首页> 美国政府科技报告 >Optimizing the NAHBE Piston Cap Design Utilizing Schlieren Photography Methods and Applications of the Helmholtz Resonator Theory
【24h】

Optimizing the NAHBE Piston Cap Design Utilizing Schlieren Photography Methods and Applications of the Helmholtz Resonator Theory

机译:利用schhlren摄影方法和亥姆霍兹谐振器理论的应用优化NaHBE活塞帽设计

获取原文

摘要

The Naval Academy Heat Balanced Engine (NAHBE) has been studied extensively for the last five years. Efforts to understand and predict the process occurring in the engine were complicated and difficult to verify experimentally. Optimization of the output of the engine, through possible, took much too long a time through parametric variation. An answer to the problem of predicting the time dependent reaction occurring in the engine was sought. Also, some easy design tool for optimizing the reaction was required. One possible solution to these problems was to model the NAHBE piston cap through the Helmholtz Resonator Theory. This theory generalizes the time dependent reaction of a volume of fluid in a chamber by the acoustic analog to the mechanical system forced oscillator. The theory enables one to predict or design the acoustic impedance of a cavity and its natural frequency by way of the cavity and inlet geometry. This study shows how the solution to the Helmholtz Theory may be obtained and the fluid mass displacement of NAHBE cap modeled by the Helmholtz Theory predicted. The solution of hte NAHBE cap reaction by the Hemholtz Theory, however, is only a hypothesis until it is substantiated. Conclusive evidence is shown in this study through a high-speed Schlieren film analysis of the actual combustion process in a NAHBE, that the theory holds true for and can predict reality. Thus, it is proven that the Helmholtz Theory, which can be used as a design tool, can model the real systems found in heat balanced engines today. (Author)

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号