CN109843721B - Search and rescue unmanned aerial vehicle arrangement - Google Patents
Search and rescue unmanned aerial vehicle arrangement Download PDFInfo
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- CN109843721B CN109843721B CN201680090107.7A CN201680090107A CN109843721B CN 109843721 B CN109843721 B CN 109843721B CN 201680090107 A CN201680090107 A CN 201680090107A CN 109843721 B CN109843721 B CN 109843721B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/20—Launching, take-off or landing arrangements for releasing or capturing UAVs in flight by another aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/20—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/82—Airborne vehicles
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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
- B64D2045/0065—Black boxes, devices automatically broadcasting distress signals
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/55—UAVs specially adapted for particular uses or applications for life-saving or rescue operations; for medical use
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Abstract
Providing a search/service rescue drone arrangement and structure, a UAV or drone called SRD (21) will permanently engage the transport and push out of its containment box (24) whenever an emergency is detected, so that the SRD (21) will track, report, locate, assist and can rescue humans or connect them to a command center without waiting for a search/rescue drone from a distance, for a passenger aircraft (20) two SRDs (21) can be installed between the tail end and the vertical wing; for a jet fighter, the SRD may be a (hover) sled 35 that directly supports the pilot or an ejector seat that supports the pilot to direct it to the appropriate landing position when the pilot is ejected into the air; for vessels, the SRD may additionally be pushed out to issue hazard lamps; for vehicles, the SRD may be a mini-drone for reporting theft or accidents while the vehicle is stationary.
Description
Technical Field
The present invention relates to unmanned or piloted mini-aircraft dedicated to the search, guidance and rescue actions of various means of transportation.
Background
Unmanned Aerial Vehicles (UAVs), also known as unmanned mini-aircraft or remotely piloted vehicles, are finding way to enter the market in recent years and will be used in numerous commercial and civilian areas in the near future. The process of imaging from thermal imaging or cameras to package delivery, agriculture, crop surveying, trick air shots in film production, search and rescue actions, construction industry, inspection of power lines, dams, pipes, calculation of wild animals and plants, provision of medical supplies to remote areas or other inaccessible areas, illegal hunting as determined by animal rights advocates, activity monitoring, wildfire mapping, pipe security, home security, road patrol, and anti-piracy, delivery of life saving tools to multiple swimmers, damage assessment, all-weather imaging through clouds, rain and fog and under day or night conditions is all performed in real time.
The unmanned aerial vehicle is also used for remote sensing tasks, and the remote sensing functions of the unmanned aerial vehicle comprise a plurality of electromagnetic spectrum sensors, gamma ray sensors, biological sensors, chemical sensors, optical sensors, infrared cameras and synthetic aperture radars.
However, the prior art does not present a drone for imaging, reporting, tracking or even searching for a wide variety of aircraft in the event of an accident in the air, nor does the prior art present a drone for vessels, yachts and boats, and therefore, does not incorporate such a vehicle to push out of the same aircraft or vessel to perform such tasks, or even perform other tasks such as fire suppression, to assist or guide other tools to the accident area in the event of an accident.
Unmanned aerial vehicles that can land on or be propelled from road vehicles can be found in the prior art, for example: motor vehicle (Motor Vehicle with Captive Aircraft) with tethered aircraft (WO 2015057832), WO2008147681, also a police drone, which is close to the accident area for imaging, reporting, communicating with the driver, is available in the prior art for road vehicles, such as police drones: w02014080388, or even a reporter drone: WO2014106814, they are still an intervention after the occurrence of an accident and are not suitable for use in aircraft or marine vessels.
Rescue drones in combination with main flights may be used in prior art applications: unmanned aerial vehicle service aircraft carrier W02014080386 contains a rescue unmanned aerial vehicle that was filed separately by application No. W02014080387, this type of unmanned aerial vehicle would be combined with an unmanned aerial vehicle aircraft carrier.
However, for manned aircraft, or pilot-loaded jet fighters, or passenger-loaded vessels, yachts, and boats, the prior art does not reveal built-in or installed mini-aircraft attached to these devices so that when these devices face an accident, the mini-aircraft can be separated from any of these devices so that they can track, search, image, report, contact rescue teams for personnel or passengers, even when an accident occurs, directly assist them or perform fire fighting processes, rather than waiting for a search and rescue drone sent from another area to delay searching and then assist other tasks.
