Method and device for audible warning when an aircraft autopilot is deactivated
An autopilot, sound alarm technology, applied in the direction of instruments, non-electric variable control, position/direction control, etc., can solve the problems of harmful aircraft flight, not knowing the autopilot, etc.
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[0021] exist figure 1 In a preferred embodiment depicted in , the aircraft acoustic warning device 1 according to the invention comprises first means 10 for monitoring the failure of the aircraft's autopilot and second means 12 for activating the sounding of the alarm in the cockpit. The first device 10 is connected via a link 20 to the autopilot 2 of the aircraft. Autopilot 2 communicates its activation / deactivation status to first device 10 via link 20 . This link 20 may be, for example, a digital data link. The first device 10 monitors the status of the autopilot and, upon detection of a change from an activated state to a disabled state, notifies the second device 12 of this change via eg a link 22 .
[0022] After the second device 12 receives the following information from the first device 10, that is, the autopilot 2 has switched from the activated state to the disabled state, it will figure 2 The instant t=0 depicted initiates the first sound with intensity I1. To...
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