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脉冲爆震发动机性能对爆震室材料强度的需求 被引量:4

Pulse Detonation Engine's Requirements for Material Strength of its Detonation Chamber
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摘要 根据脉冲爆震发动机的工作特点及其典型的失效模式,推导了脉冲爆震发动机性能与爆震室材料强度的关系,建立了发动机性能对材料强度的需求模型。研究表明,PDE推力、推重比分别与材料屈服应力的平方和屈服应力-密度比成正比。要应用于实际,必须克服高温工作环境的障碍,可以研制新的耐高温高强度材料;表面喷涂陶瓷热胀涂层;采取高效的冷却措施等。 Following the the relationship between working principle and typical failure mode of a pulse detonation engine (PDE), we induce its performance and the material strength of its detonation chamber and establish the model for the requirement of the PDE on material strength. The PDE's thrust and thrust-to-weight ratio are proportional respectively to the square of the material's yield stress and its yield stress-to-density ratio. Its application requires the removal of obstacles encountered in the high-temperature environment. To do so, high temperature-resistant and high-strength materials should be developed; adding ceramic coatings and adopting effective cooling measures are also necessary.
出处 《机械科学与技术》 CSCD 北大核心 2007年第5期623-625,共3页 Mechanical Science and Technology for Aerospace Engineering
基金 中国博士后科学基金项目(中博基[2003]03号) 军队2110工程项目资助
关键词 脉冲爆震发动机 材料强度 屈服应力 pulse detonation engine material strength yield stress
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参考文献7

  • 1陈永刚,何立明,康强,李明奎.基于特征线的脉冲爆震发动机性能估算与结构参数设计[J].空军工程大学学报(自然科学版),2005,6(3):1-3. 被引量:3
  • 2Chao T,Cirak F,Shepherd J E.Validation Experiments:Detonation-Drive Fracture of Tubes.http://bill.cacr.caltech.edu/val-workshop/upload/files/val3 -chao.pdf.
  • 3Beltman W M,Shepherd J E.Structural Response of Shells to Detonation and Shock Loading[R].GALCIT Report,Graduate Aeronautical Laboratories,California Institute of Technology,1998.
  • 4Shepherd J.Pressure Loads and Structural Response on the BNL High-temperature Detonation Tube[R].Technical Report A-3991,Brookhaven National Laboratory,Upton,New York 11973,1992.
  • 5Wintenberger E,Austin J M,Cooper M,et al.An Analytical Model for the Impulse of a Single-cycle Pulse Detonation Engine[R].AIAA2001-3811,2001.
  • 6Chao T W,et al.On the Design of Pulse Detonation Engines[R].GALCIT Report FM 00-7,Graduate Aeronautical Laboratories,California Institute of Technology,2001.
  • 7Bussing T,Pappas G.An Introduction to Pulse Detonation Engine[R].AIAA94-0263.

二级参考文献5

  • 1Lailasanath K, Patnaik G, Li V. Computation studies of Pulse Detonation Engine: a Status Report[R]. AIAA 1999-2634.
  • 2Wintenberger E,Austin J M. An Analytical Model for the Impulse of a Single - Cycle Pulse Detonation Engine[]. AIAA 2001-3811.
  • 3Chao T,Wintenberger E,Shepherd E.On the Design of Pulse Detonation Engines[R].GALCIT Report FM 00-7 CA 91125.
  • 4Bussing T,Pappas G.An Introduction to Pulse Detonation Engine[R].AIAA 94-0263.
  • 5袁泉,祝雪平,何立明,程邦勤,陈鑫.混合气压力对爆震波特征参数的影响规律[J].空军工程大学学报(自然科学版),2003,4(4):1-4. 被引量:1

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