硝酸酯增塑聚醚固体推进剂力学性能研究进展
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摘要
从黏合剂基体网络结构、固体填料及固体填料/黏合剂基体界面特性等3个方面概述了硝酸酯增塑聚醚(NEPE)固体推进剂力学性能和固体推进剂力学模型的研究进展,并指出改善NEPE推进剂力学性能的方向。
The research progress in the mechanical performance of the nitrate ester plasticized polyether(NEPE) solid propellant and the mechanical models of the solid propellant is summarized from three aspects of the matrix network structure of the binder, solid filler and the interfacial characteristic between the solid filler and the binder matrix, and the directions for improving the mechanical performance of the NEPE propellant are pointed out.
The research progress in the mechanical performance of the nitrate ester plasticized polyether(NEPE) solid propellant and the mechanical models of the solid propellant is summarized from three aspects of the matrix network structure of the binder, solid filler and the interfacial characteristic between the solid filler and the binder matrix, and the directions for improving the mechanical performance of the NEPE propellant are pointed out.
引文
[1]赵永俊,张炜,张兴高,等.NEPE推进剂贮存老化性能研究[J].含能材料,2007,15(4):332-335.
[2]解红雨,吴勋,成跃,等.高能NEPE推进剂使用性能研究进展[C]//中国航空学会动力分会火箭发动机专业委员会2010年会议论文集,2010:296.
[3]庞爱民,马新刚,唐承志.固体火箭推进剂理论与工程[M].北京:中国宇航出版社,2014:56.
[4]司馥铭.聚氧化乙烯粘合剂推进剂力学性能研究[J].固体火箭技术,2004,27(1):53-56.
[5]张明权,周集义.星型PAO粘合剂在NEPE推进剂中的应用[J].化学推进剂与高分子材料,2008,6(6):4-7.
[6]SONG Xiuduo,CAO Peng,ZHENG Wei,et al.Influences of relative molecular mass of BAMO-AMMO adhesive on mechanical properties of propellants[J].China Adhesives,2017,26(8):427-454.
[7]周集义,谭惠民.环氧乙烷-四氢呋喃共聚醚在NEPE推进剂中的应用进展[J].化学推进剂与高分子材料,2001(3):1-3.
[8]MARK J E.The use of model polymer networks to elucidate molecular aspects of rubberlike elasticity[J].Advance Polymer Science,1982,44(1):1-26.
[9]KIM S Y,AHMAD J,BOTTARO J,et al.Improvements in the stress-strain behavior of urethane rubbers by bimodal network formation[J].Journal of Applied Polymer Science,1986,32(1):3 027-3 038.
[10]池旭辉.NEPE推进剂初始模量研究[D].湖北襄樊:航天科技集团第四研究院第四十二所,2002.
[11]罗运军,李国平,张斌,等.含CL-20 NEPE推进剂的力学性能[J].火炸药学报,2005,28(4):28-31.
[12]刘晶如,宋雪晶,杨寅.NEPE推进剂粘合剂网络结构调节研究[J].固体火箭技术,2010,33(1):72-76.
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[14]曾甲牙.固体填充剂对推进剂力学性能的影响[J].固体火箭技术,2002,25(1):46-50.
[15]姚维尚,刘云飞,李晓萌.改善NEPE固体推进剂力学性能的研究[C]//2004年中国兵工学会火炸药专业委员会火炸药学术研讨会,2004.
[16]MUHAMMAD Mazhar Iqbal,SAJID Raza Ch,WANGLiang,et al.Investigating the effect of solid fillers on mechanical and rheological properties of composite propellants[J].International Journal of Energetic Materials and Chemical Propulsion,2013,12(1):75-86.
[17]van RAMSHORST Marthinus C J,Di BENEDETTOGiuseppe L,DUVALOIS Willem,et al.Investigation of the failure mechanism of HTPB/AP/Al propellant by in-situ uniaxial tensile experimentation in SEM[J].Propellants,Explosives,Pyrotechnics,2016.
[18]宋会彬,刘云飞,姚维尚.含CL-20的NEPE固体推进剂的性能[J].火炸药学报,2006,29(4):44-46.
[19]OBERTH A E,BRUENNER R S.Tear phenomena around solid inclusions in castable elastomers[J].Journal of Rheology,1965(9):165-185.
[20]KIM C S,NOBLE Paul N,YOUN Chung H,et a1.The mechanism of filler reinforcement from addition of neutral polymeric bonding agents to energetic polar propellants[J].Propellants,Explosives,Pyrotechnics,1992,17(2):51-58.
[21]张斌,罗运军,谭惠民.多种键合剂与CL-20界面的相互作用机理[J].火炸药学报,2005,28(3):23-26.
[22]王延铭,赵庆华,孙翔宇,等.新型高分子键合剂的合成及其性能的研究[J].内蒙古科技大学学报,2008,27(4):341-345.
[23]杨寅,罗运军,酒永斌,等.热塑性聚氨酯弹性体包覆CL-20及对NEPE推进剂性能影响[J].固体火箭技术,2008,31(4):358-362.