Such permanently installed unmanned aerial vehicles are very necessary, just like car-equipped jacks, spare tires, tools, emergency reflectors, and in fact unmanned aerial vehicles are more important than car-equipped ones, since they will save authorities time to learn about the situation, to try to communicate, track, search, image and rescue workers or passengers, and without these types of unmanned aerial vehicles, all these procedures require additional time, thus delaying rescue actions, which means that personnel and machine losses will double.
In some cases, the situation is even worse, for example when an aircraft is lost in the sea or ocean, millions, tens of millions or even hundreds of millions of funds are spent searching for the aircraft or vessel, while the whole passengers and staff are never lost, without any data about what happens, nor is the black box and the location of the aircraft crash known. The prior art does not reveal any such related inventions, and the present invention discloses a number of search and rescue drones that address one of the major accident problems faced by humans during this period.
Disclosure of Invention
A built-in double search and rescue drone is provided at the top of the airliner above the empennage, which is pushed out once or one by one according to commands issued from a microprocessor that collects emergency data from sensors indicating that serious accidents, faults, falls or crashes etc. will occur.
After being pushed out, the drone will track the aircraft, perform real-time video imaging of the aircraft, in particular of any external defect, send real-time photographs to the command center, and also provide a complete map with the aircraft coordinates and landing or crash location, in addition, the drone can carry fire extinguishers to extinguish the fire, or communicate with staff or passengers with a set of mini-drones.
In another embodiment, the search and rescue drone may be mounted in a jet fighter in two positions, the first at the top above the tail wing, performing the same tasks previously described, while the second resembles a (hover) skateboard mounted under the pilot's foot, with the pilot's foot attached to the skateboard by a pair of shoes, so that when the pilot is faced with an accident and deploys his parachute, the second drone skateboard helps the pilot control the landing direction away from the enemy, mountain or jungle etc. towards a safe position.
In another embodiment, the search and rescue drone may be mounted on top of a ship, yacht, watercraft, train, tram or bus to perform the same tasks as a passenger aircraft.
Drawings
● FIG. 1-A: a three-dimensional view of a passenger aircraft with a storage location for one of the double search rescue drones is shown.
● Fig. 1-B: a three-dimensional close-up view of the storage space for one of the double search and rescue drones above the top of the passenger aircraft is shown.
● Fig. 1-C: a three-dimensional view of a storage (enclosure) space for one of the double search and rescue drones over the top of a passenger aircraft is shown.
● Fig. 1-D to 1-H: and pushing out the three-dimensional view of the steps of the search and rescue unmanned aerial vehicle from the inside of the built-in storage position of the search and rescue unmanned aerial vehicle.
● Fig. 2-a, fig. 2-B: a three-dimensional view of a search and rescue jet drone as a propeller drone is shown.
● Fig. 3-a: a three-dimensional view of a search and rescue drone carrying a fire extinguishing cylinder is shown.
● Fig. 4: a three-dimensional view of a search and rescue drone (hover skateboard) under the pilot's foot in the jet fighter cockpit is shown.
● Fig. 5-a to 5-D: a three-dimensional view of a method of deriving a search and rescue drone from a jet fighter is shown.
● Fig. 6: a three-dimensional view of a marine vehicle having a storage location for a search/rescue drone is shown.
● Fig. 7-a, fig. 7-B, fig. 7-C: two-dimensional and three-dimensional views of a road vehicle with one micro unmanned aerial vehicle (MUAV: micro unmanned aerial vehicle) built into a shark antenna box are shown.
Detailed Description
Best mode for carrying out the invention:
in order to facilitate the implementation of the invention, a detailed description of the components of the invention supported by the figures is provided herein, in which the main components are arranged in order according to the importance of the components, so that it is easy to read in terms of numbers contained in the component description text and the component number list by referring to each feature, where the number of a component feature is represented sequentially starting from the number 20, to which the required number will be assigned directly each time a component feature is presented in the text. Taking fig. 1 as an example, the component features are arranged sequentially from the numerals 20, 21, 22. In addition, the search and rescue drone or the service rescue drone will be denoted as SRD.
