燃气涡轮试验与研究
燃氣渦輪試驗與研究
연기와륜시험여연구
GAS TURBINE EXPERIMENT AND RESEARCH
2014年
5期
49-52
,共4页
邹品文%程婷%韩小曼%张伟%罗畅敏
鄒品文%程婷%韓小曼%張偉%囉暢敏
추품문%정정%한소만%장위%라창민
燃气涡轮起动机%燃油泵调节器%起动加速供油特性%改进方法%占空比%特性曲线
燃氣渦輪起動機%燃油泵調節器%起動加速供油特性%改進方法%佔空比%特性麯線
연기와륜기동궤%연유빙조절기%기동가속공유특성%개진방법%점공비%특성곡선
gas turbine starter%fuel pump regulator%starting and acceleration fuel supply characteristics%improved method%duty ratio%characteristic curve
燃油泵调节器供油特性的优劣,直接关系到航空发动机能否可靠工作和充分发挥性能。某燃气涡轮起动机燃油泵调节器,为满足用户使用要求,需改变其起动加速供油特性。主要通过增加数控模块,利用其控制器和传感器来实现信号的反馈与匹配,再通过放油实现脉宽调制电磁阀对流量的修正,从而实现对燃油泵调节器起动加速供油特性的修正。最后通过试验验证了改进方法的可行性。
燃油泵調節器供油特性的優劣,直接關繫到航空髮動機能否可靠工作和充分髮揮性能。某燃氣渦輪起動機燃油泵調節器,為滿足用戶使用要求,需改變其起動加速供油特性。主要通過增加數控模塊,利用其控製器和傳感器來實現信號的反饋與匹配,再通過放油實現脈寬調製電磁閥對流量的脩正,從而實現對燃油泵調節器起動加速供油特性的脩正。最後通過試驗驗證瞭改進方法的可行性。
연유빙조절기공유특성적우렬,직접관계도항공발동궤능부가고공작화충분발휘성능。모연기와륜기동궤연유빙조절기,위만족용호사용요구,수개변기기동가속공유특성。주요통과증가수공모괴,이용기공제기화전감기래실현신호적반궤여필배,재통과방유실현맥관조제전자벌대류량적수정,종이실현대연유빙조절기기동가속공유특성적수정。최후통과시험험증료개진방법적가행성。
Fuel pump regulator is the core member of aircraft engines;its fuel properties are directly relat-ed towhether the engine can operate reliably and make engine performance into full play. Based on a gas tur-bine starter fuel regulator for the research, the improved method of starting and acceleration fuel characteris-tics of the product was explained. Mainly through the method of pulse-width modulation (PWM) solenoid valve, the starting fuel supply characteristics were modified. The feedback and matching of signal were real-ized by its controller and sensor. And the feasibility of improvement method was validated by test.