[24]孟征,欧育湘.含包覆ε-HNIW的NEPE推进剂的力学性能[J].含能材料,2008,16(1):60-62.
[25]MATOU?K,INGLIS H M,GU X,et al.Multiscale modeling of solid propellants:from particle packing to failure[J].Composites Science and Technology,2007:67(7/8):l 694-1 708.
[26]MATOU?K,GEUBELLE Philippe H.Finite element formulation for modeling particle debonding in reinforced elastomers subjected to finite deformations[J].Computer Methods in Applied Mechanics and Engineering,2006,196(1/2/3):620-633.
[27]袁嵩,汤卫红,李高春.复合推进剂的细观失效机理分析[J].固体火箭技术,2006,29(1):48-51.
[28]曲凯,张旭东,李高春.复合固体推进剂非线性界面脱粘的力学性能研究[J].弹箭与制导学报,2010,30(3):114-118.
[29]曲凯,张旭东,李高春.基于内聚力界面脱黏的复合固体推进剂力学性能研究[J].火炸药学报,2008,31(6):77-81.
[30]李高春,邢耀国,戢治洪,等.复合固体推进剂细观界面脱粘有限元分析[J].复合材料学报,2011,28(3):229-235.
[31]职世君,曹付齐,申志彬,等.复合固体推进剂颗粒脱湿损伤参数反演[J].推进技术,2016,37(10):1 977-1 983.
[32]职世君,曹付齐,申志彬,等.复合固体推进剂双折线脱湿损伤模型参数影响分析[J].固体火箭技术,2017,40(2):183-188.
[33]TAN H,LIU C,HUANG Y,et al.The cohesive law for the particle/matrix interfaces in high explosives[J].Journal of Mechanics and Physics of Solids,2005,53(8):1 892-1 917.
[34]TAN H,HUANG Y,LIU C,et al.The Mori-Tanaka method for composite materials with nonlinear interface debonding[J].International Journal of Plasticity,2005,21(10):1 890-1 918.
[35]TAN H,HUANG Y,LIU C.The viscoelastic composite with interface debonding[J].Composite Science and Technology,2008,68(15/16):3 145-3 149.
[36]CHEN J K,HUANG Z P,MAI Y W.Constitutive relation of particulate-reinforced viscoelastic composite materials with debonded microvoids[J].Acta Materials,200351(12):3 375-3 384.
[37]胡少青.NEPE推进剂的粘-超弹本构模型及其应用研究[D].南京:南京理工大学,2016.
[38]李高春,邢耀国,王玉峰,等.基于细观力学的复合固体推进剂模量预估方法[J].推进技术,2007,28(4):441-444.
[39]杨书勇,刘立胜,郑剑,等.高能固体推进剂力学性能预示系统设计[J].武汉理工大学学报,2009,31(1):1-4.
[40]贵大勇,刘剑洪,田德余,等.NEPE高能推进剂力学性能模拟计算[J].推进技术,2010,31(4):444-447.
[41]韩龙,陈雄,许进升,等.基于细观模型的复合固体推进剂宏观松弛行为[J].固体火箭技术,2017,40(1):52-59.
[2]解红雨,吴勋,成跃,等.高能NEPE推进剂使用性能研究进展[C]//中国航空学会动力分会火箭发动机专业委员会2010年会议论文集,2010:296.
[3]庞爱民,马新刚,唐承志.固体火箭推进剂理论与工程[M].北京:中国宇航出版社,2014:56.
[4]司馥铭.聚氧化乙烯粘合剂推进剂力学性能研究[J].固体火箭技术,2004,27(1):53-56.
[5]张明权,周集义.星型PAO粘合剂在NEPE推进剂中的应用[J].化学推进剂与高分子材料,2008,6(6):4-7.
[6]SONG Xiuduo,CAO Peng,ZHENG Wei,et al.Influences of relative molecular mass of BAMO-AMMO adhesive on mechanical properties of propellants[J].China Adhesives,2017,26(8):427-454.
[7]周集义,谭惠民.环氧乙烷-四氢呋喃共聚醚在NEPE推进剂中的应用进展[J].化学推进剂与高分子材料,2001(3):1-3.
[8]MARK J E.The use of model polymer networks to elucidate molecular aspects of rubberlike elasticity[J].Advance Polymer Science,1982,44(1):1-26.
[9]KIM S Y,AHMAD J,BOTTARO J,et al.Improvements in the stress-strain behavior of urethane rubbers by bimodal network formation[J].Journal of Applied Polymer Science,1986,32(1):3 027-3 038.
[10]池旭辉.NEPE推进剂初始模量研究[D].湖北襄樊:航天科技集团第四研究院第四十二所,2002.
[11]罗运军,李国平,张斌,等.含CL-20 NEPE推进剂的力学性能[J].火炸药学报,2005,28(4):28-31.
[12]刘晶如,宋雪晶,杨寅.NEPE推进剂粘合剂网络结构调节研究[J].固体火箭技术,2010,33(1):72-76.
[13]赵孝彬.NEPE推进剂的相分离研究[D].北京:中国航天科技集团公司第一研究院,2002.
