WO2022006905A1 - 一种分离式飞机保护装置、方法及系统 - Google Patents

一种分离式飞机保护装置、方法及系统 Download PDF

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Publication number
WO2022006905A1
WO2022006905A1 PCT/CN2020/101460 CN2020101460W WO2022006905A1 WO 2022006905 A1 WO2022006905 A1 WO 2022006905A1 CN 2020101460 W CN2020101460 W CN 2020101460W WO 2022006905 A1 WO2022006905 A1 WO 2022006905A1
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WIPO (PCT)
Prior art keywords
aircraft
protection device
detachable
protection
separate
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PCT/CN2020/101460
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English (en)
French (fr)
Inventor
曹庆恒
Original Assignee
曹庆恒
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Publication date
Application filed by 曹庆恒 filed Critical 曹庆恒
Priority to CN202080001214.4A priority Critical patent/CN111936388A/zh
Priority to PCT/CN2020/101460 priority patent/WO2022006905A1/zh
Publication of WO2022006905A1 publication Critical patent/WO2022006905A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • A62C3/07—Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles
    • A62C3/08—Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes
    • B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes

Definitions

  • the present invention relates to the technical field of aviation safety equipment, in particular to a separate aircraft protection device, method and system.
  • the main purpose of the present invention is to provide a separate aircraft protection device, a method and a system, and to realize a separate aircraft protection device and system by utilizing the unmanned aerial vehicle technology. Landing provides protection, reduces the possibility of aircraft crash, improves aircraft safety, and reduces personal and property damage caused by flight accidents.
  • the present invention provides a detachable aircraft protection device, comprising: the protection device and a UAV flight module, a fixed module and a control module respectively connected to the protection device;
  • the protection device is used to protect the aircraft
  • the unmanned aerial vehicle flight module is used for enabling the separate aircraft protection device to fly in the air;
  • the fixing module is used for fixing the separate aircraft protection device in a suitable position of the aircraft;
  • the control module is used to control the entire separate aircraft protection device.
  • the protection device is a buffer device
  • the buffer device includes a casing and one or more buffer air cushions and a rapid inflation device located in the casing.
  • the protection device is a parachute device
  • the parachute device includes a casing, a parachute and an ejection device inside the casing.
  • the protection device is a landing gear device
  • the landing gear device includes a bracket and a roller connected to each other, and also includes a shock absorber installed on the bracket and a roller installed on the roller. on the brake.
  • the protection device is a fire extinguishing device, which is used for extinguishing fire when the aircraft catches fire.
  • the protection device is composed of two or more devices in the buffer device, the parachute device, the landing gear device, and the fire extinguishing device.
  • the aircraft breaks down, according to the distress conditions and For forced landing conditions, choose the appropriate device to protect the aircraft.
  • the detachable aircraft protection device further includes a positioning device for acquiring the position information of the detachable aircraft protection device.
  • the detachable aircraft protection device further comprises a communication module for sending and receiving data.
  • the detachable aircraft protection device as described above, the detachable aircraft protection device further comprises a mechanical arm for repairing or dismantling a faulty component of the aircraft.
  • the detachable aircraft protection device can also provide auxiliary power for the aircraft through the UAV flight module to help the aircraft keep flying.
  • the present invention also provides an aircraft protection method of the above-mentioned detachable aircraft protection device, the method comprising:
  • the detachable aircraft protection device is flown to a suitable position on the aircraft and fixed in that position;
  • the present invention also provides an aircraft protection system comprising a server and one or more separate aircraft protection devices as described above,
  • the server formulates an aircraft protection scheme according to the aircraft alarm information, and mobilizes one or more separate aircraft protection devices to cooperate to complete the aircraft landing protection.
  • a detachable aircraft protection device, method and system of the present invention comprises: a protection device and a UAV flight module, a fixed module and a control module respectively connected to the protection device.
  • the aircraft protection method of the detachable aircraft protection device includes: receiving an aircraft alarm; the detachable aircraft protection device flies to a suitable position of the aircraft and is fixed at the position; and starts the protection device to protect the aircraft from landing.
  • the aircraft protection system includes a server and one or more separate aircraft protection devices as described above, the server formulates an aircraft protection plan according to the aircraft alarm information, and mobilizes one or more separate aircraft protection devices to cooperate to complete the aircraft landing protection.
  • the separate aircraft protection device, method and system of the present invention provide protection for the landing of the aircraft through the separate aircraft protection device when the aircraft breaks down, reduce the possibility of the aircraft crashing, improve the safety of the aircraft, and reduce the Personal and property damage caused by a flight accident.
  • FIG. 1 is a schematic diagram of a detachable aircraft protection device according to the first embodiment of the present invention.
  • FIG. 2 is a method flowchart of an aircraft protection method of a separate aircraft protection device according to a second embodiment of the present invention.
  • FIG. 3 is a system block diagram of an aircraft protection system according to a third embodiment of the present invention.
  • FIG. 1 is a schematic diagram of a detachable aircraft protection device according to the first embodiment of the present invention.
  • a detachable aircraft protection device of the present invention includes: a protection device 11 , a UAV flight module 12 , a fixing module 13 and a control module 14 respectively connected to the protection device 11 .
  • the protection device 11 is used to protect the aircraft
  • the unmanned aerial vehicle flight module 12 is used for enabling the separate aircraft protection device to fly in the air;
  • the fixing module 13 is used for fixing the detachable aircraft protection device in a suitable position of the aircraft;
  • the control module 14 is used to control the entire split aircraft protection device.
  • the detachable aircraft protection device of the present invention utilizes the unmanned aerial vehicle technology to realize a detached aircraft protection device.
