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1.
In order to investigate the effects of fuel injection distribution on the scramjet combustor performance, there are conducted three sets of test on a hydrocarbon fueled direct-connect scramjet test facility. The results of Test A, whose fuel injection is carried out with injectors located on the top-wall and the bottom-wall, show that the fuel injection with an appropriate close-front and centralized distribution would be of much help to optimize combustor performances. The results of Test B, whose fuel injection is performed at the optimal injection locations found in Test A, with a given equivalence ratio and different injection proportions for each injector, show that this injection mode is of little benefit to improve combustor performances. The results of Test C with a circumferential fuel injection distribution displaies the possibility of ameliorating combustor performance. By analyzing the effects of injection location parameters on combustor performances on the base of the data of Test C, it is clear that the injector location has strong coupled influences on combus- tor performances. In addition, an inner-force synthesis specific impulse is used to reduce the errors caused by the disturbance of fuel supply and working state of air heater while assessing combustor performances.  相似文献   
2.
用同一种发动机在不同模拟状态下,采用技改措施及加热器的火焰筒不同个数进行了试验,获得了模拟温度、气源压力与时间的关系。设备的总压系数为0.67;加热系统的总效率为0.41-0.55。与另一高空台使用同一间接加热系统的总效率(约为0.62)相比有所不同。分析了原因,并指出了解决问题的途径。上述试验方法及试验结果可供类拟发动机试验参考使用。  相似文献   
3.
冲压发动机试车台空气燃烧加热器流量参数计算   总被引:2,自引:0,他引:2       下载免费PDF全文
给出了空气燃烧加热器热力计算方程,计算得到了燃烧加热所需燃料流量以及补氧量随模拟飞行马赫数变化曲线,分析了加热器压力对加热所需燃料流量以及补氧量的影响。计算分析结果可为冲压发动机试车台空气燃烧加热器设计提供参考。  相似文献   
4.
本文报导了1992年7月在美国纳希维尔召开的 AIAA 第17届航空航天地面试验会议的概况。简要地介绍了讨论航空航天地面试验面临的技术挑战,CFD 和地面试验的相互作用,美国气动力学与气动热力学研究的未来等三个大会报告的内容。介绍了在会议报告中叙述的对高超声速气动试验的新要求和自由飞弹道靶、 脉冲风洞、稀薄气体设备、电弧加热器的新进展。最后,对我国高超声速气动试验的发展提出了建议。  相似文献   
5.
The purpose of this work is to report the experimental evidences for the influence of perturbations in the electron density in the dayside mid-latitude ionosphere, that are caused by high-frequency heating of the F2 layer, on the GNSS signals. The experiments were carried out at the Sura heater (Radio Physical Research Institute, N. Novgorod). During the sessions of ionospheric heating with different time modulations of the radiated power the rays linking the navigational satellites with the ground receiver intersected the heated region. Variations in the total electron content (TEC) were studied; these variations are proportional to the reduced phases of navigational signals. It is shown that with the square-wave modulation of the radiated power (with periods of 1, 6, 10 and 15 min), perturbations with periods of the main modulation of heating and its harmonics appear in the spectrum of TEC variations. Examples are presented of identification of the heating-induced variations in TEC, including determination of the amplitudes and time characteristics of these variations.  相似文献   
6.
A cathode mandrel with translational and rotational motion, which was supposed to obtain uniform friction effect on surface, was employed in abrasive-assisted electroforming for revolving parts with complex profile. The effects of current density, translational speed and rotational speed on the deposit properties were studied by orthogonal test. The tensile strength, elongation and micro hardness value were measured to find out how the factors affected the properties. The optimized results show that changes of current density affect the tensile strength of nickel layer most, while translational speed has the most remarkable influences on both elonga-tion and micro hardness. The low rotational speed affects the properties least. In this experiment, a smooth nickel layer with tensile strength 581 MPa, elongation 17%and micro hardness 248HV is obtained by the orthogonal test.  相似文献   
7.
隆永胜  朱新新  袁竭 《航空动力学报》2020,35(10):2028-2035
发动机尾焰、燃烧加热、电弧加热器等高温高速气流总焓测量存在较大误差,采用结构优化的质量吸入水冷焓探针,标定后的驻点热流和驻点压力探针(Fay-Riddell公式法)对高温高速气流总焓进行了对比测试。结果表明:焓值为2.5~5 MJ/kg时,焓探针的测试误差约为3.38%,采用Fay-Riddell公式法获得焓值的误差约为3%。焓探针与Fay-Riddell公式法平均偏差约为4.65%。在地面模拟试验时采用两种测焓方法确定测试精度,对减小高温高速气流测焓误差,提高试验模拟精度具有积极的作用。  相似文献   
8.
介绍了第二代B737飞机座舱增压系统后外流活门和加温垫的工作及控制原理,对实际维护中的一种典型故障进行了分析和研究。  相似文献   
9.
本文研究的是以MCS-51系列单片机为核心的计算机控制系统,用以实现化工催化剂活性检测过程床层温度程序控制。被控对象是具有3~8分钟的纯滞后,时变,非线性特性的催化剂电加热炉。控制难度大。 采用了广义最小方差自校正控制算法,具有时变滞后的极点自校正PID算法,极点对消直接PID三种算法进行了仿真与现场试验研究。前两种,由于工作过程允许的信号对系统激励不够充分,对象在线辩识有困难,试验结果表现,不能实现预期的控制要求。最终采用了极点对消直接PID算法,成功地实现了催化剂活性温度自动控制。该系统工作稳定、可靠,控制精度达到了检测标准要求。  相似文献   
10.
The method of reliability is proposed for the investigation of thermal contact conductance (TCC) in this study. A new definition is introduced, namely reliability thermal contact conductance (RTCC), which is defined as the TCC value that meets the reliability design requirement of the structural materials under consideration. An experimental apparatus with the compensation heater to test the TCC is introduced here. A practical engineering example is utilized to demonstrate the applicability of the proposed approach. By using a statistical regression model along with experimental data obtained from the interfaces of the structural materials GH4169 and K417 used in aero-engine, the estimate values and the confidence level of TCC and RTCC values are studied and compared. The results show that the testing values of TCC increase with interface pressure and the proposed RTCC model matches the test results better at high interface pressure.  相似文献   
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