摘要
根据飞机燃油油量测量的原理引出了数字式燃油测量系统中油量传感器的布局原则,由此提出了可测区的概念,并对相应的可测区计算方法中的关键技术作了阐述.最后给出了通过可测区计算及可测性验证进行油箱中油量传感器布局设计的有关结论.
The location principle of fuel sensor in digital fuel gaging system according to the principle in fuel quantity measurement is introduced.From which it presents the conception of measurable area and sets forth the key techniques in calculating it.In the end the paper provides some relative conclusions about the location design of fuel sensor in aircraft by calculating measurable area and check the measurability.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
1997年第6期783-787,共5页
Journal of Beijing University of Aeronautics and Astronautics
基金
航空科学基金
关键词
传感器
CAD
油量测量
飞机燃油
sensors
computer aided design
errors
fuel measurement