  • the detachable aircraft protection device flies to a suitable position of the aircraft and is fixed with the aircraft, and then according to the situation activates the protective device to provide protection to the aircraft.
  • the separated aircraft protection device of the present invention may further include a positioning device and a communication module.
  • the positioning device is used for acquiring the position information of the separate aircraft protection device
  • the communication module is used for sending and receiving data.
  • the detachable aircraft protection device obtains the current position information through the positioning device, and then obtains the position information of the aircraft through the communication module, and then according to its own position information and the position information of the aircraft, as well as the parts that need to be connected and fixed to the aircraft, it is planned by the control module 14.
  • the flight line of the separate aircraft protection device itself. It can also obtain its own flight line directly through the communication module, fly to the corresponding position of the aircraft according to the flight line, connect and fix it, and then activate the protection device to protect the aircraft from landing.
  • the detachable aircraft protection device may also include an image sensor for obtaining real-time imagery.
  • the aircraft may need a separate aircraft protection device to protect its landing in the event of a failure, the aircraft may not be able to control its own flight trajectory well in the event of a failure. Since the change of the flight trajectory of the aircraft will cause the flight line of the separate aircraft protection device to change accordingly, so as to ensure that the separate aircraft protection device can fly to the corresponding position of the aircraft. Therefore, when the flight trajectory of the aircraft changes, it is necessary to re-plan the flight path of the separate aircraft protection device itself.
  • the protection device 11 may be one of a buffer device, a parachute device, a landing gear device, and a fire extinguishing device, or it may be composed of two or more devices. Distress conditions and forced landing conditions, select the appropriate separate aircraft protection device to protect the aircraft. It is also possible that a plurality of identical or different separate aircraft protection devices cooperate to protect the aircraft from landing.
  • the buffer device preferably adopts an inflatable air cushion, which plays a buffering role and prevents the aircraft from violently colliding with the ground during the landing process, resulting in the crash of the aircraft. submerged in water.
  • the cushioning device may include a housing and one or more cushioning air cushions and rapid inflation devices located within the housing.
  • the casing is used for accommodating the cushion air cushion and the rapid inflation device, and has a protective effect on the cushion air cushion and the rapid inflation device.
  • the shell is provided with an opening, the cushioning air cushion includes an inflation port, and the rapid inflation device includes an inflation tube.
  • the cushioning air cushion is inflated to form a rectangular air cushion, and the middle of the air cushion is concave to form a buffer zone, which produces resistance to the original airflow, changes the airflow to form a vortex, reduces the impact force, and prevents the aircraft from being too large due to the impact force. Hit the ground to cause an explosion.
  • the cushioning device may include one cushioning air cushion or a plurality of cushioning air cushions.
  • the buffer device can also use other equipment and materials that can play a role in buffering and protection, such as the shell of anti-collision foam, the shell of high strain rate sensitive material, the shell of auxetic polymer material, or the mixture of the two, such as the shell of Armourgel material, etc.
  • the present invention is not limited.
  • the buffer device may also include a foam generating device, which generates a large amount of foam after the plane is forced to land, so as to reduce the risk of fire and explosion of the plane.
  • the buffer device may also include a refrigeration device, which sprays refrigerant after the plane is forced to land, so as to prevent the plane from catching fire and exploding.
  • the protection device 11 can also be a parachute device, which is used to provide buoyancy when the aircraft lands, protect the aircraft from landing, and prevent the aircraft from crashing.
  • the parachute device includes a housing and a parachute and ejection device located inside the housing.
  • the shell is used to store the parachute and protect the parachute from damage in peacetime.
  • the shell is provided with an ejection opening. When the parachute device is used, the ejection opening of the shell is opened, and the ejection device ejects the parachute to the outside of the shell, and the parachute opens to provide buoyancy for the aircraft.
  • the opening of the parachute is to open the parachute at a suitable altitude and timing according to the weight of the aircraft/flight altitude/flight attitude/actual impact caused by the failure.
  • the detachable aircraft protection device may also include a height measuring device, which can measure the actual height of the detachable aircraft protection device and send it to the control module 14, and the control module 14 controls the parachute device to open the parachute at a suitable height.
  • parachutes of different specifications can be used according to different sizes/weights of the aircraft. It is also possible to use multiple separate aircraft protection devices to protect the aircraft from landing through multiple parachutes. A plurality of separate aircraft protection devices are respectively fixed to the appropriate positions of the aircraft.
  • the control module 14 controls the parachute device to be at a suitable height, and at the same time or in a certain order, the parachute is opened to provide enough for the aircraft. Buoyancy, allowing the plane to land safely.
  • the protection device 11 can also be a landing gear device, the landing gear device includes a bracket and a roller connected to each other, and also includes a shock absorber mounted on the bracket and a roller mounted on the roller. on the brake.
  • the detachable aircraft protection device of the present invention can fly to the lower part of the aircraft through the UAV flight module 12 to a position suitable for connecting the landing gear, and pass the fixing module 13 Attached and fixed in place on the aircraft to provide additional landing gear for the aircraft, enabling the aircraft to land safely.
  • the separated aircraft protection device of the present invention can be a single separated aircraft protection device or a plurality of separated aircraft protection devices to provide additional landing gear devices for the aircraft according to the actual situation of the aircraft landing gear failure.
  • the detachable aircraft protection device with the landing gear device can not only be used as the landing gear when the aircraft is landing, but also can be used as the shared landing gear of the aircraft without landing gear or the aircraft with the landing gear failure, helping the aircraft to take off from the ground.
  • the separated aircraft protection device further includes an engine for providing power, so that the separated aircraft protection device can carry the aircraft to travel on the ground. After the aircraft leaves the ground, the detachable aircraft protection device separates from the aircraft and returns automatically.
