Conclusion When pilot is under physical examination for modification to equipment of high performance aircraft, the hearing standard of recommendation is binaural means of air conduction hearing threshold of 500, 1000, 2000, 3000Hz on audiogram≤20-25dB HL, normal function of eustachian tube and negative in the acoustic reflex decay test.
The simulation results (H=10 km, Ma=0.8/1.5) show: 1. When pilot draws link stably ((2/°s)), angle of incidenceαand plumb overladnzgradually grow until one of them oversteps the accepted value, and the joystick displacement is limited at last.
Based on the characteristics of the pitch PIO, a pilot aircraft loop model is presented in which the aircraft is described as an equivalent system model and the McRuer model is adopted as pilot handling.
In addition, the transient response was detected from the motor setup to smooth running within 10 s, 15 s, 20 s and 25 s respectively, and the characteristic of the transient flux is under pilot study.
Comparing the pilot results measured by previous methods, the relative error of the characteristics predicted by simulation is less than 30%.
With regards to the fuel cycle, a 100 t/a PWR spent fuel reprocessing pilot plant and a 500 kg/ a MOX fabrication plant are under construction.
The features of the opposed multi-burner (OMB) gasification technology, the method and process of the research, and the operation results of a pilot plant and demonstration plants have been introduced.
Through analyses of some pilot scale MTD-FGD tests, it can be concluded that in the MTD-FGD reactor, the sulfate reaction of sorbent particles is generally kinetically controlled.