| 摘要 |
<p>Continuos transfer of flight data from simulated aircraft controls to control computer where data is analysed. As soon as the received data correspond to G-load, computer sends signals to squeeze G-suit. The pressure in G-suit corresponds to that experienced by pilot in real aircraft during the same G-load. When computer detects that limit aerodynamic mode has been reached, when vibrations occur, it generates signals to create vibrations of frequency and amplitude equal to those in a real aircraft flying under the same conditions of stalling. Swinging frame (2) with its rear part connected to rear hydraulic cylinder (5) through pressure piping (8), which is feeded from rear hydraulic source (6). It further features a cockpit (4) with inlet (7) connected through upper pressure piping (12) and air valve (9) to pressure air accumulator (11) with compressor (10). Aircraft cockpit (4) controls (21) combined output (21.1) is connected to control computer (20) combined input (20.1), the combined output (20.2) from control computer (20) is connected both with corresponding control input (9.1) of air valve (9) and with rear hydraulic source (6) control input (6.1).</p> |