  • This detachable aircraft protection device with a landing gear device can be widely used as a shared landing gear for take-off and landing of aircraft. Through this device, the aircraft can be changed to a non-landing gear aircraft. Support and movement, including run-up before takeoff and braking after landing, can be completed by this device. Before the aircraft lands, the device flies close to the target aircraft through the UAV device and is connected and fixed with the aircraft through the fixing device. When landing, the landing gear on the device replaces the original aircraft's own landing gear to support and dampen , deceleration, taxiing on the runway, moving and stopping. When the aircraft takes off, the landing gear of the device plays the role of the original aircraft landing gear, helping the aircraft to move and accelerate.
  • the device After the aircraft takes off and leaves the ground, the device separates from the aircraft and flies according to the relevant tasks through the UAV device.
  • the combined flight method of an aircraft without a landing gear and a separate aircraft protection device with a landing gear device can greatly reduce the flight weight of the aircraft at high altitudes, save a lot of fuel and aircraft space, and reduce flight costs.
  • the device can be a landing gear with both front wheels and main wheels, or two or more devices to replace the front wheels and main wheels respectively, or the aircraft itself has a front wheel.
  • the landing gear device replaces the role of the main wheel.
  • the protection device 11 can also be a fire extinguishing device, which is used for extinguishing fire when the aircraft catches fire.
  • the fire-extinguishing device is preferably a device capable of launching dry powder fire-extinguishing bombs, and other fire-extinguishing devices such as water guns and foams can also be used, which is not limited in the present invention.
  • the fire extinguishing device includes a magazine, a launcher, and a loader.
  • the magazine is equipped with a plurality of fire-extinguishing bombs, the launcher is used for launching the fire-extinguishing bombs, and the bomb loader is used for loading the fire-extinguishing bombs into the launcher.
  • the separate aircraft protection device with fire extinguishing device flies to the vicinity of the aircraft, obtains the image of the aircraft through the image sensor, analyzes and finds the fire position by the control module 14, and controls the UAV flight module 12 to fly to a position suitable for fire fighting, and the control module 14 Control the fire extinguishing device to put out the fire.
  • the image sensor acquires the aircraft image and sends it to the server through the communication module, the server analyzes and finds the fire position, and transmits corresponding instructions through the communication module, and the control module 14 controls the UAV flight module 12 to fly to a position suitable for fire fighting according to the instructions. , extinguished by fire extinguishing device.
  • the UAV flight module 12 is used to enable the detachable aircraft protection device to fly in the air.
  • the UAV flight module 12 may be a rotor-type structure/flying-wing structure/rocket-type structure, etc., or may be other structures that facilitate flight.
  • the UAV flight module 12 adopts a rotor-type structure, with 6 rotors in total, which are respectively connected to the casing of the protection device 11 through connecting arms.
  • the connecting arms can be fixed or retractable and adjustable. .
  • the number of rotors of the UAV flight module 12 may also be other numbers, which are not limited in the present invention.
  • the UAV flight module 12 can be separated from other parts of the detachable aircraft protection device and land on its own. This prevents the UAV flight module 12 from being damaged during the landing of the aircraft, so that the UAV flight module 12 can be used multiple times, and the use cost of the separate aircraft protection device is reduced.
  • the separate aircraft protection device may include two or more groups of control modules and communication modules as required, so that after the UAV is separated, the protection device and the UAV are completed separately. instruction.
  • the fixing module 13 is used to fix the separate aircraft protection device in a suitable position of the aircraft.
  • the fixing module 13 can be connected and fixed by various tools, such as fixing cables/fixing rods/fixed link hooks/fixed locks/electromagnetic suction cups/negative pressure suction cups, etc.
  • the aircraft fuselage or wings may also have corresponding
  • the fixing device is used to connect and fix the fixing module 13 .
  • the fixed module 13 is automatically connected to the aircraft, and can also be connected through remote control. Specifically, it can be through video positioning, satellite positioning, radar positioning, electromagnetic positioning, preset positions or other positioning methods. Corresponding fixtures on the wings are attached and secured.
  • the image sensor of the detachable aircraft protection device can acquire real-time images, so that the detachable aircraft protection device can accurately fly to the corresponding position of the aircraft, and is fixed at a suitable position of the aircraft through the fixing module 13 .
  • the breakaway aircraft protection device of the present invention may also include a robotic arm for repairing or dismantling a failed component of the aircraft. For example, if there is a crack in the aircraft fuselage, the crack can be repaired by the mechanical arm to eliminate the fault; or the aircraft part is on fire and cannot be extinguished, and the fault can be eliminated by removing the part by the mechanical arm.
  • the detachable aircraft protection device of the present invention can also provide auxiliary power for the aircraft through the UAV flight module 12 to help the aircraft keep flying.
  • auxiliary power for example: for an aircraft with 4 engines, if one of the engines fails, one or more separate aircraft protection devices can be used to connect the appropriate positions of the aircraft, and the separate aircraft protection devices can provide auxiliary power for the aircraft to help the aircraft maintain Normal, balanced flight.
  • the detachable aircraft protection device can also carry an additional power source, enabling the detachable aircraft protection device to provide more power, or to provide power for a longer period of time.
  • the actions of maintenance, protection, assisting takeoff, assisting landing, providing auxiliary power or sharing the landing gear taken by the separated aircraft protection device of the present invention include the process of approaching the target aircraft, connecting and fixing, and the use of the protection device , it can be completed by the control module 14 automatically commanding and controlling the separate aircraft protection device, or it can get in touch with the aircraft or remote server through the communication module, and transmit the relevant pictures and data collected by the image sensor to the aircraft or remote server.
