US 20170073070A1 (19) United States (12) Patent Application Publication (10) Pub. No.: US 2017/0073070 A1 Xing (43) Pub. Date: Mar. 16, 2017

(54) AMPHIBIOUS VERTICAL TAKEOFF AND GOSD L/00 (2006.01) LANDING UNMANNED DEVICE WITH B60F 5/02 (2006.01) (AI) AND B60F 3/00 (2006.01) METHOD AND SYSTEM FOR MANAGING A B64D 47/08 (2006.01) CRISIS ENVIRONMENT AND (52) U.S. Cl. CONTROLLING ONE OR MORE TARGETS CPC ...... B64C39/024 (2013.01); B60F 3/0061 (2013.01); B64D 47/08 (2013.01); G05D (71) Applicant: Zhou Tian Xing, Tiburon, CA (US) I/0088 (2013.01); B60F 5/02 (2013.01); B64D 7/00 (2013.01); B64C 2203/00 (2013.01); (72) Inventor: Zhou Tian Xing, Tiburon, CA (US) B64D 2211/00 (2013.01); B64C 2201/024 (2013.01); B64C 2201/021 (2013.01); B64C (21) Appl. No.: 15/362,118 220.1/042 (2013.01); B64C 220.1/066 (22) Filed: Nov. 28, 2016 (2013.01); B64C 220 1/141 (2013.01); B64C 220 1/127 (2013.01); B64C 220 1/12 (2013.01) Related U.S. Application Data (63) Continuation-in-part of application No. 29/572.722, (57) ABSTRACT filed on Jul. 29, 2016, Continuation-in-part of appli An amphibious vertical takeoff and landing unmanned cation No. 29/567,712, filed on Jun. 10, 2016, Con device with artificial intelligence (AI) system and method tinuation-in-part of application No. 14/940,379, filed for managing a crisis environment and controlling one or on Nov. 13, 2015, now Pat. No. 9,493,235, Contin more targets through an unmanned aerial (UAV). uation-in-part of application No. 14/957,644, filed on The device includes a camera unit and a first plurality of Dec. 3, 2015, now Pat. No. 9,489,671, which is a tranquilizer guns. The camera unit captures an image of one continuation-in-part of application No. 14/815,988, or more targets. The first communication unit integrated filed on Aug. 1, 2015, now Pat. No. 9,342.829, which with the camera unit to receive the image of the target. The is a continuation-in-part of application No. 13/760, GPS unit configured with the first communication unit to 214, filed on Feb. 6, 2013, now Pat. No. 9,016,565. track geographical location of the one or more targets, and further tracks the itinerary of the . Publication Classification The crisis detection unit to analyze the crisis environment. (51) Int. C. The first plurality of tranquilizer guns to receive the ana B64C39/02 (2006.01) lyzed data from the crisis detection unit and initiates an B64D 700 (2006.01) action in order to sedate one or more targets.

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AMPHIBIOUS VERTICAL TAKEOFF AND The copyright and trademark owner(s) has no objection to LANDING UNMANNED DEVICE WITH the facsimile reproduction by any of the patent disclosure, as ARTIFICIAL INTELLIGENCE (AI) AND it appears in the Patent and Trademark Office files or records, METHOD AND SYSTEM FOR MANAGING A but otherwise reserves all copyright and trademark rights CRISIS ENVIRONMENT AND whatsoever. CONTROLLING ONE OR MORE TARGETS TECHNICAL FIELD RELATED PATENT APPLICATION AND 0008. The presently disclosed embodiments are related, INCORPORATION BY REFERENCE in general, to an apparatus that corresponds to an unmanned 0001. This is a utility application and is a continuation in aerial vehicle (UAV). More particularly, the presently dis part of application Ser. No. 15/345.308 Confirmation Num closed embodiments are related to UAVs for managing a ber 6610 titled “An amphibious vertical take off and landing crisis environment and controlling one or more targets. unmanned device with AI data processing apparatus' filed Nov. 7, 2016: BACKGROUND 0002 This application is a continuation-in-part of U.S. 0009 Traditionally available unmanned aerial vehicle application Ser. No. 29/572/722, entitled “Amphibious vtol, (UAV) able to stay in the air for much longer as it is not hover, backward, leftward, rightward, turbojet, turbofan, constrained by a human's physical limits. Existing UAVs rocket engine, ramjet, pulse jet, afterburner, and Scramjet may perform precise, repetitive and hard tasks over a long single/dual all in one jet engine (fuel/electricity) with period which would be too hard, repetitively boring or need onboard self computer based autonomous module gimbaled to much precision for an on-board pilot to perform. The swivel propulsion (GSP) system device, same as ducted aforementioned UAVs do not put the operator in danger So fan(fuel/electricity)', filed Jul. 29, 2016. may fly in extreme and hostile climates as the operator may 0003. This application is a continuation-in-part of U.S. be stationed the other side of the world. Due to current application Ser. No. 29/567,712, entitled “Amphibious vtol, uncertain social environment, it has become imperative to hover, backward, leftward, rightward, turbojet, turbofan, step up the development of unmanned aerial vehicle (UAV), rocket engine, ramjet, pulsejet, afterburner, and scramjet all protected and in aircraft. in one jet engine (fuel/electricity) with onboard self com 0010 Thus, there is a need in the art for methods and puter based autonomous gimbaled Swivel propulsion system systems for managing a crisis environment and controlling device' filed Jun. 10, 2016. one or more target through an unmanned aerial vehicle. 