Design of Anti-ice Valve with Electromagnetic Servo Control Technology

ZHANG Xiao, PEI Fei-fei

Hydraulics Pneumatics & Seals ›› 2023, Vol. 43 ›› Issue (7) : 98-103.

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Hydraulics Pneumatics & Seals ›› 2023, Vol. 43 ›› Issue (7) : 98-103. DOI: 10.3969/j.issn.1008-0813.2023.07.020
System & Application

Design of Anti-ice Valve with Electromagnetic Servo Control Technology

  • ZHANG Xiao, PEI Fei-fei
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Abstract

According to the variable flow anti-ice requirements of CR929 air craft wing anti-ice system, the variable flow anti-ice valve based on electromagnetic servo control is designed to make its anti-ice flow meeting the requirements that change with the flight altitude.

Key words

variable flow anti icing / anti-ice valve / flight altitude / design

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ZHANG Xiao, PEI Fei-fei. Design of Anti-ice Valve with Electromagnetic Servo Control Technology[J]. Hydraulics Pneumatics & Seals, 2023, 43(7): 98-103 https://doi.org/10.3969/j.issn.1008-0813.2023.07.020

References

[1] 常士楠,杨波,冷梦尧,等.飞机热气防冰系统研究[J].航空动力学报,2017,32(5):1025-1034.
[2] 丁同堂,马辰,高梅.A320系列飞机发动机防冰活门故障分析[J].科技展望,2014,(15):55,57.
[3] 刘广锋,王路瑶,袁文科.波音787飞机新型大翼防冰系统及其维护[J].航空维修与工程,2022,(7):93-95.
[4] 周家希.大型飞机防冰系统研制发展研究[J].中国战略新兴产业,2017,(24):47.
[5] 王真,蒋红娜.飞机防冰系统及其技术发展现状[J].中国科技信息,2017,(13):56-58.
[6] 李革萍,ARJ21-700飞机机翼防冰系统性能验证技术[Z].上海:中国商飞上海飞机设计研究院,2013.
[7] Yeoman K E. Efficiency of a Bleed Air Powered Inlet Icing[R]. AIAA, 94-0717,1994.

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