  • remote operators can command and control the separate aircraft protection device to complete the relevant actions, or the remote server/artificial intelligence can command and control the separate aircraft protection device to complete the relevant actions according to the relevant process.
  • FIG. 2 is a method flowchart of an aircraft protection method of a separate aircraft protection device according to a second embodiment of the present invention.
  • the aircraft protection method of a separate aircraft protection device of the present invention includes:
  • S3 Activate the protection device according to the actual situation to protect the aircraft from landing.
  • the aircraft protection method of a detachable aircraft protection device of the present invention is based on a detachable aircraft protection device of the present invention, and their structural features correspond one-to-one. Reference can be made to the description of the aforementioned detachable aircraft protection device. No longer.
  • FIG. 3 is a system block diagram of an aircraft protection system according to a third embodiment of the present invention.
  • an aircraft protection system includes a server 1 and more than one separate aircraft protection device 2 as described in the first embodiment of the present invention.
  • the server 1 formulates an aircraft protection plan according to the aircraft alarm information, and mobilizes one or more separate aircraft protection devices 2 to cooperate to complete the aircraft landing protection.
  • the detachable aircraft protection device of the present invention can be matched with different devices such as a buffer device, a parachute device, a landing gear device, a fire extinguishing device, etc., to realize different aircraft protection functions. According to the actual situation of the aircraft, one or more separate aircraft protection devices with the same function or different functions can be called to provide protection for the aircraft together.
  • a plurality of separate aircraft protection devices 2 are used jointly under the guidance of the server 1 to provide protection for the aircraft.
  • the server 1 formulates an aircraft protection plan according to the aircraft alarm information.
  • the aircraft protection plan includes: calling the type/quantity of the separate aircraft protection devices, the task target/target position/flight route of each separate aircraft protection device, and the protection of each separate aircraft.
  • the cooperation method/activation timing of the device may also include whether the estimated protection effect is achieved after the aircraft protection scheme is activated, and further measures to be taken if the protection effect is not achieved.
