Autonomous escape type aviation black box unmanned aerial vehicle system

Abstract

The autonomous escape type aviation black box unmanned aerial vehicle system comprises an ejection system and an unmanned aerial vehicle system, the unmanned aerial vehicle system is installed on the upper portion of the ejection system, and the unmanned aerial vehicle system comprises a vehicle body, an undercarriage, sliding wheels, a temperature sensor, a camera module and a navigation beacon module; a black box is arranged in the machine body; undercarriages, a temperature sensor and a camera module are mounted at the bottom of the fuselage; a navigation beacon module is mounted at the tail of the fuselage; four arms are mounted on two sides of the fuselage, and a rotor mechanism is mounted at the outer end of each arm. The unmanned aerial vehicle system is an innovative aviation safety device and is used for rapidly deploying and guiding to a safe area through a preset program when an emergency occurs to an airplane, and the integrity and accessibility of an airplane black box are protected to the maximum extent. The design of the system considers various possible emergency situations, including high-altitude automatic pop-up, low-altitude or water surface landing scenes.

Description

Technical Field

[0001] The invention belongs to the field of unmanned aerial vehicles, and in particular relates to an autonomous escape-type aviation black box unmanned aerial vehicle system. Background Art

[0002] With the development of aviation technology, the performance and reliability of black boxes, as critical safety equipment on aircraft, have attracted widespread attention from the global aviation industry and research institutions. Although existing black box systems are carefully designed to withstand extreme shock and high temperatures, they still face a series of challenges and defects. Globally, several aviation manufacturing giants, including Boeing in the United States and Airbus in Europe, as well as regulatory agencies such as the Civil Aviation Administration of China, are promoting the advancement of black box technology. But even so, traditional black boxes may still fail in extreme accidents due to mechanical damage, fire or underwater pressure. Therefore, despite huge investment in the research and development of black box technology worldwide, the current black box system still has key defects such as damage, difficulty in rapid positioning and high data recovery costs. The existence of these problems, coupled with the experience of the difficulty of recovering black boxes in several major aviation accidents in recent years, highlights the urgency of developing more advanced, reliable and efficient black box systems. Summary of the invention

[0003] Purpose of the invention: The purpose of the present invention is to provide an autonomous escaping aviation black box drone system, which can ensure the safety of the black box and facilitate the search.

[0004] Technical solution: An autonomous escape-type aviation black box drone system of the present invention comprises an ejection system and a drone system, wherein the drone system is installed on the upper part of the ejection system and can eject a passenger plane under certain conditions and deploy a drone to achieve escape flight;

[0005] The UAV system includes a fuselage, a landing gear, a sliding wheel, a temperature sensor, a camera module and a navigation beacon module; a black box is installed inside the fuselage; a landing gear, a temperature sensor and a camera module are installed at the bottom of the fuselage; a navigation beacon module is installed at the tail of the fuselage; four arms are installed on both sides of the fuselage, and a rotor mechanism is installed at the outer end of each arm.

[0006] Furthermore, the ejection system includes an ejection base, a track limit buckle, a rope tractor, an elastic rope and a T-shaped buckle from bottom to top; the rope tractor is installed behind the ejection base, the elastic rope connects the ejection base and one end of the T-shaped buckle, and the other end of the T-shaped buckle is fixed to the drone system.

[0007] Furthermore, a black box, an arm limit buckle, a power supply, and an arm drive module are installed inside the fuselage.

[0008] Furthermore, the power supply and arm drive module are installed below the black box.

[0009] Furthermore, the number of the arm limit buckles is 8, which are respectively fixed at the starting point and the end point of the rotation stroke of the arm driving module.

[0010] Furthermore, airbags are installed on both sides of the landing gear.

[0011] Beneficial effects: Compared with the prior art, the present invention has the following significant advantages:

[0012] (1) The drone system of the present invention is an innovative aviation safety device that is used to quickly deploy and guide to a safe area through a preset program when an emergency occurs on an aircraft, thereby maximizing the protection of the integrity and accessibility of the aircraft's black box. The system design takes into account a variety of possible emergency situations, including high-altitude automatic ejection, low-altitude or water landing scenarios.

[0013] (2) In the event of an emergency, the black box drone system can be used to escape from the crashed aircraft, thereby protecting the integrity and findability of the aircraft's black box to the greatest extent possible. The design of the drone system takes into account a variety of possible landing scenarios, including fire escape and water landing. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the working principle of the present invention;

[0015] Figure 2 It is a schematic diagram of the main structure of the present invention;

[0016] Figure 3 It is an enlarged structural diagram of the fuselage;

[0017] Figure 4 This is an enlarged structural diagram of the ejection base.