0004. This application is a continuation-in-part of U.S. 0011 Further limitations and disadvantages of conven application Ser. No. 14/940,379, entitled “AMPHIBIOUS tional and traditional approaches will become apparent to VERTICAL TAKEOFF AND LANDING UNMANNED one of skill in the art, through comparison of described SYSTEMAND FLYING CAR WITH MULTIPLE AERIAL systems with Some aspects of the present disclosure, as set AND AQUATIC FLIGHT MODES FOR CAPTURING forth in the remainder of the present application and with PANORAMIC VIRTUAL REALITY VIEWS, INTERAC reference to the drawings. TIVE VIDEO AND TRANSPORTATION WITH MOBILE AND WEARABLE APPLICATION filed Nov. 13, 2015. SUMMARY 0005. This application is a continuation-in-part of U.S. application Ser. No. 14/957,644 (publication no. 2016/0086, 0012. According to embodiments illustrated herein, there 161), entitled “SYSTEMS AND METHODS FOR MOBILE may be provided an unmanned aerial vehicle (UAV) for APPLICATION, WEARABLE APPLICATION, TRANS managing a crisis environment and controlling one or more ACTIONAL MESSAGING, CALLING, DIGITAL MUL target. The UAV includes a camera unit, a first communi TIMEDIA CAPTURE AND PAYMENT TRANSAC cation unit, a GPS unit, a crisis detection unit, and a first TIONS'', filed Dec. 3, 2015; which is continuation-in-part of plurality of tranquilizer gun. The camera unit captures an U.S. patent application Ser. No. 14/815,988 (publication no. image of one or more target. The first communication unit 2015/0371,215), entitled “SYSTEMS AND METHODS integrated with the camera unit to receive the image of the FOR MOBILE APPLICATION, WEARABLE APPLICA target. The GPS unit configured with the first communica TION, TRANSACTIONAL MESSAGING, CALLING, tion unit to track geographical location of the one or more DIGITAL MULTIMEDIA CAPTURE AND PAYMENT target, and further tracks the itinerary of the unmanned aerial TRANSACTIONS' filed Aug. 1, 2015; which is continua vehicle. The crisis detection unit to analyze the crisis envi tion-in-part of Ser. No. 13/760,214 filed Feb. 6, 2013, which ronment. The first plurality of tranquilizer guns to receive in turn is a continuation-in-part of Ser. No. 10/677,098 the analyzed data from the crisis detection unit and initiates which claims priority to Provisional Application Ser. No. an action in order to sedate one or more target. The crisis 60/415,546, filed on Oct. 1, 2002, the content of which is detection unit includes a processing unit, a sensor unit, and incorporated herein by reference in its entirety. a second communication unit. The processing unit to control 0006 Moreover, the inventor(s) incorporate herein by the movement of the unmanned aerial vehicle based on the reference any and all patents, patent applications, and other received geographical location data of the target and itiner documents hard copy or electronic, cited or referred to in ary data from the GPS unit. The sensor unit having pre this application. stored instructions to sense the threat pertaining to the captured one or more target, and further the sensor unit COPYRIGHT AND TRADEMARK NOTICE programmed in order to initiate at least one of a semi autonomous decision, and an autonomous decision. The 0007. This application includes material which is subject second communication unit to communicate the sensed data or may be subject to copyright and/or trademark protection. received from the sensor unit. US 2017/0073070 A1 Mar. 16, 2017

BRIEF DESCRIPTION OF THE DRAWINGS property, element, or limitation. Further, repeated use of the phrase “in an embodiment” does not necessarily refer to the 0013 The accompanying drawings illustrate the various same embodiment. embodiments of systems, methods, and other aspects of the 0022. Unless otherwise noted in this specification or in disclosure. Any person with ordinary skills in the art will the claims, all of the terms used in the specification and the appreciate that the illustrated element boundaries (e.g., claims will have the meanings normally ascribed to these boxes, groups of boxes, or other shapes) in the figures terms by workers in the art. represent one example of the boundaries. In some examples, 0023. Unless the context clearly requires otherwise, one element may be designed as multiple elements, or throughout the description and the claims, the words "com multiple elements may be designed as one element. In some prise.” “comprising and the like are to be construed in an examples, an element shown as an internal component of inclusive sense as opposed to an exclusive or exhaustive one element may be implemented as an external component sense; that is to say, in a sense of “including, but not limited in another, and vice versa. Further, the elements may not be to.” Words using the singular or