推进技术
推進技術
추진기술
JOURNAL OF PROPULSION TECHNOLOGY
2015年
4期
629-634
,共6页
高明%郭晓燕%邹美帅%杨荣杰
高明%郭曉燕%鄒美帥%楊榮傑
고명%곽효연%추미수%양영걸
铝/镁合金%水反应金属燃料%固相产物%一次燃烧%二次燃烧
鋁/鎂閤金%水反應金屬燃料%固相產物%一次燃燒%二次燃燒
려/미합금%수반응금속연료%고상산물%일차연소%이차연소
Al-Mg alloy%Hydro-reactive metal fuel%Solid products%Primary combustion%Secondary com-bustion
为了探索在水冲压发动机中高金属含量铝/镁合金水反应金属燃料的稳态燃烧,开展了其一次燃烧和二次燃烧实验研究,其中铝/镁合金含量达到80%。采用氧弹量热仪收集一次燃烧固相产物,并将一次燃烧固相产物置于水蒸气高温管式炉中模拟二次燃烧。采用TGA对铝、镁和铝/镁合金进行了热性能分析,并采用XRD,SEM及化学分析方法对铝/镁合金和推进剂的一、二次燃烧固相产物进行了表征。结果表明,铝/镁合金的启动氧化温度530℃优于镁的600℃,铝/镁合金在第二阶段的氧化性能优于铝的。铝/镁合金为Mg17Al12,一次燃烧固相产物中主要存在MgAl,Mg2Al3,MgAl2等合金相和MgO,在二次燃烧的固相产物中有MgO,Al和Al2MgO4,其中剩余Al的含量随着管式炉温度增大先增大后减小。分析认为铝/镁合金在燃烧过程中镁先行发生了反应,而后其中的铝才发生反应。
為瞭探索在水遲壓髮動機中高金屬含量鋁/鎂閤金水反應金屬燃料的穩態燃燒,開展瞭其一次燃燒和二次燃燒實驗研究,其中鋁/鎂閤金含量達到80%。採用氧彈量熱儀收集一次燃燒固相產物,併將一次燃燒固相產物置于水蒸氣高溫管式爐中模擬二次燃燒。採用TGA對鋁、鎂和鋁/鎂閤金進行瞭熱性能分析,併採用XRD,SEM及化學分析方法對鋁/鎂閤金和推進劑的一、二次燃燒固相產物進行瞭錶徵。結果錶明,鋁/鎂閤金的啟動氧化溫度530℃優于鎂的600℃,鋁/鎂閤金在第二階段的氧化性能優于鋁的。鋁/鎂閤金為Mg17Al12,一次燃燒固相產物中主要存在MgAl,Mg2Al3,MgAl2等閤金相和MgO,在二次燃燒的固相產物中有MgO,Al和Al2MgO4,其中剩餘Al的含量隨著管式爐溫度增大先增大後減小。分析認為鋁/鎂閤金在燃燒過程中鎂先行髮生瞭反應,而後其中的鋁纔髮生反應。
위료탐색재수충압발동궤중고금속함량려/미합금수반응금속연료적은태연소,개전료기일차연소화이차연소실험연구,기중려/미합금함량체도80%。채용양탄량열의수집일차연소고상산물,병장일차연소고상산물치우수증기고온관식로중모의이차연소。채용TGA대려、미화려/미합금진행료열성능분석,병채용XRD,SEM급화학분석방법대려/미합금화추진제적일、이차연소고상산물진행료표정。결과표명,려/미합금적계동양화온도530℃우우미적600℃,려/미합금재제이계단적양화성능우우려적。려/미합금위Mg17Al12,일차연소고상산물중주요존재MgAl,Mg2Al3,MgAl2등합금상화MgO,재이차연소적고상산물중유MgO,Al화Al2MgO4,기중잉여Al적함량수착관식로온도증대선증대후감소。분석인위려/미합금재연소과정중미선행발생료반응,이후기중적려재발생반응。
In order to explore the steady-state combustion of high-metal Al-Mg alloy hydro-reactive metal fuels for water ramjet engines,experiments were conducted to study the primary combustion and the secondary combustion of propellant with the Al-Mg alloy content 80%.Oxygen bomb calorimeter was used to collect the sol?id products of primary combustion.The secondary combustion was simulated in the high temperature tube furnace by using the solid products of primary combustion and water vapor.Thermal performance of Al,Mg and Al-Mg al?loy was analyzed by thermogravimetric analysis(TGA).The solid products were characterized by using scanning electron microscopy(SEM),x-ray diffraction(XRD),chemical analysis method.TGA traces in air indicate that the oxidation onset temperature(530℃)of Al-Mg alloy powders is lower than that(600℃)of Mg and the oxida?tion performance of Al-Mg alloy powders is better than that of Al in case II.There were MgO,MgAl,Mg2Al3, MgAl2 produced by Mg17Al12 in the primary combustion. There were MgO,Al and Al2MgO4 in the products of sec?ondary combustion.The content of residual aluminum increases with the increasing of temperature of the tube fur?nace,and then decreases.It is thought that the combustion of magnesium in Al-Mg alloy occurs first and the com?bustion of aluminum happens later.