Passenger aircraft SRD:
in order to provide SRD 21 to guest 20, there are many obstacles that will face and should be addressed:
1. since it is important that the SRD 20 is not pushed out so as to strike the body of the aircraft 20, the location of the housing or storage location of the SRD is inevitably such that the SRD 21 is positioned near the top of the aircraft tail 22 near the rear vertical wing 23, from where pushing out the SRD will cause it to exit behind the aircraft body (figures 1-a to 1-B).
Number of srds 21: the dual SRD 21 is selected such that one is positioned to the right of the vertical wing 23 and one is positioned to the left of the vertical wing 23 over the tail 22, which arrangement and positioning will maintain symmetry of the main body of the aircraft 20 side-to-side.
3. Shape of the housing box 24: for newly manufactured aircraft 20, the tanks 24 can be built into the fuselage interior at the above-mentioned locations, whereas for aircraft that are already commercially available and equipped with such techniques for search work, it is advisable to install the containment tanks 24 so that the shape of the latter should not disrupt the aerodynamics of the aircraft 20, which means that they should be proportioned, smoothly curved towards the rear and from right to left, without rough edges. The preferred shape is a jet fighter cockpit canopy where the vertical wing 23 divides the containment box 24 of the dual SRD 21 into two similar and symmetrical sections (fig. 1-C).
4. Door 25 of containing box 24: the door 25 should not be of a swinging type, as high speed, sonic or supersonic air flow may damage it or prevent it from closing, and the air swirl of the flight may also make it difficult to close, the most preferred type being a collapsible door 25 that does not swing outside the containment box 24, a collapsible door 25 that can be folded up and closed directly down after pushing out the SRD 21 (fig. 1-D).
5. Internal structure of the housing case 24:
a. since the most preferred push-out direction of the SRD 21 is 30-45 ° from the horizon to avoid striking any part of the rear side of the fuselage, the platform 26 on which the SRD 21 rests should be inclined away from the vertical wing 23 and up so that the push-out of the SRD 21 will cause it to follow a track that is approximately 30-45 ° up and 30-45 ° from horizontal (fig. 1-E).
b. The folding door 25 should be opened (folded) by pulling it upward conventionally according to a driving motor, and closed (unfolded) by pushing it downward according to the same motor.
The SRD is not free inside the containment box 24 but needs to be attached in a conventional way, but without any obstruction that would hinder its ejection, wherein the SRD can be ejected by guiding it towards the door 25, as shown in fig. 1-C, wherein the SRD is ejected by its own force, or it needs to be guided in the opposite way but in the same direction as the aircraft 20, such that when the pressure of the force pressing the plate 28 against the spring 27 by the tension of the electromagnetic arm 29 is released, by releasing the spring 27 loaded under tension, said pressure, once released, will release the pressure from the spring 27, which will push back the plate 28, pushing the SRD 21 outwards (fig. 1-F to 1-H).
The wiring of the srd 21 housing 24 should be connected by any conventional electrical and electronic circuitry to a microprocessor that gathers data concerning all types of hazards and emergency situations faced by the aircraft 20, such as: sudden speed changes, engine failure, fuel leakage, wing damage, internal smoke, sending emergency information, losing communication with the aircraft, terrorist attacks, etc. The microprocessor may automatically derive the SRD 21 based on pre-installed program operational data based on such data.
The SRD 21 also collects the same data that will be forwarded to the black box of the aircraft 20 so that it is stored in the memory of the SRD 21 and transferred to the aviation center after the SRD 21 is pushed out, or later retrieved.
Push out time for srd 21: any aircraft 20 facing an emergency will not necessarily fall directly, nor crash in the air at a height of 10,000 meters, with a fatal accident of 10.0% at climb, 8.0% at cruise, and 4.0% at descent, meaning that nearly 22.0% of the fatal accidents occur at high altitudes, and nearly 50.0% occur at take-off, last approach or landing, meaning that half of the fatal accidents occur at low altitudes, and about 28.0% at medium altitudes, such statistics indicate that since the aircraft fatal accidents do not occur primarily at high altitudes, but crash accidents occur primarily at low altitudes, this low in accident occurrence will provide a suitable environment for the SRD 21 to be pushed out, since the SRD 21 will operate at such low altitudes, while the speed of the aircraft 20 will be reduced, which will facilitate the SRD 21 to follow the aircraft 20.