plural number also include drawn to scale. the plural or singular number, respectively. Additionally, the 0014 Various embodiments will hereinafter be described words “herein,' 'above,” “below,” and words of similar in accordance with the appended drawings, which are pro import, when used in this application, shall refer to this vided to illustrate and not to limit the scope in any manner, application as a whole and not to any particular portions of wherein similar designations denote similar elements, and in this application. which: 0024 FIG. 1 is illustrates an unmanned aerial vehicle 0015 FIGS. 1a-1c are illustrating an unmanned aerial (UAV) 100 for managing a crisis environment and control vehicle (UAV) for managing a crisis environment and con ling one or more target, in accordance with at least one trolling one or more targets, in accordance with at least one embodiment. As shown in FIG. 1, by way of example but not embodiment; limitation, Schematic diagram of the unmanned aerial 0016 FIGS. 2a-2e are exemplary operational views of a vehicle (UAV) for managing a crisis environment and con first unmanned aerial vehicle (UAV) for managing a crisis trolling one or more target may include at least one UAV or environment and controlling one or more targets, in accor at least one remotely controlled UAV. dance with at least one embodiment; 0025. For certain example embodiments, a UAV 100 may 0017 FIGS. 3a-3b are illustrating a fuselage having a comprise or include a vehicle that is not capable of being forward cockpit to house a second plurality of tranquilizers, occupied by a human pilot (e.g., due to size, shape, power, in accordance with at least one embodiment; atmospheric pressure, or a combination thereof, etc. con straints), a vehicle that is not designed to seat or otherwise 0018 FIGS. 3C-3d are exemplary operational views of a safely support a person, a vehicle that is not controllable by second unmanned aerial vehicle (UAV) for managing a an onboard human pilot, a vehicle that is being autono crisis environment and controlling one or more targets, in mously controlled at least partially by at least one onboard accordance with at least one embodiment; and module, a vehicle that is being autonomously controlled at 0019 FIG. 4 is a flowchart that illustrates a method for least partially by at least one off-board module, a combina managing a crisis environment and controlling one or more tion thereof, or so forth. For certain example embodiments, targets through an unmanned aerial vehicle (UAV), in accor a UAV 100 may be at least comparable to or may comprise dance with at least one embodiment. or include at least a portion of any one or more of an unoccupied flying vehicle (UFV), a remotely piloted vehicle DETAILED DESCRIPTION OF EMBODIMENTS (RPV), an unmanned combat air vehicle (UCAV), an OF THE INVENTION unmanned aircraft (UA), a drone, an optionally-piloted vehicle (OPV) that is not currently being controlled by an 0020. The present disclosure may be best understood on-board pilot, a remotely piloted aircraft (RPA), a remotely with reference to the detailed figures and description set operated aircraft (ROA), a radio-controlled aircraft (R/C forth herein. Various embodiments are discussed below with aircraft), an unmanned-aircraft vehicle system (UAVS), an reference to the figures. However, those skilled in the art will unmanned aircraft system (UAS), a small unmanned air readily appreciate that the detailed descriptions given herein system (suAS), a combination thereof, or so forth. For with respect to the figures are simply for explanatory pur certain example embodiments, a UAV 100 may fly through poses as the apparatuses, methods and systems may extend a fluid (e.g., the earth's atmosphere or the air), through at beyond the described embodiments. For example, the teach least a partial vacuum (e.g., space or near-earth orbit), a ings presented and the needs of a particular application may combination thereof, or so forth. However, claimed subject yield multiple alternative and Suitable approaches to imple matter is not limited to any particular described embodi ment the functionality of any detail described herein. There ments, implementations, examples, etc. fore, any approach may extend beyond the particular imple 0026. As shown in FIGS. 1a-1c the UAV 100 includes a mentation choices in the following embodiments described camera unit 102, a first communication unit (not shown in and shown. FIG. 1), a GPS unit (not shown in FIG. 1), a crisis detection 0021 References to “one embodiment, at least one unit (not shown in FIG. 1), a first plurality of tranquilizer embodiment,” “an embodiment, one example.” “an gun (shown and explained in conjunction with FIG. 2), and example,” “for example,” and so on indicate that the plurality of fans 108. The camera unit 102 captures a embodiment(s) or example(s) may include a particular fea real-time video of the target, a real-time image of the target, ture, structure, characteristic, property, element, or limita and 360-degree panoramic video recording of the target used tion but that not every embodiment or example necessarily for virtual reality view. The camera unit 102 is further includes that particular feature, structure, characteristic, configured to adjust one or more of the parameters such as US 2017/0073070 A1 Mar. 16, 2017

