国防科技大学学报
國防科技大學學報
국방과기대학학보
JOURNAL OF NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY
2014年
1期
110-115
,共6页
邹腾安%潘存云%徐小军%陈虎
鄒騰安%潘存雲%徐小軍%陳虎
추등안%반존운%서소군%진호
双转子%活塞%零维模型%数值模拟
雙轉子%活塞%零維模型%數值模擬
쌍전자%활새%령유모형%수치모의
twin-rotor%piston%zero-dimension model%numerical simulation
双转子活塞发动机是一种新型的差速式转子发动机,与传统发动机相比较具有很多优点,如不需要复杂的阀门装置,而且功率密度更高等。为了分析和研究双转子活塞发动机的运行特性,针对该发动机工作循环的热力学过程建立了其零维模型,确定了主要的边界条件,运用Matlab/simulink进行了数值模拟。对应不同的主轴转角,计算出气缸内工质的质量值、压力值和温度值。基于算得的压力值,求取了该发动机的平均指示压力和功重比等参数,与传统发动机相比较,双转子活塞发动机气缸工作容积的利用程度更大,整体结构更加紧凑。
雙轉子活塞髮動機是一種新型的差速式轉子髮動機,與傳統髮動機相比較具有很多優點,如不需要複雜的閥門裝置,而且功率密度更高等。為瞭分析和研究雙轉子活塞髮動機的運行特性,針對該髮動機工作循環的熱力學過程建立瞭其零維模型,確定瞭主要的邊界條件,運用Matlab/simulink進行瞭數值模擬。對應不同的主軸轉角,計算齣氣缸內工質的質量值、壓力值和溫度值。基于算得的壓力值,求取瞭該髮動機的平均指示壓力和功重比等參數,與傳統髮動機相比較,雙轉子活塞髮動機氣缸工作容積的利用程度更大,整體結構更加緊湊。
쌍전자활새발동궤시일충신형적차속식전자발동궤,여전통발동궤상비교구유흔다우점,여불수요복잡적벌문장치,이차공솔밀도경고등。위료분석화연구쌍전자활새발동궤적운행특성,침대해발동궤공작순배적열역학과정건립료기령유모형,학정료주요적변계조건,운용Matlab/simulink진행료수치모의。대응불동적주축전각,계산출기항내공질적질량치、압력치화온도치。기우산득적압력치,구취료해발동궤적평균지시압력화공중비등삼수,여전통발동궤상비교,쌍전자활새발동궤기항공작용적적이용정도경대,정체결구경가긴주。
Dual-rotor piston engine (DRPE)is a new type of differential rotary engine,with the pistons moving in a circle rather than linearly. Compared with the conventional engines,the complex valve systems can be omitted,and its power density is higher.In order to study the major performance indicators of DRPE,Matlab/simulink was used to simulate the zero-dimension model of its thermodynamic process.With regard to the characteristics of DRPE’s working process,the differential equations were established.Taking into account various period features,the equations were simplified.The ways to solve the major boundary conditions were found.Values of the mass,pressure and temperate were calculated according to different shaft angles.Then DRPE ’s indicated mean effective pressure and power to weight ratio were calculated.Compared with some conventional internal combustion engines,the volume of DRPE’s chamber is used more efficiently,and its integral structure is more compact.