农业工程学报
農業工程學報
농업공정학보
2013年
18期
34-42
,共9页
宋淑然%阮耀灿%洪添胜%代秋芳%夏侯炳
宋淑然%阮耀燦%洪添勝%代鞦芳%夏侯炳
송숙연%원요찬%홍첨성%대추방%하후병
数值计算%优化%试验%风送式喷雾机%喷幅%喷筒
數值計算%優化%試驗%風送式噴霧機%噴幅%噴筒
수치계산%우화%시험%풍송식분무궤%분폭%분통
numerical analysis%optimization%experiments%air-blast sprayer%spray width%duct
风送式喷雾机喷筒结构的不同,影响其流场的分布及喷幅的大小,该文提出在原有的圆形喷筒喷雾机的基础上附加扩幅段的方法,使同一台风送式喷雾机具有不同的喷雾特性。利用数值计算方法,采用RNG k-ε模型,对附加3种不同类型扩幅段的喷筒进行了数值计算与分析。仿真分析发现,喷筒中气流运动分为3个阶段:靠近风扇区域中,气流呈紊流状态,在柱形喷筒与收缩喷筒区域中,层流与紊流并存,而在扩幅喷筒中,气流存在紊流并发生了流速的重新分布。其中,3种类型的喷筒中,在柱形喷筒及收缩喷筒内,I型和III型喷筒内气流速度的突变区域较多,II型喷筒中气流速度的突变区域较少;在扩幅喷筒中,I型和III型喷筒内的紊流区域较多,使得I型和III型喷筒效率较低。以喷筒效率高为优化目标,获得了宽喷幅风送式喷雾机扩幅段喷筒的优化结构,并试制了试验样机;利用试验样机,对宽喷幅风送式喷雾机的出风口风速及喷幅进行了实际测试。试验结果表明,采用优化后的扩幅喷筒,在出风口处实测的流场数据与仿真结果之间的误差在-1.49%~1.91%内;宽喷幅风送式喷雾机喷幅与送风距离间成二次多项式变化规律,在喷筒轴线方向上距出风口4.5 m处出现的喷幅最宽为3.56 m,与同功率下的未加扩幅喷筒的风送式喷雾机最大喷幅2.29 m相比,喷幅扩大了55.46%。
風送式噴霧機噴筒結構的不同,影響其流場的分佈及噴幅的大小,該文提齣在原有的圓形噴筒噴霧機的基礎上附加擴幅段的方法,使同一檯風送式噴霧機具有不同的噴霧特性。利用數值計算方法,採用RNG k-ε模型,對附加3種不同類型擴幅段的噴筒進行瞭數值計算與分析。倣真分析髮現,噴筒中氣流運動分為3箇階段:靠近風扇區域中,氣流呈紊流狀態,在柱形噴筒與收縮噴筒區域中,層流與紊流併存,而在擴幅噴筒中,氣流存在紊流併髮生瞭流速的重新分佈。其中,3種類型的噴筒中,在柱形噴筒及收縮噴筒內,I型和III型噴筒內氣流速度的突變區域較多,II型噴筒中氣流速度的突變區域較少;在擴幅噴筒中,I型和III型噴筒內的紊流區域較多,使得I型和III型噴筒效率較低。以噴筒效率高為優化目標,穫得瞭寬噴幅風送式噴霧機擴幅段噴筒的優化結構,併試製瞭試驗樣機;利用試驗樣機,對寬噴幅風送式噴霧機的齣風口風速及噴幅進行瞭實際測試。試驗結果錶明,採用優化後的擴幅噴筒,在齣風口處實測的流場數據與倣真結果之間的誤差在-1.49%~1.91%內;寬噴幅風送式噴霧機噴幅與送風距離間成二次多項式變化規律,在噴筒軸線方嚮上距齣風口4.5 m處齣現的噴幅最寬為3.56 m,與同功率下的未加擴幅噴筒的風送式噴霧機最大噴幅2.29 m相比,噴幅擴大瞭55.46%。
풍송식분무궤분통결구적불동,영향기류장적분포급분폭적대소,해문제출재원유적원형분통분무궤적기출상부가확폭단적방법,사동일태풍송식분무궤구유불동적분무특성。이용수치계산방법,채용RNG k-ε모형,대부가3충불동류형확폭단적분통진행료수치계산여분석。방진분석발현,분통중기류운동분위3개계단:고근풍선구역중,기류정문류상태,재주형분통여수축분통구역중,층류여문류병존,이재확폭분통중,기류존재문류병발생료류속적중신분포。기중,3충류형적분통중,재주형분통급수축분통내,I형화III형분통내기류속도적돌변구역교다,II형분통중기류속도적돌변구역교소;재확폭분통중,I형화III형분통내적문류구역교다,사득I형화III형분통효솔교저。이분통효솔고위우화목표,획득료관분폭풍송식분무궤확폭단분통적우화결구,병시제료시험양궤;이용시험양궤,대관분폭풍송식분무궤적출풍구풍속급분폭진행료실제측시。시험결과표명,채용우화후적확폭분통,재출풍구처실측적류장수거여방진결과지간적오차재-1.49%~1.91%내;관분폭풍송식분무궤분폭여송풍거리간성이차다항식변화규률,재분통축선방향상거출풍구4.5 m처출현적분폭최관위3.56 m,여동공솔하적미가확폭분통적풍송식분무궤최대분폭2.29 m상비,분폭확대료55.46%。
The distribution of flow field, efficiency and spraying swath of an air-blast sprayer were influenced by its structure and its shape of the duct outlet. In this paper, an additional expansion swath duct was subjoined to the original circular duct in order to make the same air-blast sprayer have different spray characteristics. Aiming at the high duct efficiency, three different types of wide-swath air-blast sprayer’s segment of expanding duct structure were optimized via numerical calculation and analysis of the internal flow field by using the RNG k-εmodel. The simulating results indicated that the wind flowed in the duct was divide into three stages. The air flow was turbulent near the fan area. Inside the cylindrical duct and contraction duct, the air flow was not only layered but also turbulent. Moreover, in the expanding duct, the air flow was turbulent and the wind speed distributed renewed. Furthermore, the areas where air flow velocity change suddenly in type I and type III ducts were larger than that of type II duct. In the expanding duct, the turbulent area were also larger in type I and type III ducts, and that leaded this two types duct efficiency was more less than that of type II duct. The air flow total pressure at inlet and outlet, the air flow average speed and the duct efficiency were simulated. The optimized structure of expansion swath duct was obtained and the testing prototype was manufactured based on the numerical calculation results. The wind speed at the outlet and the swath of wide-swath air-blast sprayer were tested and measured via prototype test. The test results showed that the error between measuring and simulating of the flow field was within -1.49% to 1.91%. The relationship between spraying swath and blast distance of wide-swath air-blast sprayer appears to be quadratic polynomial. The widest spraying swath measured away from the outlet 4.5m along the duct axial direction was 3.56 m. Compared with the same power air-blast sprayer without segment of expanding duct, the swath of the wide-swath air-blast sprayer was expanded by 55.46%. The errors between numerical calculation and actual measurement were within the engineering tolerated values. The numerical calculation model, boundary conditions, numerical calculation hypothesis, and the methods what selected in this paper can meet the requirement of engineering numerical calculation.