Nose-wheel steering system of aircraft
A front wheel turning and aircraft technology, applied in the field of aeronautical engineering, can solve the problems of large size, unstable turning control, poor scalability, etc., and achieve the effect of small size, high safety and compact structure
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[0017] The present invention is a kind of digital fly-by-wire front wheel steering system, which will be described in further detail below.
[0018] Functional block diagram and composition connection diagram of the present invention are respectively as figure 1 and figure 2 shown. The system includes: a turning control box 1, a command sensor 2, a combined hydraulic valve 3, a turning actuator 4, a feedback sensor 5 and auxiliary components such as cable connecting lines and hydraulic pipelines.
[0019] The turning control box 1 is fixed in the electrical equipment cabin of the aircraft with bolts, and is connected with the command sensor 2, the combined hydraulic valve 3 and the feedback sensor 5 through cable lines, and introduces power switch, turning button and wheel load switch signals. One end of the command sensor 2 is fixed under the floor of the aircraft cockpit with bolts, and the other end is hinged with the pedals by bolts to ensure that the command sensor and...
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