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In order to detect whether or not this system is working properly, typically, fuel system analyzes the data of fuel quantity and pump outlet pressure signal. 6 Research of Aircraft Fuel System Feeding Failure 47 Fig. 2 Aircraft fuel system simulation model In this simulation, pressure sources stand for two engines . In Fig. 2, they are components 5, 6. Three 3-Armed Tanks, components 1, 13, 14, represent three fuel tanks. The left and right wing tanks have two boost pumps. In order to simulate fewer iterations and fast convergence, two boost pumps are fitted to one.
Wang Á L. Chen Beijing Aeronautical Technology Research Center, Beijing 100076, China B. Xu Á S. Wei Faculty of Remanufacturing Engineering, Academy of Armored Force Engineering, Beijing 100072, China J. 1007/978-3-642-54236-7_3, Ó Springer-Verlag Berlin Heidelberg 2014 19 20 X. Wang et al. With the development of science and technology, the ratio of flight accidents every 100,000 flight hours has dramatically decreased. During the past 100 years, this ratio of avion serious accidents has decreased more than 350 times, and that of civil airplane has also notably decreased, reaching two times every 100,000 flight hours.
9. This result make sure that the silicon typical absorption of oil in the failure plug. 0 cm-1 Fig. 6 Property Test and Analysis of Rubber The existence of lubrication oil in the plug obviously disobeys the rules of the plug use. How does the oil affect the rubber in the plug? What extent is it? What are the effective and practical measures which will prevent or cut down the similar faults happening? 2), evaluate the oil resistivity of rubber. DVð%Þ ¼ ðm3 À m4 þ m5 Þ À ðm1 À m2 þ m5 Þ Â 100 m1 À m2 þ m5 ð3:1Þ m3 À m1 Â 100 m1 ð3:2Þ Dmð%Þ ¼ 26 X.