However, even at low altitudes, it is difficult for the propeller unmanned aerial vehicle to track the aircraft 20, however, the virginia manufacturer Aurora Flight Sciences, specializing in advanced UAV systems, is pushing the outer shell of the UAV design by cooperating with Stratasys to create world-first-frame jet-powered three-dimensional print UAV aircraft, prototyping to 150MPH, which exceeds the take-off, landing or last approach speed of the aircraft, although further developments would make such UAVs suitable for tracking aircraft at lower altitudes.
Fortunately, methods and systems for determining and verifying the current physical and geographical location of a network device in an emergency situation using emergency messages containing traditional 911, E911 and text to 911 messages from an Unmanned Aerial Vehicle (UAV) or drone have been available in the art and are available from US20150140954; a method and system (Method and System For an Emergency Location Service) entitled "emergency positioning services".
Pushing out SRDs 21 from emergency data unnecessarily ensures that the aircraft 20 will inevitably fail, while keeping the push-out delay of SRDs 21 unbiased until ensuring that the aircraft is experiencing a complete crash, in order to separate these problems, two SRDs 21 are selected for each airliner so that they are pushed out separately, wherein the first SRD is pushed out according to a program set in a microprocessor that issues a command to perform a first push out to get a first view of the aircraft 20 from outside and sends the view directly as a live report to the aviation center with all other data, it may happen that the aircraft 20 does not fall within 10 minutes or within 100km, the aircraft 20 may fly farther, or even be approaching a position close to the airport, in which case the first SRD 21 cannot track the aircraft so long that it is meaningless to use only one SRD 21, the second SRD 21 should remain in the aircraft 20 and will be pushed out later on when one of the following conditions occurs:
a. when the microprocessor program is manipulating the data, it follows that an extreme emergency situation will occur with the aircraft 20 and that the indicator shows that the aircraft 20 will inevitably fall or crash.
b. If the situation is not very bad and still controllable, the push of the second SRD 21 will be paused, but it should be pushed out at the last approach of the aircraft 20 in order to provide a real-time video report from behind it, for a number of reasons: an aircraft may accidentally crash during the last approach phase, it may crash upon landing, etc., it may be very advantageous to the airline hub to provide all data about the aircraft 20 during the last approach or landing of the aircraft 20, so that all preparation work is done from a real-time report of the situation behind the aircraft 20.
This argument does not mean that the SRD 21 should be pushed out over a long time interval, in case of a severe emergency in which the aircraft 21 is about to crash or explode or has exploded, the push out of two SRDs 21 can be performed at a time.
Jet fighter 34:
the first SRD 21 for search and rescue may be mounted in any suitable location on the underside, with the same housing structure and method of operation as mentioned in the present invention for the airliner, the SRD may be pushed out of the interior of the build-in chamber, or dropped into the interior of a container that opens to release the SRD after dropping, or by enclosing the SRD inside a projector or booster for later pushing out of the Unmanned Aerial Vehicle (UAV) from the projector or booster interior.
The second SRD would be a service and rescue drone that would take on special tasks and have high jet power, a suitable SRD that can be selected from the prior art under the name of flyboard Air 35, or Jetpack/Hoverboard, assigned to Frank Zapata, which pushed the first field demonstration through the You tube and Zapata rating website, but no patent is disclosed for this invention.
This is an air propelled version that obtained a ginis record of the furthest flight through the suspension board at month 2016. Zapata states that depending on the internal four engines at power of 250hp each, up to 10,000 feet can be flown, up to 150km/h, and 10 minutes of operation can be achieved. Totaling 1000hp, which enables the skateboard to carry a person weighing approximately 200 pounds, the skateboard 35 is sized to be approximately 55.0cm in length, 45.0cm in width and 35.0cm in height.
