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Crash detection device, flying body crash detection method, parachute or paraglider deployment device, and airbag device

A detection device and technology for aircraft, applied in airbags, aircraft, parachutes, etc., can solve problems such as the risk of falling accidents of aircraft, hinder the popularization of aircraft, etc., and achieve the effect of improving reliability

Active Publication Date: 2020-05-15
NIPPON KAYAKU CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] On the other hand, the risk of crash accidents of the above-mentioned aircraft is considered to be very dangerous, hindering the popularization of the aircraft

Method used

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  • Crash detection device, flying body crash detection method, parachute or paraglider deployment device, and airbag device
  • Crash detection device, flying body crash detection method, parachute or paraglider deployment device, and airbag device
  • Crash detection device, flying body crash detection method, parachute or paraglider deployment device, and airbag device

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Embodiment Construction

[0033] Hereinafter, an aircraft to which a parachute or paraglider deployment device according to an embodiment of the present invention is applied will be described with reference to the drawings.

[0034] figure 1 It is a figure which shows an example of the aircraft to which the deployment apparatus 90 of a parachute or a paraglider is applied. Such as figure 1 As shown, the aircraft 100 has a body 1, one or more propulsion mechanisms (such as propellers, etc.) 2 combined with the body 1 and propelling the body 1, a plurality of legs 3 arranged at the bottom of the body 1, a parachute or a paraglider The deployment device 90. The deploying device 90 of the parachute or paraglider is arranged on the body 1 .

[0035] in addition, figure 2 An example of a deployment device 90 for a parachute or paraglider is shown, at figure 2 An example of a deployment device for parachute deployment is given in , which will be described below.

[0036] Such as figure 2 A parachute...

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Abstract

[Problem] To provide a crash detection device, a flying body crash detection method, a parachute or paraglider deployment device, and an airbag device capable of improving safety reliability. [Solution] This flying body crash detection device comprises: a detection unit capable of detecting the flight state of a flying body; a calculation unit capable of determining, on the basis of the flight state data for the flying body obtained by the detection unit, whether the flight state of the flying body is abnormal; and an abnormality signal output unit capable of outputting an abnormality signal to the outside if the calculation unit determines that the flight state of the flying body is abnormal. The calculation unit acquires data from the detection unit at a sampling frequency of 1 kHz or more and if the data is at least a certain preset threshold value, determines whether the data is indication of an abnormal flight state for the flying body or noise constituting unnecessary data. If the calculation unit determines the former, then the flight state of the flying body is determined to be abnormal.

Description

technical field [0001] The invention relates to a fall detection device mounted on an aircraft, a method for detecting the fall of the aircraft, a parachute or paraglider deployment device and a safety air bag device. Background technique [0002] In recent years, along with the development of autonomous control technology and flight control technology, the industrial use of aircraft with multiple rotors called unmanned aerial vehicles, for example, has been accelerated. For example, the UAV rotates a plurality of rotors in a balanced manner at the same time, ascends and descends by increasing and decreasing the number of rotations of the rotors, and advances and retreats by tilting the body by increasing and decreasing the number of rotations of the rotors. It can be predicted that this kind of aircraft will develop in the world in the future. [0003] On the other hand, the risk of crash accidents of the above-mentioned aircraft is considered to be very dangerous, which h...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D25/00B64C39/02B64D17/54
CPCB64D17/54B64D25/00B64D2201/00B64D45/06B64D17/80B64U70/83B64U20/83G05D1/0055G05D1/0066G05B23/0205B64U10/13G05D1/617G05D1/83B64C39/02
Inventor 中村博八木橋泰彦笹本幸一
Owner NIPPON KAYAKU CO LTD
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