某发动机调节器自动检测异常故障分析

针对某型发动机自动调节器自动检测异常的故障现象,对产生发动机自动调节器自动检测异常的原因进行了深入地研究分析,并提出了针对性的预防措施。     

Satellite launch vehicle effect on the Earth’s lower ionosphere: A case study

The effect of the rocket exhaust products on the D-region of the ionosphere is investigated with the help of Very low frequency (VLF) electromagnetic wave propagation characteristics within the Earth-ionosphere waveguide. The changes in the electron density profile are computed from the observed VLF signal amplitude perturbations about 3 dB during the rocket launch. We find a localized electron depletion in the lower ionosphere at an altitude of around 58 km, that is thought to be originated by the attachment of ionospheric ion and molecular hydrogen along with water molecule in the exhaust product of first stage burn of Geosynchronous Launch Vehicle (GSLV) rocket at the time of GSLV launched from Sriharikota, India, on 27 August 2015 at 11:22 UT (16:52 IST). The ionospheric depletion perturbed the navigational VLF signal (VTX = 17 kHz) 134 s after the launch of the GSLV rocket.     

浅谈水洗发动机对大修成本的影响

通过对深圳航空公司CFM56-7B发动机水洗方法改进前后的发动机进厂大修数据进行比较,主要分析HPT导向器报废率的变化,说明改进的发动机水洗方式对于延长发动机在翼时间、降低HPT导向器报废率、节约大修成本起到良好促进作用。     

Three-dimensional numerical analysis on combustion performance and flow of hybrid rocket motor with multi-segmented grain

This paper presents the combustion characteristics in hybrid rocket motors with multi-segmented grain through three-dimensional numerical simulations. Multi-segmented grain is composed of several thin grains with two or more ports. The numerical model consists of Navier-Stokes equations with turbulence, solid fuel pyrolysis, chemical reactions, a fluid–solid coupling model and a regression rate model. The simulations adopt 90% Hydrogen Peroxide (HP) and PolyEthylene (PE) as the propellant combination. The effects of the rotation, port number, fuel grain segment number and mid-chamber length on the flow field and combustion performances are analyzed. The results indicate that the multi-segmented grain configuration can strengthen the flow field, and the regression rate and combustion efficiency are enhanced. Take the cases with two grain segments and three ports for example, the regression rate is increased by 32.4%−45.1% and the combustion efficiency increases by 6%−8.6% in different rotation angles.     

ENERGY-SAVING MATCHING STRATEGY AND EXPERIMENTAL STUDY OF PUMPING SYSTEM FOR TRUCK-MOUNTED CONCRETE PUMP

Aiming at the high fuel consumption and use-cost of truck-mounted concrete pump , an energy-saving matching strategy of pumping system is presented and the experimental study is conducted.Since pumping system occupies most resources of engine , the matching strategy between engine and main pump is analyzed to meet the load demand and reduce the engine rational speed drop.The testing method is established to measure the fuel consumption of engine under various working conditions , and the experimental data are analyzed to find the law of the fuel consumption of engine.The system performance can be improved by adjusting the system input value.Finally , the energy-saving matching strategy is established to reduce the fuel consumption of truck for unit workload , which provides a new approach for the energy-saving of truck-mounted concrete pump.     

某靶用型无人机发动机空中停车故障分析

针对某新型靶机出现的发动机空中停车故障,对测控站记录数据进行分析,发现了转速采集系统和ECU控制系统存在的缺陷,并提出了解决措施。     

某型涡轴发动机起动冷转异响故障分析

针对外场某型涡轴发动机首次装直升机起动冷运转过程中,发动机有异常响声的故障现象,对发动机进行了分解检查、质量复查、原因分析和机理分析等工作,找准了故障原因,制定了预防措施,完善规范了发动机装配工艺规程,有利于预防同类故障的再发生,提高了该型航空发动机的安全性和可靠性。     

PW4000发动机2.5级放气系统故障分析

介绍了PW4000发动机2.5放气系统的构成、工作原理及常见故障,针对一起机械连接失效导致的喘振故障进行分析并寻找故障根源,为故障判断和该型发动机的工程管理提供了参考。     

柴油发动机热管理系统的高度特性

基于空中和高原环境的特点,研究了柴油发动机散热器传热性能的高度特性;进一步建立了发动机热管理系统的流动和传热模型,研究了热管理系统的高度特性;给出了基于最小功耗原则的热管理系统运行参数匹配方法.在固定系统热负荷条件下的计算结果表明:随着海拔高度的增加,在空中环境下,散热器的散热性能先上升后下降,热管理系统中冷却液和润滑油温度先下降后上升,热管理系统所需的最小功耗先减小后增加;在高原环境下,散热器的散热性能随高度增加大幅下降,热管理系统中冷却液和润滑油温度大幅上升,发动机出现过热问题,为了给发动机提供足够的散热能力,热管理系统所需要的最小功耗随着海拔高度的增加而大幅增加.      

翼吊发动机安装结构等效建模及其隔振设计

为了研究翼吊发动机安装结构隔振特性并优化其隔振器设计,建立了发动机安装节-吊架-机翼结构理论分析及有限元模型.利用有限元方法进行了模态验证并分析了安装结构的隔振特性.进行发动机3种典型工况下的结构动响应分析确定了振动传递的主路径.基于振动传递路径法研究了隔振器参数和安装位置对安装系统隔振性能的影响规律.结果表明:振动载荷经安装结构后低压转子转频和高压转子转频峰值响应分别降低22.03%和14.65%.低压转子转频振动传递主路径为发动机-前安装节-吊架-机翼,高压转子转频为发动机-后安装节-上连杆-机翼.通过合理设置隔振器位置可以使安装系统隔振率达到50.41%,隔振器的频率比为5和阻尼比为0.25时安装系统隔振率可达70.67%.为了优化整个发动机安装系统的隔振效果,设计隔振器时必须选取合适的安装位置和参数.