PDF下载 分享
[1]张留欢,杜 泉,逯婉若,等.裂解度对甲醇ATR发动机的性能影响分析[J].火箭推进,2019,45(01):31-35.
　ZHANG Liuhuan,DU Quan,LU Wanruo,et al.Effect of cracking ratio on the performance of methanol ATR engine[J].Journal of Rocket Propulsion,2019,45(01):31-35.
点击复制

裂解度对甲醇ATR发动机的性能影响分析

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 45 期数: 2019年01期 页码: 31-35 栏目: 研究与设计 出版日期: 2019-02-28
Title:
Effect of cracking ratio on the performance of methanol ATR engine
文章编号:
1672-9374(2019)01-0031-05
作者:
张留欢; 杜 泉; 逯婉若; 张蒙正; 李光熙
(西安航天动力研究所,陕西 西安710100)
Author(s):
ZHANG Liuhuan;  DU Quan;  LU Wanruo;  ZHANG Mengzheng;  LI Guangxi
(Xi'an Aerospace Propulsion Institute, Xi'an 710100, China)
关键词:
碳氢燃料裂解;  ATR发动机;  裂解度
Keywords:
hydrocarbon fuel cracking;  ATR engine;  cracking ratio
分类号:
V439
文献标志码:
A
摘要:
提出了一种基于甲醇裂解工作的ATR发动机方案,并对特定裂解气成分的甲醇ATR发动机性能进行计算,研究了裂解气中裂解度对发动机性能的影响规律。结果表明:随着发动机转速上升,推力逐渐上升,比冲先增加后减小,在90%转速百分比时,比冲最高; 在同一转速下,甲醇裂解度越高,发动机比冲越大,在裂解度100%、转速百分比90%条件下,发动机比冲最高达到约793 s; 随着裂解度逐渐升高,裂解气比热容逐渐升高。
Abstract:
A new ATR(Air Turbo Rocket)engine scheme based on the methanol cracking is proposed in this paper.The performance of methanol ATR engine with specific composition of cracking gas is calculated, and the influence of cracking ratio on the engine performance is investigated.The results show that the thrust gradually increases, and the specific impulse increases first then decreases as the engine speed increases.The specific impulse reaches the top at the 90% designed speed.Under the same engine speed, the higher the cracking ratio of methanol, the greater the specific impulse of engine.Under the condition of 100% cracking ratio and 90% rotation speed, the specific impulse is up to 793s.In addition, the specific heat capacity of cracking gas increases with the increase of cracking ratio.

参考文献/References:

[1] CHRISTENSEN K.Air turborocket/vehicle performance comparison[J].Journal of Propulsion and Power, 1999, 15(5):706-712.
[2] 南向谊,王拴虎,李平.空气涡轮火箭发动机研究的进展与展望[J].火箭推进,2008,34(6):31-35.
NAN X Y, WANG S H, LI P.Investigation on status and prospect of air turbine rocket[J].Journal of Rocket Propulsion, 2008, 34(6): 31-35.
[3] TANATSUGU N, NARUO Y, ROKUTANDA I.Test results on air turbo ramjet for a future space plane:AIAA1992-5054[R].Reston: AIAA,1992.
[4] CHRISTENSEN K.Comparison of methods for calculating turbine work in the air turbo rocket[J].Journal of Propulsion and Power, 2001, 17(2): 256-261.
[5] SULLEREY K, PRADEEP M, KEDIA M.Performance comparison of air turbo rocket engine with different fuel systems: AIAA2003-4417[R].Reston: AIAA, 2003.
[6] BUSSI G, COLASURDO G, PASTRONE D.Analysis of air-turbo-rocket performance[J].Journal of Propulsion and Power, 1995,11(5): 950-954.
[7] TANATSUGU N.Developments in high speed vehicle propulsion systems[M].Reston: AIAA, 1996.
[8] RYOJIRO M, KAZUYUKI H, NOBUHIRO T.Design and development of bio-Ethanol fueled GG-cycle air turbo ramjet engine for supersonic UAV: ISABE-2013-1654[R].Busan: ISABE, 2013.
[9] MINATO R, HIGASHINO H, TANATSUGU N.Design and performance analysis of bio-ethanol fueled GG-cycle air turbo ramjet engine: AIAA2012-0842[R].Reston: AIAA, 2012.
[10] HARADA K, TANATSUGU N, SATO T.Development study on precooler for ATREX Engine: AIAA1999-4897[R].Reston: AIAA, 1999.
[11] SHUJIRO S, TETSUYA S, HIROAKI K, NOBUHIRO T.Flight test plan for ATREX engine development: AIAA2003-7027[R].Reston: AIAA, 2003.
[12] 赵祖亮.吸热型碳氢燃料结焦与超临界压力下传热性质研究[D].杭州:浙江大学,2006.
[13] 王艳华,郑国璋.甲醇燃料在车用发动机上的应用研究[J].内燃机工程,2005,26(2): 22-25.
[14] 朱建军,寇子明,王淑平,等.纯甲醇发动机冷起动系统的研发[J].汽车工程,2011,33(4): 298-302.
[15] 杨蔚权,许世海.甲醇作为发动机燃料的使用方法[J].内燃机,2005(5): 32-35.
[16] 王放.缸内直喷点燃式甲醇发动机冷启动试验研究[D].长春:吉林大学,2012.
[17] 王进.纯甲醇裂解气发动机试验研究[D].济南:山东大学,2013.
[18] 姚春德,李旭聪,徐元利.甲醇裂解气发动机排放性能试验[J].内燃机学报,2012,30(2): 118-123.
[19] 姚春德,徐元利,杨建军,等.甲醇裂解气对点燃式发动机性能影响研究[J].工程热物理学报,2009, 30(2): 353-356.
[20] 杨永广.甲醇裂解气发动机的试验研究[D].济南:山东大学,2011.
[21] 张琴,刘国柱,李国柱,等.主动冷却通道内甲醇催化分解吸热过程[J].推进技术,2015,36(6): 927-932.
[22] 姚春德,李旭聪,唐超,等.铜基/钯基催化剂甲醇裂解气发动机的燃烧特性[J].内燃机学报,2012,30(6): 486-491.
[23] ALEXANDER B, BRANKO R.Third millennium ideal gas and condensed phase thermochemical database for combustion with updates from active thermochemical tables[R].Argonne: Argonne National Laboratory, 2005.
[24] 胡骏,吴铁鹰,曹人靖.航空叶片机原理[M].北京:国防工业出版社,2006.

相似文献/References:

[1]李永洲,李哲,李光熙,等.ATR/冲压组合动力高超声速飞行器性能分析[J].火箭推进,2018,44(03):6.
　LI Yongzhou,LI Zhe,LI Guangxi,et al.Performance analysis of hypersonic aircraft with ATR/ramjet combined power[J].Journal of Rocket Propulsion,2018,44(01):6.
[2]张留欢,马化杰,周建平,等.氨解离度对无水肼ATR发动机性能影响研究[J].火箭推进,2019,45(02):16.
　ZHANG Liuhuan,MA Huajie,ZHOU Jianping,et al.Performance analysis of hydrazine ATR with different dissociated ratios of NH3different[J].Journal of Rocket Propulsion,2019,45(01):16.

备注/Memo

收稿日期:2017-06-25
基金项目:装备预研航天科技联合基金(6141B0606260401)
作者简介:张留欢(1986—),男,硕士,工程师,研究领域为组合推进系统气动热力技术

更新日期/Last Update: 2019-02-20