  • one or more separate aircraft protection devices 2 establish a connection with the aircraft through respective communication modules, and one or more separate aircraft protection devices 2 are manually controlled by the pilot or automatically by the aircraft system to provide protection for the aircraft.
  • one of the separate aircraft protection devices directs the plurality of separate aircraft protection devices to jointly provide protection for the aircraft.
  • the detachable aircraft protection device of the present invention can be stored on the ground, such as airports or other places prone to aircraft accidents, or a separate isolation bin or interlayer can be provided on the aircraft, where the detachable aircraft protection device is stored,
  • the aircraft fails or a nearby aircraft fails, the aircraft opens the isolation compartment or the mezzanine, and the separate aircraft protection device flies out of the isolation chamber or mezzanine to protect the current aircraft or the nearby faulty aircraft from landing.
  • the present invention provides a detachable aircraft protection device, method and system.
  • the detachable aircraft protection device includes: a protection device and a UAV flight module, a fixed module and a control module respectively connected thereto.
  • the aircraft protection method of the detachable aircraft protection device includes: receiving an aircraft alarm; the detachable aircraft protection device flies to a suitable position of the aircraft and is fixed at the position; and starts the protection device to protect the aircraft from landing.
  • the aircraft protection system includes a server and one or more separate aircraft protection devices as described above, the server formulates an aircraft protection plan according to the aircraft alarm information, and mobilizes one or more separate aircraft protection devices to cooperate to complete the aircraft landing protection.
  • the separate aircraft protection device, method and system of the present invention provide protection for the landing of the aircraft through the separate aircraft protection device when the aircraft breaks down, reduce the possibility of the aircraft crashing, improve the safety of the aircraft, and reduce the Personal and property damage caused by a flight accident.

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  • Aviation & Aerospace Engineering (AREA)
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Abstract

一种分离式飞机保护装置、方法及系统，分离式飞机保护装置包括：保护装置（11）和分别与其连接的无人机飞行模块（12）、固定模块（13）和控制模块（14）。分离式飞机保护装置的飞机保护方法包括：接到飞机报警；分离式飞机保护装置飞至飞机适合位置并固定在该位置；启动保护装置，保护飞机降落。飞机保护系统包括服务器（1）和一个或一个以上如上所述的分离式飞机保护装置（2），所述服务器根据飞机报警信息制定飞机保护方案，调动一个或一个以上分离式飞机保护装置协同完成飞机着陆保护。在飞机发生故障时，通过分离式飞机保护装置来对飞机着陆提供保护，降低飞机坠毁的可能性，提高了飞机的安全性，减轻了飞行事故所导致的人身和财产损失。

Description

一种分离式飞机保护装置、方法及系统 技术领域
本发明涉及航空安全设备技术领域，特别是涉及一种分离式飞机保护装置、方法及系统。
背景技术
随着航空业的发展，机场分布范围不断扩大，飞机的保有量越来越多，利用率也越来越高，乘坐飞机已经成为人们出行的重要选择。随着技术的进步，飞机的故障率已经大幅降低了，但是，由于飞机飞行环境的特殊性，导致一旦发生故障，就可能造成灾难性的后果。
