燃气发生器应用综述
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摘要
燃气发生器是适用于航空航天、舰船、石油及汽车工业等领域的燃气生成装置,具有应用范围广、种类多等特点,受到了各行各业的关注。通过对国内外的大量文献进行分类总结,分析了燃气发生器的应用研究领域。根据其工作原理进行了分类,系统阐述了各类燃气发生器的工作特点及研究进展,对各类燃气发生器在应用过程中存在的技术难点和发展前景进行了简要分析。认为研制高效、稳定、可靠的燃气发生器是各行各业发展的重点,相关研究结果可为燃气发生器的选型及研制提供参考。
Gas generator is applied to aerospace,ships and warships,petroleum industry,automobile industry and other fields as a device for producing combustion-gas. It arouses general concern of every industry or trade for its widespread use and various types. In this paper,literature was classified and summarized from a lot of published references at home and abroad and applications of gas generator were viewed briefly. The gas-generators were classified on the basis of its working principle. Furthermore,working characteristics and research progress of various gas generators were described systematically. The technical difficulties encountered in the process of application and development prospect of gas generator were also analyzed. It is concluded that the development of efficient,stable and reliable gas generator is a key point of development in various fields. The research results provide references for the selection and development of gas generator.
Gas generator is applied to aerospace,ships and warships,petroleum industry,automobile industry and other fields as a device for producing combustion-gas. It arouses general concern of every industry or trade for its widespread use and various types. In this paper,literature was classified and summarized from a lot of published references at home and abroad and applications of gas generator were viewed briefly. The gas-generators were classified on the basis of its working principle. Furthermore,working characteristics and research progress of various gas generators were described systematically. The technical difficulties encountered in the process of application and development prospect of gas generator were also analyzed. It is concluded that the development of efficient,stable and reliable gas generator is a key point of development in various fields. The research results provide references for the selection and development of gas generator.
引文
[1]康忠涛,李清廉,张新桥.基于V型槽的空气/煤油燃气发生器火焰稳定方法研究[J].推进技术,2013,34(9):1231-1239.
[2]钟战.燃气发生器点火与燃烧性能研究[D].长沙:国防科学技术大学,2008.
[3]李刚,危懿,褚卫华.燃气发生器空气压力控制策略研究与实现[C]//中国空气动力学会测控专业委员会第六届六次全国学术交流会论文集.惠州:中国空气动力学会测控专业委员会,2015.
[4]张新宇,陈立红,顾洪斌,等.超燃冲压模型发动机实验设备与实验技术[J].力学进展,2003,33(4):491-498.
[5]SARISIN M N. Design of Connected Pipe Test Facility for Ramjet Applications[Z]. METU Mechanical Eng Dept Master Thesis,2005.
[6]刘友朋.低总温空气加热器数值仿真与试验研究[D].长沙:国防科学技术大学,2010.
[7]冯军红.高焓高压空气加热器数值仿真与试验研究[D].长沙:国防科学技术大学,2011.
[8]赵芳.低总温直连式空气加热器数值仿真与试验研究[D].长沙:国防科学技术大学,2012.
[9]李卫强,宋文艳.水组分对高超声速冲压发动机性能的影响[J].空军工程大学学报(自然科学版),2006,7(5):10-12.
[10]LE J L,LIU W X,SONG W Y,et al. Experimental and numerical investigation of air vitiation effects on scramjet test performance:AIAA-2009-7344[R]. Bremen:AIAA,2009.
[11]VYAS M A,ENGBLIM W A,GEORGIADIS N J,et al.Numerical simulation of vitiation effects on a hydrogen-fueled dual-mode scramjet:AIAA-2010-1127[R]. Orlando:AIAA,2010.
[12]陈亮,宋文艳,李建平.实验气体污染对超音速燃烧性能影响的数值模拟研究[J].弹箭与制导学报,2011,31(3):142-146.
