航空兵器
航空兵器
항공병기
HANGKONG BINGQI
2014年
3期
36-39
,共4页
固体燃气发生器%燃气阀%姿轨控%内流场分析
固體燃氣髮生器%燃氣閥%姿軌控%內流場分析
고체연기발생기%연기벌%자궤공%내류장분석
solid propellant gas generator%hot-gas valve%divert attitude control%analysis of inter nal flow field
固体燃气阀技术是姿轨控发动机控制的关键技术之一。通过数值模拟对固体燃气阀开关状态进行内流场分析,结果表明:燃气阀两侧存在有效驱动力,能够实现阀的开启和关闭,并确定了影响驱动力的主要构型参数;同时考虑燃气阀周向间隙影响,需设法增大阀尾腔出口面积、减小间隙和增大 ds/dr ,以增大燃气阀开启力;最后对确定阀芯移动距离的原则予以说明。研究结果为后期燃气阀机理分析、设计和优化提供参考和支撑。
固體燃氣閥技術是姿軌控髮動機控製的關鍵技術之一。通過數值模擬對固體燃氣閥開關狀態進行內流場分析,結果錶明:燃氣閥兩側存在有效驅動力,能夠實現閥的開啟和關閉,併確定瞭影響驅動力的主要構型參數;同時攷慮燃氣閥週嚮間隙影響,需設法增大閥尾腔齣口麵積、減小間隙和增大 ds/dr ,以增大燃氣閥開啟力;最後對確定閥芯移動距離的原則予以說明。研究結果為後期燃氣閥機理分析、設計和優化提供參攷和支撐。
고체연기벌기술시자궤공발동궤공제적관건기술지일。통과수치모의대고체연기벌개관상태진행내류장분석,결과표명:연기벌량측존재유효구동력,능구실현벌적개계화관폐,병학정료영향구동력적주요구형삼수;동시고필연기벌주향간극영향,수설법증대벌미강출구면적、감소간극화증대 ds/dr ,이증대연기벌개계력;최후대학정벌심이동거리적원칙여이설명。연구결과위후기연기벌궤리분석、설계화우화제공삼고화지탱。
The solid propellant hot-gas valve is the key technology of diver attitude control .The in-ternal flow field of solid propellant hot-gas valve in its opened and closed condition is analyzed based on numerical simulation .It is shown that there is available driving force on both sides of the hot-gas valve to open and close the valve , and the main structure parameters of changing the driving force are gotten;The larger export and smaller gap should be made to get greater opening force .Then, the method calculates the moving distance of valve .It proposes a reference and support for the future analyses , design and opti-mization of the hot -gas valve.