Nozzle effects on thrust and inlet pressure of a multi-cycle air-breathing pulse detonation engine （APDE） are investigated experimentally. An APDE with 68 mm in diameter and 2 050 mm in length is operated using gaso...Nozzle effects on thrust and inlet pressure of a multi-cycle air-breathing pulse detonation engine （APDE） are investigated experimentally. An APDE with 68 mm in diameter and 2 050 mm in length is operated using gasoline/air mixture. Straight nozzle, converging nozzle, converging-diverging nozzle and diverging nozzle are tested. The results show that thrust augmentation of converging-diverging nozzle, diverging nozzle or straight nozzle is better than that of converging nozzle on the whole. Thrust augmentation of straight nozzle is worse than those of converging-diverging nozzle and diverging nozzle. Thrust augmentations of diverging nozzle with larger expansion ratio and converging-diverging nozzle with larger throat area range from 20% to 40% on tested frequencies and are better than those of congeneric other nozzles respectively. Nozzle effects on inlet pressure are also researched. At each frequency it is indicated that filling pressures and average peak pressures of inlet with diverging nozzle and converging-diverging nozzle with large throat cross section area are higher than those with straight nozzle and converging nozzle Pressures near thrust wall increase in an increase order from without nozzle, with diverging nozzle, straight nozzle and converging-diverging nozzle to converging nozzle.展开更多
There exists inlet-engine match conflict between high and low speeds for a non-adjustable bump inlet.A scheme of using a bistable bump surface at the throat region of the inlet is proposed to adjust the throat area.Th...There exists inlet-engine match conflict between high and low speeds for a non-adjustable bump inlet.A scheme of using a bistable bump surface at the throat region of the inlet is proposed to adjust the throat area.The FEM model of the bistable surface is established with hinged constraint,and the bistability condition and structural transition process are investigated in detail.Moreover,the effects of loading method,loading position and structural parameters on critical driving force,input energy and structural strain are studied.Finally,the influences of an elastic boundary condition on the structural bistability are discussed.The results show that the bistability of the adjustable bump surface requires a certain boundary constraint and geometric parameter combination,and that there are local and overall snap-through phenomena during transition which are related to the loading position and structural parameters.Therefore,suitable loading position and structural material could reduce input energy and meet the demand of structural strain.展开更多
为了提高汽油机部分负荷下的燃油经济性,该文通过改变废气再循环率(EGR,exhaust gas recirculation)和过量空气系数,在一台增压进气道喷射汽油机上进行试验,研究了过量空气系数与EGR耦合对发动机部分负荷下燃油经济性和排放的影响。结...为了提高汽油机部分负荷下的燃油经济性,该文通过改变废气再循环率(EGR,exhaust gas recirculation)和过量空气系数,在一台增压进气道喷射汽油机上进行试验,研究了过量空气系数与EGR耦合对发动机部分负荷下燃油经济性和排放的影响。结果表明:随着EGR率和过量空气系数α的增加,燃烧循环变动率变大,燃烧持续期变长,且EGR是影响两者的主要因素;泵气损失显著减少,有效燃油消耗率显著降低,与EGR率=0和过量空气系数α=1条件下相比,EGR率=20%和过量空气系数α=1.1条件下的有效燃油消耗率降低了8.37%;随着EGR率的增加,THC(total hydrocarbon)排放增加,但NOx排放显著降低,高达约80%。因此,将三效催化转化器和EGR技术相结合,燃烧稀混合气,可以在满足欧Ⅴ排放法规的同时,大幅提高汽油机部分负荷下的燃油经济性。展开更多
基金National Natural Science Foundation of China(50976094, 51176158)Reseach Fund for the Doctoral Program of Higher Education of China(20096102110022)Doctorate Foundation of Northwestern Polytechnical University (CX200909)
文摘Nozzle effects on thrust and inlet pressure of a multi-cycle air-breathing pulse detonation engine （APDE） are investigated experimentally. An APDE with 68 mm in diameter and 2 050 mm in length is operated using gasoline/air mixture. Straight nozzle, converging nozzle, converging-diverging nozzle and diverging nozzle are tested. The results show that thrust augmentation of converging-diverging nozzle, diverging nozzle or straight nozzle is better than that of converging nozzle on the whole. Thrust augmentation of straight nozzle is worse than those of converging-diverging nozzle and diverging nozzle. Thrust augmentations of diverging nozzle with larger expansion ratio and converging-diverging nozzle with larger throat area range from 20% to 40% on tested frequencies and are better than those of congeneric other nozzles respectively. Nozzle effects on inlet pressure are also researched. At each frequency it is indicated that filling pressures and average peak pressures of inlet with diverging nozzle and converging-diverging nozzle with large throat cross section area are higher than those with straight nozzle and converging nozzle Pressures near thrust wall increase in an increase order from without nozzle, with diverging nozzle, straight nozzle and converging-diverging nozzle to converging nozzle.
基金supported by the National Natural Science Foundation of China(Nos.11172128,51475228)the Specialized Research Fund for the Doctoral Program of Higher Education of China (No.20123218110001)+1 种基金the Research Fund of State Key Laboratory of Mechanics and Control of Mechanics Structures (Nanjing University of Aeronautics and Astronautics)(No.0515G01)the Priority Academic Program Development of Jiangsu Higher Education Institutions and the Funding of Jiangsu Innovation Program for Graduate Education(the Fundamental Research Funds for the Central Universities)(No.CXZZ12_ 0139)
文摘There exists inlet-engine match conflict between high and low speeds for a non-adjustable bump inlet.A scheme of using a bistable bump surface at the throat region of the inlet is proposed to adjust the throat area.The FEM model of the bistable surface is established with hinged constraint,and the bistability condition and structural transition process are investigated in detail.Moreover,the effects of loading method,loading position and structural parameters on critical driving force,input energy and structural strain are studied.Finally,the influences of an elastic boundary condition on the structural bistability are discussed.The results show that the bistability of the adjustable bump surface requires a certain boundary constraint and geometric parameter combination,and that there are local and overall snap-through phenomena during transition which are related to the loading position and structural parameters.Therefore,suitable loading position and structural material could reduce input energy and meet the demand of structural strain.
文摘为了提高汽油机部分负荷下的燃油经济性,该文通过改变废气再循环率(EGR,exhaust gas recirculation)和过量空气系数,在一台增压进气道喷射汽油机上进行试验,研究了过量空气系数与EGR耦合对发动机部分负荷下燃油经济性和排放的影响。结果表明:随着EGR率和过量空气系数α的增加,燃烧循环变动率变大,燃烧持续期变长,且EGR是影响两者的主要因素;泵气损失显著减少,有效燃油消耗率显著降低,与EGR率=0和过量空气系数α=1条件下相比,EGR率=20%和过量空气系数α=1.1条件下的有效燃油消耗率降低了8.37%;随着EGR率的增加,THC(total hydrocarbon)排放增加,但NOx排放显著降低,高达约80%。因此,将三效催化转化器和EGR技术相结合,燃烧稀混合气,可以在满足欧Ⅴ排放法规的同时,大幅提高汽油机部分负荷下的燃油经济性。