[13]张新桥,李清廉,康忠涛.空气/煤油/水燃气发生器点火特性试验[J].国防科技大学学报,2013,35(4):35-40.
[14]贺武生.超燃冲压发动机研究综述[J].火箭推进,2005,31(1):29-32.HE W S. Review of scramjet engine development[J].Journal of Rocket Propulsion,2005,31(1):29-32.
[15]VAUGH N,DUST Y,GARRA R D,et al. Transitioning to fly the mission:AIAA-2010-1714[R]. Nashville:AIAA,2010.
[16]金鹏.舰船燃气轮机机匣处理数值模拟研究[D].哈尔滨:哈尔滨工程大学,2013.
[17]翁一武,闻雪友,翁史烈.燃气轮机技术及发展[J].自然杂志,2017,39(1):43-47.
[18]蒋红梅.燃气轮机主要构件可靠性分析[D].哈尔滨:哈尔滨工程大学,2008.
[19]CONNAUGHTON J C. Application of a hydrazine gas generator to vacuum ejector pumping of a chemical laser:AIAA-1977-0892[R]. Orlando:AIAA,1977.
[20]徐万武.高性能、大压缩比化学激光器压力恢复系统研究[D].长沙:国防科学技术大学,2003.
[21]罗智锋.一种以乙醇为燃料的环形燃烧室燃气发生器:201310683250. 5[P]. 2014-04-02.
[22]罗智锋,冯大强,屈成泽,等.一种以乙醇为燃料的单管燃烧室燃气发生器:CN204534569U[P]. 2015-08-05.
[23]李春红,张小平,马冬英,等.液氧/甲烷燃气发生器点火方案研究[J].火箭推进,2010,36(5):7-12.LI C H,ZHANG X P,MA D Y,et al. Ignition scheme of LOX/methane gas generator[J]. Journal of Rocket Propulsion,2010,36(5):7-12.
[24]刘盛田,胡兴伟,柳琪,等.一氧化二氮/乙醇燃气发生器试验研究[J].舰船科学技术,2008,30(S2):223-226.
[25]金盛宇,许宏博,吉林.空气/煤油燃气发生器技术研究[J].火箭推进,2014,40(3):29-32.JIN S Y,XU H B,JI L. Technology research on air/jet fuel gas generator[J]. Journal of Rocket Propulsion,2014,40(3):29-32.
[26]严成忠.“昆仑”发动机的衍生发展[J].航空发动机,2009,35(1):11-17.
[27]钟志华,杨济匡.汽车安全气囊技术及其应用[J].中国机械工程,2012,11(S1):234-237.
[28]姚俊,罗运强,牛振宇,等.气体发生器低温点火稳定性研究[J].当代化工,2013,42(4):452-455.
[29]NAKAYASU M I,NOMA N I. Gas generator for restraining device for vehicle:US20070927503[P]. 2009-09-22.
[30]KOBAYASHI T,MATSUDA N. Gas generator for re-straining device of vehicle:WO2010JP50659[P]. 2010-07-22.
[31]岳通通,刘丹,何步金.一种安全气囊气体发生器:CN203391723U[P]. 2014-01-15.
[32]刘亮,罗运强,张文龙,等.安全气囊点火药点火性能的研究[J].当代化工,2013,42(10):1398-1400.
[33]王卫国.汽车安全带预紧器用气体发生器的研究[D].南京:南京理工大学,2004.
[34]余义.预紧式安全带防护效率研究[D].武汉:武汉理工大学,2012.
[35]牛振宇,王小强,付文斌.燃气发生器在无人机上的应用[J].飞航导弹,2015(5):89-92.
[36]都军民,张宇.发射动力系统主装药温度变化规律研究[J].火工品,2008(3):1-3.
[37]赵世平,鲍福廷.燃气蒸汽式发射系统内弹道若干问题研究[J].固体火箭技术,2003,26(3):7-10.