1. if the pilot 40 is at an unsuitable altitude to open the parachute 41 after aerial ejection, the sled 35 can save the pilot's life, can be accomplished simply by actuating the sled, does not require long distance, high altitude and long time periods to fully operate and maneuver as the parachute 41 does, can be run directly, and can be controlled to safely lower the pilot in its selected proper position.
2. If the pilot 40 is highly fitted after the aerial ejection he opens the parachute 41, but he finds that the area is unsuitable for landing when moving downwards, for example on rivers, steep mountains, enemy areas, etc., the pilot can control his aircraft 41 to move him away from these unsuitable landing environments.
In another embodiment, the ejector seat may be loaded directly onto the sled, as shown in fig. 5-D, which means that the driver will not land on both feet, but on the ejector seat, which may be beneficial to the pilot in case of injury.
It is apparent here that some inventors may require that the skateboard be used instead of the parachute for a pilot sitting in an ejector seat, while the parachute is placed on standby, where the inventors ensure that this is obvious to them.
Marine, railway and road vehicles:
the transportation means include marine vessels, yachts 42 and ships, rail trains and trams, road buses and trucks. For these vehicles, one SRD 21 (service and rescue drone) may be installed over any center of the rear flat and horizontal portion of fig. 6. For the same aerodynamic reasons mentioned, the shape of the containment tank 24 may be similar to the shape of a jet fighter roof. The size of the SRD 21 and thus the size of its containment box 24 may be selected according to the size and area of use of the vehicle. The ejector mechanism internal structure is the same for the passenger aircraft SRD 21. The task to be performed by SRD 21 is to send a real-time video presentation of any incident or emergency situation to a particular command center to determine the location of the incident, and if at night, to send an emergency (hazard) warning light to the location of the incident and an alarm from impacting an idle vehicle, and if there is a fire, to conduct a fire extinguishing task, to contact the command sender with the survivor to evaluate the situation and evaluate the personnel and materials required to rescue the survivor.
Road vehicle:
while the prior art also shows that pushing out certain types of drones from road vehicles, it is very dangerous to push out such drones when the vehicle is moving on the road and about to encounter an accident, because these drones are uncontrolled when pushing out in a congested road, they may hit any vehicle from behind, causing a new accident, while if the drone is pushed out sideways it may hit other passing vehicles or hit trees, bridges, traffic lights/posts or pedestrians, thus providing 4WD and Salon vehicles would be limited to mini-drones 43 within the containment box 24 which would push out when the vehicle is stationary or only when started by the driver or command center knowing that the car is sending an emergency message, so these mini-drones would have the following design and task in the road vehicle:
1. the task of the drone 43 will be limited to an anti-theft system such that when the car is parked, the thief tries to open the door or window hard, the anti-theft system pushes out the drone 43 to send the real-time video presentation of the thief to the car owner's smart phone and the nearest police department, as shown in fig. 7-a.
2. The containment box 24 should be mounted in place of a shark antenna (rear side of roof top) and have a cockpit roof shape for aerodynamic reasons, as shown in fig. 7-B, 7-C.
3. The housing box 24 should be as small as possible to accommodate the antenna and one micro-drone 43 within it.
4. The pushing out of the micro-drone 43 should be the same as the SRD 21 in the passenger aircraft, but should be pushed out vertically upwards of 1.0 to 1.5 meters.
5. If a thief tries to cover the receiving box of the micro-drone 43, the sensor should detect and the alarm system is activated.
6. In an emergency situation, only the driver or a command center in the police department may push out the micro-drone 43 when the vehicle is stationary, which will be pushed up 1.0 to 1.5 meters to provide a real-time report on the emergency situation.