[0018] In the figure, 1-ejection base, 2-rope tractor, 3-elastic rope, 4-T-type buckle, 5-landing gear, 6-sliding wheel, 7-airbag bag, 8-temperature sensor, 9-camera module, 10-navigation beacon module, 11-fuselage, 12-arm;

[0019] 1-1-track limit buckle, 11-1-black box, 11-2-arm limit buckle, 11-3-power supply, 11-4-arm drive module. DETAILED DESCRIPTION

[0020] The technical solution of the present invention is further described below in conjunction with the accompanying drawings.

[0021] like Figure 1As shown, the technical problem to be solved by the present invention is to provide an autonomous escape aviation black box drone system which can automatically escape from an aircraft before the aircraft crashes and ensure the safety of the black box and facilitate the search.

[0022] The present invention provides an autonomous escape-type aviation black box drone system, comprising an ejection system and a drone system, such as Figure 2-Figure 4 As shown, the UAV system is installed on the upper part of the ejection system, and can eject the passenger plane under certain conditions and deploy the UAV to achieve escape flight; the ejection system is divided into an ejection base, a rope tractor, an elastic rope and a T-shaped buckle from bottom to top, the rope tractor is installed behind the ejection base, the elastic rope connects the ejection base and the T-shaped buckle, and the T-shaped buckle is fixed on the UAV system; the UAV system includes a landing gear, a sliding wheel, an airbag bag, a temperature sensor, a camera module, a navigation beacon module and a fuselage; the sliding wheel is installed under the landing gear, the airbag bag is installed on both sides of the landing gear, the landing gear, the temperature sensor and the camera module are installed together at the bottom of the fuselage, and the navigation beacon module is installed at the tail of the fuselage; four arms are installed on both sides of the fuselage, and the outer end of each arm is installed with a rotor mechanism. The fuselage is equipped with a black box, an arm limit buckle, a power supply, and an arm drive module, wherein there are eight arm limit buckles fixed at the starting point and end point of the arm rotation stroke.

[0023] During the plane crash, the fuselage attitude sensor will send a crash alarm to the pilot. If the pilot does not cancel the alarm within 5 seconds. The black box escape system will start working, the track limit buckle on the ejection base will open immediately, and the drone system carrying the black box will fly out from the tail of the passenger plane through the traction ejection of the elastic rope, unfold the retracted arm, and rotate the propeller to take off and hover in the air. At this time, the positioning beacon will be activated, and the drone's navigation module will guide the drone to fly to the nearest land in the 120-degree horizontal fan-shaped area facing the direction of the passenger plane's crash, and confirm that there is no fire at the landing site through the temperature sensor module and visual module under the drone. After confirming that the landing site is safe, the drone will slowly descend to a height of 2.5m from the landing point and hover again. At this time, the airbag under the drone will be inflated and unfolded. After the airbag is inflated to the right position, the drone will slowly land again. If the landing point is on the water, the airbag can also act as a floating raft waiting for the rescue team to recover it.

Claims

1. An autonomous escape-type aviation black box drone system, characterized in that: It includes an ejection system and a drone system, wherein the drone system is installed on the upper part of the ejection system and can eject the passenger plane under certain conditions and deploy the drone to achieve escape flight; The unmanned aerial vehicle system comprises a fuselage (11), a landing gear (5), a sliding wheel (6), a temperature sensor (8), a camera module (9) and a navigation beacon module (10); a black box (11-1) is installed inside the fuselage (11); the landing gear (5), a temperature sensor (8) and a camera module (9) are installed at the bottom of the fuselage (11); a navigation beacon module (10) is installed at the tail of the fuselage (11); four arms (12) are installed on both sides of the fuselage (11), and a rotor mechanism (13) is installed at the outer end of each arm.

2. The autonomous escape-type aviation black box drone system according to claim 1, characterized in that: The ejection system comprises, from bottom to top, an ejection base (1), a track limit buckle (1-1), a rope tractor (2), an elastic rope (3) and a T-shaped buckle (4); the rope tractor (2) is installed behind the ejection base (1), the elastic rope (3) connects the ejection base (1) and one end of the T-shaped buckle (4), and the other end of the T-shaped buckle (4) is fixed on the UAV system.

3. The autonomous escape-type aviation black box drone system according to claim 1, characterized in that: The fuselage (11) is internally provided with a black box (11-1), an arm limit buckle (11-2), a power supply (11-3), and an arm drive module (11-4).

4. The autonomous escape-type aviation black box drone system according to claim 3 is characterized in that: The power supply (11-3) and the arm driving module (11-4) are installed below the black box (11-1).

5. The autonomous escape-type aviation black box drone system according to claim 3 is characterized in that: The number of the arm limit buckles (11-2) is 8, which are respectively fixed at the starting point and the end point of the rotation stroke of the arm drive module (11-4).

6. The autonomous escape-type aviation black box drone system according to claim 1, characterized in that: Airbags (7) are installed on both sides of the landing gear (5).

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