[14]曾甲牙.固体填充剂对推进剂力学性能的影响[J].固体火箭技术,2002,25(1):46-50.
[15]姚维尚,刘云飞,李晓萌.改善NEPE固体推进剂力学性能的研究[C]//2004年中国兵工学会火炸药专业委员会火炸药学术研讨会,2004.
[16]MUHAMMAD Mazhar Iqbal,SAJID Raza Ch,WANGLiang,et al.Investigating the effect of solid fillers on mechanical and rheological properties of composite propellants[J].International Journal of Energetic Materials and Chemical Propulsion,2013,12(1):75-86.
[17]van RAMSHORST Marthinus C J,Di BENEDETTOGiuseppe L,DUVALOIS Willem,et al.Investigation of the failure mechanism of HTPB/AP/Al propellant by in-situ uniaxial tensile experimentation in SEM[J].Propellants,Explosives,Pyrotechnics,2016.
[18]宋会彬,刘云飞,姚维尚.含CL-20的NEPE固体推进剂的性能[J].火炸药学报,2006,29(4):44-46.
[19]OBERTH A E,BRUENNER R S.Tear phenomena around solid inclusions in castable elastomers[J].Journal of Rheology,1965(9):165-185.
[20]KIM C S,NOBLE Paul N,YOUN Chung H,et a1.The mechanism of filler reinforcement from addition of neutral polymeric bonding agents to energetic polar propellants[J].Propellants,Explosives,Pyrotechnics,1992,17(2):51-58.
[21]张斌,罗运军,谭惠民.多种键合剂与CL-20界面的相互作用机理[J].火炸药学报,2005,28(3):23-26.
[22]王延铭,赵庆华,孙翔宇,等.新型高分子键合剂的合成及其性能的研究[J].内蒙古科技大学学报,2008,27(4):341-345.
[23]杨寅,罗运军,酒永斌,等.热塑性聚氨酯弹性体包覆CL-20及对NEPE推进剂性能影响[J].固体火箭技术,2008,31(4):358-362.
[24]孟征,欧育湘.含包覆ε-HNIW的NEPE推进剂的力学性能[J].含能材料,2008,16(1):60-62.
[25]MATOU?K,INGLIS H M,GU X,et al.Multiscale modeling of solid propellants:from particle packing to failure[J].Composites Science and Technology,2007:67(7/8):l 694-1 708.
[26]MATOU?K,GEUBELLE Philippe H.Finite element formulation for modeling particle debonding in reinforced elastomers subjected to finite deformations[J].Computer Methods in Applied Mechanics and Engineering,2006,196(1/2/3):620-633.
[27]袁嵩,汤卫红,李高春.复合推进剂的细观失效机理分析[J].固体火箭技术,2006,29(1):48-51.
[28]曲凯,张旭东,李高春.复合固体推进剂非线性界面脱粘的力学性能研究[J].弹箭与制导学报,2010,30(3):114-118.
[29]曲凯,张旭东,李高春.基于内聚力界面脱黏的复合固体推进剂力学性能研究[J].火炸药学报,2008,31(6):77-81.
[30]李高春,邢耀国,戢治洪,等.复合固体推进剂细观界面脱粘有限元分析[J].复合材料学报,2011,28(3):229-235.
[31]职世君,曹付齐,申志彬,等.复合固体推进剂颗粒脱湿损伤参数反演[J].推进技术,2016,37(10):1 977-1 983.
[32]职世君,曹付齐,申志彬,等.复合固体推进剂双折线脱湿损伤模型参数影响分析[J].固体火箭技术,2017,40(2):183-188.
[33]TAN H,LIU C,HUANG Y,et al.The cohesive law for the particle/matrix interfaces in high explosives[J].Journal of Mechanics and Physics of Solids,2005,53(8):1 892-1 917.
[34]TAN H,HUANG Y,LIU C,et al.The Mori-Tanaka method for composite materials with nonlinear interface debonding[J].International Journal of Plasticity,2005,21(10):1 890-1 918.
[35]TAN H,HUANG Y,LIU C.The viscoelastic composite with interface debonding[J].Composite Science and Technology,2008,68(15/16):3 145-3 149.
[36]CHEN J K,HUANG Z P,MAI Y W.Constitutive relation of particulate-reinforced viscoelastic composite materials with debonded microvoids[J].Acta Materials,200351(12):3 375-3 384.
[37]胡少青.NEPE推进剂的粘-超弹本构模型及其应用研究[D].南京:南京理工大学,2016.
[38]李高春,邢耀国,王玉峰,等.基于细观力学的复合固体推进剂模量预估方法[J].推进技术,2007,28(4):441-444.
[39]杨书勇,刘立胜,郑剑,等.高能固体推进剂力学性能预示系统设计[J].武汉理工大学学报,2009,31(1):1-4.
[40]贵大勇,刘剑洪,田德余,等.NEPE高能推进剂力学性能模拟计算[J].推进技术,2010,31(4):444-447.
[41]韩龙,陈雄,许进升,等.基于细观模型的复合固体推进剂宏观松弛行为[J].固体火箭技术,2017,40(1):52-59.