of the respective operation mode and environment, the approach to 3-D aerodynamic modeling of rotor blades is different from stator vanes. Based on the understanding of the mechanism of the corner flow and the consideration of intensity problem for rotors, this paper uses a variety of blade 3-D optimization approaches, such as loading distribution optimization, perturbation of departure angles and stacking-axis manipulation, which are suitable for rotors and stators respectively. The obtained 3-D blades and vanes can improve the corner flow features by end-bending and bow effects. The results of this study show that flows in corners of the fan/booster, such as the fan hub region, the tip and hub of the vanes of the booster, are very complex and dominated by 3-D effects. The secondary flows there are found to have a strong detrimental effect on the compressor performance. The effects of both end-bending and bow can improve the flow separation in corners, but the specific ways they work and application scope are somewhat different. Redesigning the blades via blade 3-D optimization to control the corner flow has effectively reduced the loss generation and improved the stall margin by a large amount.