因而如何保证在飞机发生故障的情况下，仍然能够安全着陆，避免造成机毁人亡的恶劣后果，成为世界各国都十分重视的问题。随着无人机技术的不断进步，利用无人机技术实现一种分离式的飞机保护装置及系统，在飞机发生故障时，通过分离式飞机保护装置来对飞机着陆提供保护，降低飞机坠毁的可能性，具有非常重要的价值及意义。
发明内容
本发明的主要目的是：提供分离式飞机保护装置、方法及系统，利用无人机技术实现一种分离式的飞机保护装置及系统，在飞机发 生故障时，通过分离式飞机保护装置来对飞机着陆提供保护，降低飞机坠毁的可能性，提高了飞机的安全性，减轻了飞行事故所导致的人身和财产损失。
为实现上述目的，本发明提供了一种分离式飞机保护装置，包括：保护装置和分别与其连接的无人机飞行模块、固定模块和控制模块；
所述保护装置用于对飞机起到保护作用；
所述无人机飞行模块用于使所述分离式飞机保护装置能够在空中飞行；
所述固定模块用于将所述分离式飞机保护装置固定在飞机的适合位置；
所述控制模块用于控制整个分离式飞机保护装置。
如上所述的分离式飞机保护装置，所述保护装置为缓冲装置，所述缓冲装置包括壳体以及位于壳体内的一个或一个以上缓冲气垫和快速充气装置。
如上所述的分离式飞机保护装置，所述保护装置为降落伞装置，所述降落伞装置包括外壳以及位于外壳内部的降落伞和弹出装置。
如上所述的分离式飞机保护装置，所述保护装置为起落架装置，所述起落架装置包括相互连接的支架和滚轮，还包括安装在所述支架上的减震器以及安装在所述滚轮上的制动器。
如上所述的分离式飞机保护装置，所述保护装置为灭火装置，用于在飞机起火时灭火。
如上所述的分离式飞机保护装置，所述保护装置由缓冲装置、降落伞装置、起落架装置、灭火装置中的2个或2个以上装置组合而成，在飞机发生故障时，根据遇险条件和迫降条件，选择适合的装置保护飞机。
如上所述的分离式飞机保护装置，所述分离式飞机保护装置还包括定位装置，用于获取所述分离式飞机保护装置的位置信息。
如上所述的分离式飞机保护装置，所述分离式飞机保护装置还包括通讯模块，用于发送和接收数据。
如上所述的分离式飞机保护装置，所述分离式飞机保护装置还包括机械臂，用于维修或拆卸所述飞机发生故障的部件。
如上所述的分离式飞机保护装置，所述分离式飞机保护装置，还能通过所述无人机飞行模块为飞机提供辅助动力，帮助飞机保持飞行。
本发明还提供一种如上所述的分离式飞机保护装置的飞机保护方法，所述方法包括：
接到飞机报警；
分离式飞机保护装置飞至飞机适合位置并固定在该位置；
根据实际情况启动保护装置，保护飞机降落。
本发明还提供一种飞机保护系统，所述系统包括服务器和一个或一个以上如上所述的分离式飞机保护装置，
所述服务器根据飞机报警信息制定飞机保护方案，调动一个或一个以上分离式飞机保护装置协同完成飞机着陆保护。
本发明的一种分离式飞机保护装置、方法及系统，分离式飞机保护装置包括：保护装置和分别与其连接的无人机飞行模块、固定模块和控制模块。分离式飞机保护装置的飞机保护方法包括：接到飞机报警；分离式飞机保护装置飞至飞机适合位置并固定在该位置；启动保护装置，保护飞机降落。飞机保护系统包括服务器和一个或一个以上如上所述的分离式飞机保护装置，所述服务器根据飞机报警信息制定飞机保护方案，调动一个或一个以上分离式飞机保护装置协同完成飞机着陆保护。本发明的一种分离式飞机保护装置、方法及系统，在飞机发生故障时，通过分离式飞机保护装置来对飞机着陆提供保护，降低飞机坠毁的可能性，提高了飞机的安全性，减轻了飞行事故所导致的人身和财产损失。
附图说明
图1为本发明第一实施例一种分离式飞机保护装置的示意图。
图2为本发明第二实施例一种分离式飞机保护装置的飞机保护方法的方法流程图。
图3为本发明第三实施例一种飞机保护系统的系统框图。
具体实施方式
为进一步阐述本发明达成预定目的所采取的技术手段及功效，以下结合附图及实施例，对本发明的具体实施方式，详细说明如下。
本发明第一实施例参阅图1。图1为本发明第一实施例一种分离式飞机保护装置的示意图。如图所示，本发明的一种分离式飞机保护装置包括：保护装置11和分别与其连接的无人机飞行模块12、固定模块13和控制模块14。
保护装置11用于对飞机起到保护作用；
无人机飞行模块12用于使所述分离式飞机保护装置能够在空中飞行；
固定模块13用于将所述分离式飞机保护装置固定在飞机的适合位置；
控制模块14用于控制整个分离式飞机保护装置。
本发明的分离式飞机保护装置，是利用无人机技术实现一种分离式的飞机保护装置，在飞机发生故障时，分离式飞机保护装置飞至飞机适合位置并与飞机固定在一起，然后根据情况启动保护装置，对飞机提供保护。
本发明的分离式飞机保护装置，还可以包括定位装置和通讯模块。定位装置用于获取所述分离式飞机保护装置的位置信息，通讯模块用于发送和接收数据。分离式飞机保护装置通过定位装置获取当前的位置信息，再通过通讯模块获取飞机的位置信息，再根据自 身位置信息和飞机的位置信息，以及需要连接固定至飞机的部位，由控制模块14规划出分离式飞机保护装置自身的飞行线路。也可以是通过通讯模块直接获得自身的飞行线路，按照飞行线路飞至飞机的相应位置并连接固定，然后启动保护装置保护飞机降落。分离式飞机保护装置还可以包括图像传感器，用于获取实时影像。
在本发明中，因为飞机可能是在发生故障的情况下，需要分离式飞机保护装置来保护其降落，因而飞机在故障情况下很可能已经不能很好的控制自身的飞行轨迹了。由于飞机飞行轨迹的改变会导致分离式飞机保护装置的飞行线路也要相应的发生变化，才能保证分离式飞机保护装置飞至飞机的相应位置。所以，在飞机的飞行轨迹发生变化的情况下，需要重新规划分离式飞机保护装置自身的飞行线路。
在本发明中，保护装置11可以是由缓冲装置、降落伞装置、起落架装置、灭火装置中的1个，也可以是由2个或2个以上装置组合而成，在飞机发生故障时，根据遇险条件和迫降条件，选择适合的分离式飞机保护装置保护飞机。还可以是多个相同的或不同的分离式飞机保护装置协同保护飞机着陆。
缓冲装置优选采用充气气垫，起到缓冲作用，防止飞机着陆过程中与地面剧烈碰撞，导致机毁人亡，采用充气气垫作为缓冲装置还可以在飞机在水面迫降时起到保护作用，并且防止飞机沉入水中。
缓冲装置可以包括壳体以及位于壳体内的一个或一个以上缓冲气垫和快速充气装置。所述壳体用于收纳缓冲气垫和快速充气装置，并对缓冲气垫和快速充气装置起到保护作用。壳体设有开口，缓冲 气垫包括充气口，快速充气装置包括充气管，当保护装置11启用时，壳体开口打开，缓冲气垫落到壳体外部，快速充气装置的充气管插入缓冲气垫的充气口，快速向缓冲气垫充气。
在本实施例中，缓冲气垫充气后形成一个长方体气垫，气垫中部内凹，形成一个缓冲区，对原有气流产生阻力，使气流发生改变形成涡流，减少冲击力，防止飞机因冲击力过大撞击地面引发爆炸。在本发明中，缓冲装置可以包括1个缓冲气垫也可以包括多个缓冲气垫。