[38]芮守祯,邢玉明.导弹发射动力系统发展研究[J].战术导弹技术,2003(5):4-9.
[39]孔令海.海洋平台燃气透平电站的选型设计[J].中国海上油气(工程),2001,13(4):48-51.
[40]BOWN N,DARLEY M. Advanced airbag landing systems for planetary landers[C]//18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.Reston,Virigina:American Institute of Aeronautics and Astronautics,2005.
[41]张丽梅,郝芳.火星气囊气体发生器充气过程稳压仿真研究[J].航天返回与遥感,2012,33(6):30-38.
[42]邵志建.次生气囊在无人机回收系统中的应用[J].南京航空航天大学学报,2009,41(S1):93-96.
[43]卢福刚.自由装填装药固体火箭发动机点火冲击研究[J].弹箭与制导学报,2015,35(6):83-86.
[44]JEON K S,LEE J W,LEE C,et al. Optimal gas generator design for the liquid rocket engine:AIAA-2004-0032[R]. Reno:AIAA,2004.
[45]郑大生,王菊金,胡长喜.液体发动机变推力的研究和实现[C]//航天动力技术发展与应用学术会议论文集.沈阳:中国航天第三专业信息网第二十七届年会,2006.
[46]刘朋,张平,周源泉.某燃气发生器壳体的结构可靠性分析与评估[J].推进技术,2001,22(5):411-414.
[47]闫璞,王敏庆,盛美萍.燃烧腔不稳定燃烧的有限元数值分析[J].噪声与振动控制,2005,25(5):21-23,28.
[48]FOURNET A,LONCHARD J M,THOMAS J L. Technological demonstration for low cost gas generator:AIAA-2004-4006[R]. Fort Lauderdale:AIAA,2004.
[49]NGUYEN H. Flow/thermal analysis of X-34 orbital stage gas generator design:AIAA-1996-3226[R]. Lake Buena Vista:AIAA,1996.
[50]聂万胜,庄逢辰.喷雾特性对液体火箭发动机燃烧稳定性的影响[J].推进技术,2000,21(3):56-59.
[51]苗淼,王文杰.某燃气发生器地面台架试车性能分析[J].航空动力学报,2006,21(1):41-44.
[52]KIM J,HONG S S,JEONG E H,et al. Development of a turbo pump for a 30 ton class engine:AIAA-2007-5516[R]. Cincinnati:AIAA,2007.
[53]DENNIS H J,SANDERS T. NASA fastrac engine gas generator component test program and results:AIAA-2000-3401[R]. Las Vegas:AIAA,2000.
[54]MAH C S. Evaluating the operational limits of a gas generator:AIAA-2001-3990[R]. Salt Lake City:AIAA,2001.
[55]肖锋.过氧化氢自燃点火器的试验研究[D].长沙:国防科学技术大学,2005.
[56]陈建华,李龙飞,周立新,等.液氧/煤油补燃火箭发动机整流栅应用研究[J].火箭推进,2007,33(2):1-6.CHEN J H,LI L F,ZHOU L X,et al. Application of the perforated distribution plate in the LOX/kerosene staged combustion rocket engine[J]. Journal of Rocket Propulsion,2007,33(2):1-6.
[57]童晓艳,蔡国飙,尘军,等.燃气发生器身部多学科设计优化[J].北京航空航天大学学报,2006,32(10):1250-1254
[2]钟战.燃气发生器点火与燃烧性能研究[D].长沙:国防科学技术大学,2008.
[3]李刚,危懿,褚卫华.燃气发生器空气压力控制策略研究与实现[C]//中国空气动力学会测控专业委员会第六届六次全国学术交流会论文集.惠州:中国空气动力学会测控专业委员会,2015.
[4]张新宇,陈立红,顾洪斌,等.超燃冲压模型发动机实验设备与实验技术[J].力学进展,2003,33(4):491-498.
[5]SARISIN M N. Design of Connected Pipe Test Facility for Ramjet Applications[Z]. METU Mechanical Eng Dept Master Thesis,2005.