Note that:
it should be noted that it is fully obvious to the inventors of the present invention that the connection of the slide 35 carrying a person above it to the parachute 41 as a tool will cause other inventors to require the invention of a new system to perform specific tasks based on this design (slide+person+parachute) = (slide+person+tool) so that the inventors can put any of the other inventions into this arrangement and then claim them as a true invention, so that the inventors wish here to ensure that he uses this arrangement for:
1. a person sits on a chair and flies in the air with the support of a bottom slide, using the tools and process mentioned in the following international patent applications to clean surfaces: WO2013108141, WO2013190397, WO2014037821
2. Police officers stand or sit attached to skateboards and carry tools for traffic control or accident control tasks, such as the tools claimed in the following applications: WO2014080388
3. Tools for facade cleaning when mounted directly on a skateboard, such as the tools claimed in the following applications: WO2013076711, WO2013076712
4. A person stands or sits attached to the skateboard and carries a tool for extinguishing a fire, such as a fire extinguishing cylinder or similar tool as claimed in the following application: WO2014080385
5. A person stands or sits attached to the skateboard and carries means for real-time video reporting, media interview: WO2014106814
6. Two persons perform facade cleaning within a netpen supported by two or more skids by means of the tools claimed in the following applications, or any similar maintenance of high-altitude facades, construction sites, power lines, industrial sites which are not accessible without the use of a crane: WO2013105001
Note-2:
the arrangement or arrangement of pilot's safety ejection seat 38 from its bottom to hover sled 35 by search/service and rescue (UAV/drone) 21 may be applied to many civilian services, particularly but not limited to: fire fighting in high rise buildings, facade cleaning or maintenance, high rise industrial structure maintenance, police action, etc. or further, it may be connected to similar seats and housed inside the canopy to provide a safe means of transportation.
Note-2:
it should be noted that it is fully apparent to the inventors of the present invention that an SRD carrying a fire suppression cartridge will lead other inventors to invent a new system to perform specific tasks based on this design by providing a full time drone carrying a fire suppression cartridge at specific areas around the building or tower facade or even inside thereof, which directly starts when a fire is detected, approaches an apartment or office in fire 10 to 30 minutes earlier than civil defence, and enters by e.g. breaking a window glass with a front metal protrusion, etc., and starts fire suppression work, providing a complete real time video report to the command center.
Industrial applicability:
1. unmanned aerial vehicle search, service and Rescue (SRD) is made of available tools, components, mechanisms, and can be modified appropriately.
2. (SRD) can save lives, materials and money for a variety of uses in civilian and military applications.
3. The fabrication of the containment box shapes simply uses available successfully aerodynamic shaped tools and develops them to accommodate the current area of use.
4. The push-out mechanism depends on the available tools that are arranged and modified to accommodate the current area of use.
Component diagram index:
20. a passenger aircraft.
21. search/Service Rescue Drone (SRD).