缓冲装置也可以采用其他能够起到缓冲保护作用的设备和材料，如防撞泡沫的外壳、应变率高敏感材料外壳、拉胀高分子材料外壳或者是两者的混合体如Armourgel材料外壳等，本发明不做限制。缓冲装置还可以包括泡沫发生装置，在飞机迫降后产生大量泡沫，降低飞机着火、爆炸的危险。缓冲装置还可以包括制冷装置，在飞机迫降后喷洒制冷剂，防止飞机着火、爆炸。
本发明的分离式飞机保护装置，保护装置11还可以是降落伞装置，用于在飞机降落时提供浮力，保护飞机降落，防止飞机坠毁。所述降落伞装置包括外壳以及位于外壳内部的降落伞和弹出装置。外壳用于收纳降落伞，并在平时保护降落伞不受损坏，外壳设有弹出口，当降落伞装置使用时，外壳的弹出口打开，弹出装置将降落伞弹出到外壳外部，降落伞打开，为飞机提供浮力。降落伞打开是根据飞机的重量/飞行高度/飞行姿态/故障造成的实际影响等情况，在适合的高度及时机打开降落伞。分离式飞机保护装置还可以包括高度测量设备，能够测量分离式飞机保护装置的实际高度，发送至控制模块14，控制模块14控制降落伞装置在适合的高度打开降落 伞。在本发明中，可以根据飞机的不同大小/重量，采用不同规格的降落伞。也可以是采用多个分离式飞机保护装置，通过多个降落伞来保护飞机降落。多个分离式飞机保护装置，分别固定至飞机的适合位置，根据通讯模块接收到的指令，由控制模块14控制降落伞装置在适合的高度，同时或者按照一定的顺序打开降落伞，为飞机提供足够的浮力，使飞机能够安全降落。
本发明的分离式飞机保护装置，保护装置11还可以是起落架装置，所述起落架装置包括相互连接的支架和滚轮，还包括安装在所述支架上的减震器以及安装在所述滚轮上的制动器。当飞机的起落架发生故障或飞机不包括起落架时，本发明的分离式飞机保护装置，可以通过自身的无人机飞行模块12飞至飞机的下部适合连接起落架的位置，通过固定模块13连接并固定在飞机合适的位置，为飞机提供额外的起落架装置，使飞机能够安全降落。本发明的分离式飞机保护装置，根据飞机起落架故障的实际情况，可以是单个分离式飞机保护装置，也可以是多个分离式飞机保护装置为飞机提供额外的起落架装置。在本发明中，带有起落架装置的分离式飞机保护装置不仅可以在飞机降落时作为起落架，还可以作为无起落架飞机或起落架故障的飞机的共享起落架，帮助飞机从地面起飞。此时，分离式飞机保护装置还包括用于提供动力的发动机，使分离式飞机保护装置能够承载飞机在地面行驶。飞机飞离地面后，分离式飞机保护装置与飞机分离，自动返回。
这种带有起落架装置的分离式飞机保护装置可以作为共享式起落架广泛的应用于飞行器的起飞、降落，通过这种装置，飞机可以改为无起落架飞机，无起落架飞机在地面的支撑、移动包括起飞前 的助跑和落地后的刹车，可以由该装置完成。在飞机降落前，该装置通过无人机装置在空中飞行靠近目标飞机并通过固定装置与飞机连接固定，落地时由该装置上的起落架代替原有飞机自身起落架，起到支撑、减震、减速、在跑道滑行、移动以及停机的作用。飞机起飞时，该装置的起落架起到原有飞机起落架的作用，帮助飞机的移动、加速，待飞机起飞离开地面后，该装置与飞机脱离，并通过无人机装置按相关任务飞行。这种无起落架飞机与带有起落架装置的分离式飞机保护装置联合飞行的方式，可以大幅降低飞机在高空的飞行重量，节约大量燃油和飞机空间，降低飞行成本。飞机使用这种装置替代起落架时，该装置可以是同时带有前轮和主轮的起落架，也可以是两个以上装置分别替代前轮和主轮，也可以是飞机自身带有前轮而起落架装置替代主轮的作用。
本发明的分离式飞机保护装置，保护装置11还可以是灭火装置，用于在飞机起火时灭火。在本实施例中，灭火装置优选为可发射干粉式灭火弹的装置，也可以采用水枪、泡沫等其他方式的灭火装置，本发明不作限制。所述灭火装置包括弹仓、发射器、上弹器。所述弹仓中装有多个灭火弹，所述发射器用于将灭火弹发射出去，所述上弹器用于将灭火弹上到发射器中。带有灭火装置的分离式飞机保护装置飞至飞机附近，通过图像传感器获取飞机图像，由控制模块14分析找到着火位置，并控制无人机飞行模块12飞至适合灭火的位置，由控制模块14控制灭火装置灭火。也可以是图像传感器获取飞机图像后通过通讯模块发送至服务器，由服务器分析找到着火位置，并通过通讯模块传输相应指令，由控制模块14按照指令控制无人机飞行模块12飞至适合灭火的位置，由灭火装置灭火。
无人机飞行模块12用于使所述分离式飞机保护装置能够在空中飞行。在本发明中，无人机飞行模块12可以是旋翼式结构/飞翼式结构/火箭式结构等，也可以是其他利于飞行的结构。如图1所示，无人机飞行模块12采用旋翼式结构，共有6个旋翼，分别通过连接臂连接在保护装置11的外壳上，连接臂可以是固定的，也可以是可伸缩可调节的。无人机飞行模块12的旋翼数量也可以是其他数量，本发明不作限制。在本发明中，分离式飞机保护装置的保护装置11通过固定模块13固定在飞机上后，无人机飞行模块12就可以与分离式飞机保护装置的其他部分分离，自行降落。这就避免在飞机着陆过程中，无人机飞行模块12受到损伤，从而使无人机飞行模块12可以多次利用，降低了分离式飞机保护装置的使用成本。所述分离式飞机保护装置在无人机飞行模块可以分离的实现方式中，根据需要可以包括两组及以上控制模块、通讯模块，以实现无人机分离后，保护装置与无人机分别完成指令。
在本发明中，固定模块13用于将所述分离式飞机保护装置固定在飞机的适合位置。固定模块13可以是由各种工具实现连接及固定，如固定索/固定杆/固定链结钩/固定锁扣/电磁吸盘/负压吸盘等，飞机机身或机翼上也可以有相应的固定装置用于与固定模块13连接并固定。固定模块13是自动连接飞机，也可以通过远程操控实现连接，具体可以是通过视频定位、卫星定位、雷达定位、电磁定位、预先设定位置或其他定位方式，使固定模块13与飞机机身或机翼上相应的固定装置连接并固定。分离式飞机保护装置的图像传感器，能够获取实时影像，使分离式飞机保护装置能够精准的飞至飞机的相应位置，通过固定模块13固定在飞机的适合位置。
本发明的分离式飞机保护装置还可以包括机械臂，用于维修或拆卸所述飞机发生故障的部件。例如：飞机机身出现裂缝，可以通过机械臂修补该裂缝来消除故障；或者是飞机部件着火又不能扑灭，通过机械臂将该部件拆除来消除故障。
本发明的分离式飞机保护装置，还可以通过所述无人机飞行模块12为飞机提供辅助动力，帮助飞机保持飞行。例如：拥有4个发动机的飞机，其中一个发动机发生故障，则可以通过一个或多个分离式飞机保护装置，连接都飞机适合的位置，通过分离式飞机保护装置为飞机提供辅助动力，帮助飞机保持正常、平衡的飞行。执行辅助飞行任务时，分离式飞机保护装置还可以携带额外的动力源，使分离式飞机保护装置能够提供更大的动力，或者更长时间提供动力。
