Safety protection system of aircraft with multiple rotor wings
A multi-rotor aircraft, safety protection technology, applied in aircraft parts, parachutes, transportation and packaging, etc., can solve the problems of unable to maintain attitude, economic loss, propeller damage, etc., to avoid loss and personal injury, reduce its own weight, and apply wide range of effects
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Embodiment 2
[0065] The difference between embodiment 2 and embodiment 1 is that the first controller in embodiment 2 is connected with multiple parachute pop-up devices in a wireless manner.
[0066] Such as Figure 12 As shown, in addition to being provided with an acceleration sensor, a three-axis gyroscope, a first controller and a relay, the safety device control circuit in Embodiment 2 is also provided with one or more wireless communication modules, which are realized through the first wireless communication module. Connection of the first controller to the parachute ejection device.
[0067] When the first controller is wirelessly connected with the parachute pop-up device 3 , a trigger device control circuit needs to be set to control the parachute pop-up device 3 . Such as Figure 13 As shown, the trigger device control circuit includes a second controller, a second wireless communication module, a discharge circuit and a power supply (not shown in the figure), and the power supp...
Embodiment 3
[0071] The difference between Embodiment 3 and Embodiment 1 is that, in the parachute ejection device 3 , the trigger mechanism 8 is omitted.
[0072] Such as Figure 14~15 As shown, the inside of the shell 7 is divided into a parachute cavity 6 above and a trigger cavity 10 below by a positioning plate 9 inside the shell 7 . Have some positioning plate air outlets 18 on the positioning plate 9, and the positioning plate air outlets 18 are sealed by wax under normal conditions. A parachute is inserted in the parachute cavity 6, and a second discharge electrode 17 is fixed in the trigger cavity 10. Same as Embodiment 1, an opening is provided at the bottom of the housing 7 , and the opening is blocked by a baffle 13 . Combustion agent is placed in the entire trigger chamber 10, and the wire 11 is connected to the second discharge electrode 17 through the opening on the side of the shell 7, and the opening on the side of the shell 7 can only allow the wire 11 to pass through. ...
Embodiment 4
[0074] Embodiment 4 differs from Embodiment 3 in that: in Embodiment 4, the bottom surface and one side of the parachute pop-up device 3 are closed, and the baffle plate 13 is arranged on the other side to block the parachute chamber 6 and the trigger chamber 10 from the side. The setting mode of positioning plate 9 is the same as that of embodiment 3. In this embodiment, the parachute pop-up device 3 is also detachably fixed on the inclined surface at the end of the fixed arm 4 .
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