22. An aircraft tail.
23. A vertical wing.
24. A containing box.
25. And (3) a door.
26. A platform.
27. And (3) a spring.
28. A plate.
29. Electromagnetic switch + arm.
30. A turbine powered UAV.
31. Unmanned propeller.
32. And a propeller.
33. A fire extinguishing cylinder.
34. Jet fighter plane.
35. And (3) a sliding plate.
36. A boot.
37. And a cockpit.
38. Ejecting the seat.
39. Roof board.
40. And (3) a pilot.
41. A parachute.
42. Yacht.
43. And the miniature unmanned plane.
Claims (1)
1. A search and rescue unmanned aerial vehicle arrangement suitable for a passenger aircraft, comprising: two search and rescue unmanned aerial vehicles, one is positioned on the right side of the vertical wing, the other is positioned on the left side of the vertical wing above the empennage, and the arrangement and the positioning ensure that the main body of the passenger plane is left and right symmetrical, and the search and rescue unmanned aerial vehicle comprises an airplane empennage; a vertical wing;
the accommodating box is positioned in the accommodating box, the accommodating box adopts a proportional shape similar to a top awning of a cockpit for aerodynamic reasons, the vertical wing divides the accommodating box of the searching and rescuing unmanned aerial vehicle into a left part and a right part which are similar and symmetrical, the accommodating box is provided with a rear folding door, the folding door is folded upwards and unfolded, and after the searching and rescuing unmanned aerial vehicle is pushed out by self force, the folding door is directly closed downwards, the method comprises the steps that a plate is pressed to a spring through release or due to the tensile force of an electromagnetic arm, so that the spring generates pressure, the plate is pushed back through release of the pressure of the spring loaded under the tensile force of the electromagnetic arm, and therefore the search and rescue unmanned aerial vehicle is pushed outwards, the two search and rescue unmanned aerial vehicles are respectively a first search and rescue unmanned aerial vehicle and a second search and rescue unmanned aerial vehicle, and the first search and rescue unmanned aerial vehicle and the second search and rescue unmanned aerial vehicle adopt unmanned aerial vehicles in a turbine power or propeller unmanned aerial vehicle switchable mode;
a fire extinguishing cylinder hovering at a low speed around the crash part of the passenger aircraft, thereby providing continuous real-time video of the conditions of the passenger aircraft and passengers through the first search and rescue unmanned aerial vehicle, specifying the exact position of the passenger aircraft according to its built-in GPS, they can also extinguish fire using the fire extinguishing cylinder carried by the second search and rescue unmanned aerial vehicle;
the airliner selectively pushes out two search and rescue drones separately, wherein the first search and rescue drone is pushed out according to a program set in the microprocessor, which issues a command to perform the first push out to get a first view of the airliner from outside and send the view directly as a real-time report to the aviation center together with all other data, a situation may occur in which the airliner does not fall within 10 minutes, the airliner may fly farther, or even be close to a location near the airport, in which case the first search and rescue drone cannot track the airliner so far that it is meaningless to use only one search and rescue drone, the second search and rescue drone should remain in the middle and will push out later when one of the following conditions occurs;
a. when the microprocessor setup program is manipulating the data, it follows that an extreme emergency will occur for the guest and the indicator shows that the guest will inevitably fall or crash;
b. if the situation is not very bad and still controllable, the push-out of the second rescue drone will be paused, but it should be pushed out when the passenger aircraft finally enters in order to provide a real-time video report from behind it;
or in severe emergency situations in which the airliner is about to crash or explode, or has exploded, two search and rescue drones are being pushed out at a time.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/IB2016/001552 WO2016203322A2 (en) | 2016-10-27 | 2016-10-27 | Search and rescue drone arrangement |
Publications (2)
| Publication Number | Publication Date |
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| CN109843721A CN109843721A (en) | 2019-06-04 |
| CN109843721B true CN109843721B (en) | 2023-04-21 |
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| CN201680090107.7A Active CN109843721B (en) | 2016-10-27 | 2016-10-27 | Search and rescue unmanned aerial vehicle arrangement |
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| CN (1) | CN109843721B (en) |
| WO (1) | WO2016203322A2 (en) |
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| US10741088B1 (en) | 2017-09-29 | 2020-08-11 | DroneUp, LLC | Multiplexed communications for coordination of piloted aerial drones enlisted to a common mission |
| US10988251B2 (en) * | 2017-12-01 | 2021-04-27 | Jean Edrice Georges | On-board emergency response system for a vehicle |
| US11970285B2 (en) * | 2017-12-01 | 2024-04-30 | Jean Edrice Georges | On-board emergency remote assistance and data retrievable system for an aerial vehicle |
| US10814977B2 (en) * | 2018-03-15 | 2020-10-27 | International Business Machines Corporation | Backup rescue notification from deep sea |
| US20210001999A1 (en) * | 2018-03-21 | 2021-01-07 | Massimo Massa | Deployable flight data recorder with data recovery and method |
| US11100726B2 (en) * | 2018-06-01 | 2021-08-24 | Honeywell International Inc. | Systems and methods for real-time streaming of flight data |
| CN109747831B (en) * | 2018-12-27 | 2022-04-19 | 中国航空工业集团公司西安飞机设计研究所 | Tail sliding cable type air-based unmanned aerial vehicle launching device and launching method |
| CN110354426B (en) * | 2019-07-29 | 2024-04-16 | 陶文英 | Design method and system for fire-fighting system of multi-rotor unmanned aerial vehicle |
| JP7409225B2 (en) | 2020-05-19 | 2024-01-09 | マツダ株式会社 | Vehicle-mounted aircraft launch and landing platform device |
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Also Published As
| Publication number | Publication date |
|---|---|
| WO2016203322A3 (en) | 2017-05-18 |
| WO2016203322A2 (en) | 2016-12-22 |
| CN109843721A (en) | 2019-06-04 |
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