本发明的分离式飞机保护装置对飞机所采取的维修、保护、协助起飞、协助降落、提供辅助动力或共享起落架的行动，包括与目标飞机靠近，连接固定的过程，以及对保护装置的使用，可以是由控制模块14自动指挥控制分离式飞机保护装置完成，也可以是通过通讯模块与飞机或远程服务器取得联系，将图像传感器采集的相关画面及数据传输至飞机或远程服务器，相关由飞行员或远程操作人员进行指挥控制分离式飞机保护装置完成相关行动，还可以是由远程服务器/人工智能根据相关流程指挥指挥控制分离式飞机保护装置完成相关行动。
本发明第二实施例参阅图2。图2为本发明第二实施例一种分离式飞机保护装置的飞机保护方法的方法流程图。如图所示，本发明的一种分离式飞机保护装置的飞机保护方法包括：
S1：接到飞机报警；
S2：分离式飞机保护装置飞至飞机适合位置并固定在该位置；
S3：根据实际情况启动保护装置，保护飞机降落。
本发明的一种分离式飞机保护装置的飞机保护方法是基于本发明的一种分离式飞机保护装置的，它们结构特征一一对应，可以参照前述一种分离式飞机保护装置的说明，在此不再赘述。
本发明第三实施例参阅图3。图3为本发明第三实施例一种飞机保护系统的系统框图。如图所示，一种飞机保护系统包括服务器1和超过一个如本发明第一实施例所述的分离式飞机保护装置2。
服务器1根据飞机报警信息制定飞机保护方案，调动一个或一个以上分离式飞机保护装置2协同完成飞机着陆保护。
本发明的分离式飞机保护装置，可以搭配不同的装置如：缓冲装置、降落伞装置、起落架装置、灭火装置等等，实现不同的飞机保护功能。还可以根据飞机的实际情况，调用一个或多个相同功能或不同功能的分离式飞机保护装置，一起为飞机提供保护。
多个分离式飞机保护装置2在服务器1的指导下联合使用，为飞机提供保护。服务器1根据飞机报警信息制定飞机保护方案，飞机保护方案包括：调用分离式飞机保护装置的种类/数量、每个分离式飞机保护装置的任务目标/目标位置/飞行路线、每个分离式飞机保护装置的配合方式/启用时机，还可以包括启用飞机保护方案后是否达到预估的保护效果、以及未达到保护效果需要采取的进一步措施等等。也可以是一个或多个分离式飞机保护装置2通过各自的通 讯模块与飞机建立连接，由飞行员人工或飞机系统自动控制一个或多个分离式飞机保护装置2为飞机提供保护。还可以是多个分离式飞机保护装置2通过各自的通讯模块相互建立连接后，由其中的一个分离式飞机保护装置指挥所述的多个分离式飞机保护装置联合为飞机提供保护。
本发明的分离式飞机保护装置，可以存放在地面，如机场或其他易发生飞机事故的地方，也可以是在飞机上设有单独的隔离仓或夹层，将分离式飞机保护装置存放在这里，当飞机发生故障时或附近的飞机发生故障时，飞机打开所述的隔离仓或夹层，分离式飞机保护装置飞出隔离仓或夹层，保护当前飞机或附近发生故障的飞机降落。
综上所述，本发明的一种分离式飞机保护装置、方法及系统，分离式飞机保护装置包括：保护装置和分别与其连接的无人机飞行模块、固定模块和控制模块。分离式飞机保护装置的飞机保护方法包括：接到飞机报警；分离式飞机保护装置飞至飞机适合位置并固定在该位置；启动保护装置，保护飞机降落。飞机保护系统包括服务器和一个或一个以上如上所述的分离式飞机保护装置，所述服务器根据飞机报警信息制定飞机保护方案，调动一个或一个以上分离式飞机保护装置协同完成飞机着陆保护。本发明的一种分离式飞机保护装置、方法及系统，在飞机发生故障时，通过分离式飞机保护装置来对飞机着陆提供保护，降低飞机坠毁的可能性，提高了飞机的安全性，减轻了飞行事故所导致的人身和财产损失。
以上所述的具体实施方式，对本发明的目的、技术方案和有益效果进行了进一步详细说明，所应理解的是，以上所述仅为本发明 的具体实施方式而已，并不用于限定本发明的保护范围，凡在本发明的精神和原则之内，所做的任何修改、等同替换、改进等，均应包含在本发明的保护范围之内。

Claims (12)

  1. 一种分离式飞机保护装置，其特征在于，所述分离式飞机保护装置包括：保护装置和分别与其连接的无人机飞行模块、固定模块和控制模块；
    所述保护装置用于对飞机起到保护作用；
    所述无人机飞行模块用于使所述分离式飞机保护装置能够在空中飞行；
    所述固定模块用于将所述分离式飞机保护装置固定在飞机的适合位置；
    所述控制模块用于控制整个分离式飞机保护装置。
  2. 根据权利要求1所述的分离式飞机保护装置，其特征在于：所述保护装置为缓冲装置，所述缓冲装置包括壳体以及位于壳体内的一个或一个以上缓冲气垫和快速充气装置。
  3. 根据权利要求1所述的分离式飞机保护装置，其特征在于：所述保护装置为降落伞装置，所述降落伞装置包括外壳以及位于外壳内部的降落伞和弹出装置。
  4. 根据权利要求1所述的分离式飞机保护装置，其特征在于：所述保护装置为起落架装置，所述起落架装置包括相互连接的支架和滚轮，还包括安装在所述支架上的减震器以及安装在所述滚轮上的制动器。
  5. 根据权利要求1所述的分离式飞机保护装置，其特征在于：所述保护装置为灭火装置，用于在飞机起火时灭火。
  6. 根据权利要求1所述的分离式飞机保护装置，其特征在于：所述保护装置由缓冲装置、降落伞装置、起落架装置、灭火装置中的2个或2个以上装置组合而成，在飞机发生故障时，根据遇险条件和迫降条件，选择适合的装置保护飞机。
  7. 根据权利要求1-6中任一权利要求所述的分离式飞机保护装置，其特征在于：所述分离式飞机保护装置还包括定位装置，用于获取所述分离式飞机保护装置的位置信息。
  8. 根据权利要求1-6中任一权利要求所述的分离式飞机保护装置，其特征在于：所述分离式飞机保护装置还包括通讯模块，用于发送和接收数据。
  9. 根据权利要求1-6中任一权利要求所述的分离式飞机保护装置，其特征在于：所述分离式飞机保护装置还包括机械臂，用于维修或拆卸所述飞机发生故障的部件。
  10. 根据权利要求1-6中任一权利要求所述的分离式飞机保护装置，其特征在于：所述分离式飞机保护装置，还能通过所述无人机飞行模块为飞机提供辅助动力，帮助飞机保持飞行。
  11. 一种如权利要求1-10中任一权利要求所述的分离式飞机保护装置的飞机保护方法，其特征在于，所述方法包括：
    接到飞机报警；
    分离式飞机保护装置飞至飞机适合位置并固定在该位置；
    根据实际情况启动保护装置，保护飞机降落。
  12. 一种飞机保护系统，其特征在于：所述系统包括服务器和一个或一个以上如权利要求1-10中任一权利要求所述的分离式飞机保护装置，
    所述服务器根据飞机报警信息制定飞机保护方案，调动一个或一个以上分离式飞机保护装置协同完成飞机着陆保护。
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