[6]刘友朋.低总温空气加热器数值仿真与试验研究[D].长沙:国防科学技术大学,2010.
[7]冯军红.高焓高压空气加热器数值仿真与试验研究[D].长沙:国防科学技术大学,2011.
[8]赵芳.低总温直连式空气加热器数值仿真与试验研究[D].长沙:国防科学技术大学,2012.
[9]李卫强,宋文艳.水组分对高超声速冲压发动机性能的影响[J].空军工程大学学报(自然科学版),2006,7(5):10-12.
[10]LE J L,LIU W X,SONG W Y,et al. Experimental and numerical investigation of air vitiation effects on scramjet test performance:AIAA-2009-7344[R]. Bremen:AIAA,2009.
[11]VYAS M A,ENGBLIM W A,GEORGIADIS N J,et al.Numerical simulation of vitiation effects on a hydrogen-fueled dual-mode scramjet:AIAA-2010-1127[R]. Orlando:AIAA,2010.
[12]陈亮,宋文艳,李建平.实验气体污染对超音速燃烧性能影响的数值模拟研究[J].弹箭与制导学报,2011,31(3):142-146.
[13]张新桥,李清廉,康忠涛.空气/煤油/水燃气发生器点火特性试验[J].国防科技大学学报,2013,35(4):35-40.
[14]贺武生.超燃冲压发动机研究综述[J].火箭推进,2005,31(1):29-32.HE W S. Review of scramjet engine development[J].Journal of Rocket Propulsion,2005,31(1):29-32.
[15]VAUGH N,DUST Y,GARRA R D,et al. Transitioning to fly the mission:AIAA-2010-1714[R]. Nashville:AIAA,2010.
[16]金鹏.舰船燃气轮机机匣处理数值模拟研究[D].哈尔滨:哈尔滨工程大学,2013.
[17]翁一武,闻雪友,翁史烈.燃气轮机技术及发展[J].自然杂志,2017,39(1):43-47.
[18]蒋红梅.燃气轮机主要构件可靠性分析[D].哈尔滨:哈尔滨工程大学,2008.
[19]CONNAUGHTON J C. Application of a hydrazine gas generator to vacuum ejector pumping of a chemical laser:AIAA-1977-0892[R]. Orlando:AIAA,1977.
[20]徐万武.高性能、大压缩比化学激光器压力恢复系统研究[D].长沙:国防科学技术大学,2003.
[21]罗智锋.一种以乙醇为燃料的环形燃烧室燃气发生器:201310683250. 5[P]. 2014-04-02.
[22]罗智锋,冯大强,屈成泽,等.一种以乙醇为燃料的单管燃烧室燃气发生器:CN204534569U[P]. 2015-08-05.
[23]李春红,张小平,马冬英,等.液氧/甲烷燃气发生器点火方案研究[J].火箭推进,2010,36(5):7-12.LI C H,ZHANG X P,MA D Y,et al. Ignition scheme of LOX/methane gas generator[J]. Journal of Rocket Propulsion,2010,36(5):7-12.
[24]刘盛田,胡兴伟,柳琪,等.一氧化二氮/乙醇燃气发生器试验研究[J].舰船科学技术,2008,30(S2):223-226.
[25]金盛宇,许宏博,吉林.空气/煤油燃气发生器技术研究[J].火箭推进,2014,40(3):29-32.JIN S Y,XU H B,JI L. Technology research on air/jet fuel gas generator[J]. Journal of Rocket Propulsion,2014,40(3):29-32.
[26]严成忠.“昆仑”发动机的衍生发展[J].航空发动机,2009,35(1):11-17.
[27]钟志华,杨济匡.汽车安全气囊技术及其应用[J].中国机械工程,2012,11(S1):234-237.
[28]姚俊,罗运强,牛振宇,等.气体发生器低温点火稳定性研究[J].当代化工,2013,42(4):452-455.
[29]NAKAYASU M I,NOMA N I. Gas generator for restraining device for vehicle:US20070927503[P]. 2009-09-22.
[30]KOBAYASHI T,MATSUDA N. Gas generator for re-straining device of vehicle:WO2010JP50659[P]. 2010-07-22.
[31]岳通通,刘丹,何步金.一种安全气囊气体发生器:CN203391723U[P]. 2014-01-15.
[32]刘亮,罗运强,张文龙,等.安全气囊点火药点火性能的研究[J].当代化工,2013,42(10):1398-1400.
[33]王卫国.汽车安全带预紧器用气体发生器的研究[D].南京:南京理工大学,2004.
[34]余义.预紧式安全带防护效率研究[D].武汉:武汉理工大学,2012.
[35]牛振宇,王小强,付文斌.燃气发生器在无人机上的应用[J].飞航导弹,2015(5):89-92.
[36]都军民,张宇.发射动力系统主装药温度变化规律研究[J].火工品,2008(3):1-3.
[37]赵世平,鲍福廷.燃气蒸汽式发射系统内弹道若干问题研究[J].固体火箭技术,2003,26(3):7-10.
[38]芮守祯,邢玉明.导弹发射动力系统发展研究[J].战术导弹技术,2003(5):4-9.
[39]孔令海.海洋平台燃气透平电站的选型设计[J].中国海上油气(工程),2001,13(4):48-51.
[40]BOWN N,DARLEY M. Advanced airbag landing systems for planetary landers[C]//18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.Reston,Virigina:American Institute of Aeronautics and Astronautics,2005.
[41]张丽梅,郝芳.火星气囊气体发生器充气过程稳压仿真研究[J].航天返回与遥感,2012,33(6):30-38.
[42]邵志建.次生气囊在无人机回收系统中的应用[J].南京航空航天大学学报,2009,41(S1):93-96.
[43]卢福刚.自由装填装药固体火箭发动机点火冲击研究[J].弹箭与制导学报,2015,35(6):83-86.
[44]JEON K S,LEE J W,LEE C,et al. Optimal gas generator design for the liquid rocket engine:AIAA-2004-0032[R]. Reno:AIAA,2004.
[45]郑大生,王菊金,胡长喜.液体发动机变推力的研究和实现[C]//航天动力技术发展与应用学术会议论文集.沈阳:中国航天第三专业信息网第二十七届年会,2006.
[46]刘朋,张平,周源泉.某燃气发生器壳体的结构可靠性分析与评估[J].推进技术,2001,22(5):411-414.
[47]闫璞,王敏庆,盛美萍.燃烧腔不稳定燃烧的有限元数值分析[J].噪声与振动控制,2005,25(5):21-23,28.
[48]FOURNET A,LONCHARD J M,THOMAS J L. Technological demonstration for low cost gas generator:AIAA-2004-4006[R]. Fort Lauderdale:AIAA,2004.
[49]NGUYEN H. Flow/thermal analysis of X-34 orbital stage gas generator design:AIAA-1996-3226[R]. Lake Buena Vista:AIAA,1996.
[50]聂万胜,庄逢辰.喷雾特性对液体火箭发动机燃烧稳定性的影响[J].推进技术,2000,21(3):56-59.
[51]苗淼,王文杰.某燃气发生器地面台架试车性能分析[J].航空动力学报,2006,21(1):41-44.
[52]KIM J,HONG S S,JEONG E H,et al. Development of a turbo pump for a 30 ton class engine:AIAA-2007-5516[R]. Cincinnati:AIAA,2007.
[53]DENNIS H J,SANDERS T. NASA fastrac engine gas generator component test program and results:AIAA-2000-3401[R]. Las Vegas:AIAA,2000.
[54]MAH C S. Evaluating the operational limits of a gas generator:AIAA-2001-3990[R]. Salt Lake City:AIAA,2001.
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