Zoom, shutter speed, aperture, ISO, focal length, depth of a lock mechanism. In an embodiment the lock mechanism field, exposure compensation, white balance, video or photo operated by at least one of numerical passwords, word frame size and orientation, camera resolution and frame passwords, fingerprint recognition, face recognition, eye rates. recognition, and a physical key. 0027. The first communication unit integrated with the 0034. The unmanned aerial vehicle 100 further includes camera unit 102 to receive the captured data of the target, a wireless unit to establish a communication with the remote and further performs high definition low latency real time unit in order to transmit the notification to the one or more data downlink. The first communication unit is a high power, authority. The unmanned aerial vehicle 100 further includes high gain, and ultra-high frequency electronic device. The a power Supply unit to provide a DC power Supply to the GPS unit configured with the first communication unit to crisis detection unit. The unmanned aerial vehicle 100 track geographical location of the one or more target, and further includes plurality of landing gear to enable the UAV further tracks the itinerary of the unmanned aerial vehicle to taking off and landing. The unmanned aerial vehicle 100 100. The crisis detection unit to analyze the crisis environ further comprising an observing unit to observe one or more ment. The crisis detection unit includes a processing unit, a weather condition. The unmanned aerial vehicle 100 further sensor unit, and a second communication unit. The process includes a Solar panel to power the crisis detection unit. The ing unit to control the movement of the unmanned aerial unmanned aerial vehicle 100 further includes a wind turbine vehicle based on the received geographical location data of unit to power the crisis detection unit. the target and itinerary data from the GPS unit. 0035. The unmanned aerial vehicle 100 further includes 0028. The processing unit includes a flight controlling a rear propeller to enhance the speed of the unmanned aerial module to perform stable transitions between a hover mode, vehicle. The unmanned aerial vehicle 100 further includes a a full forward flight mode, and an underwater mode. The measuring unit to measure the distance of the target from the flight controlling module is selected from at least one an unmanned aerial vehicle. The unmanned aerial vehicle 100 external micro controller or an internal micro controller; and further includes a display unit to display the images being a barometer, an accelerometer, a gyroscope, and a magne taken by the camera unit. Additionally, the UAV 100 tometer. Further, the flight controlling module enables or includes a broadcasting unit to transmit the captured data to disables the GPS unit, records flight parameters, allow one or more external devices. Examples of the external inverted flight, aerial and aquatic rolls and flips, stabilize device includes but not limited to a display Screen, a proportional, activates the UAV after user inputs an arming projector, a split screen, a Switch screen, and a headset. action or an arming sequence. 0036 FIGS. 2a-2e are exemplary operational view 200a, 0029. The GPS unit enables autonomous flying at low 200b, 200c, and 200d of a first unmanned aerial vehicle altitude and avoiding obstacles. The GPS unit further evalu (UAV) for managing a crisis environment and controlling ates and selects landing sites in an unmapped terrain. Addi one or more target, in accordance with at least one embodi tionally, the GPS unit detects high-tension wires over a ment. The first plurality of tranquilizer gun 202a, 202b, and desert terrain. 202c gun to receive the analyzed data from the crisis 0030. In an embodiment, a navigation sensing unit con detection unit and initiates an action in order to sedate one figured with the GPS unit to map an unknown area where or more target. The plurality of tranquilizer gun 202 filled obstructions limited landing sites. The navigation sensing with at least one of a sedative chemical; an anesthetic agent; unit includes an inertial sensor to look forward and a laser and a paralytic agent. a plurality of rotors. In an embodi scanner to look down. Additionally, the navigation sensing ment, the present UAV includes a plurality of rotors being unit aborts paths to enable responding to unexpected cir operable to tilt on a three axis, the one or more of the Cum Stances. plurality of motors is attached to at least one arm, and a 0031. The sensor unit having pre-stored instructions to mating tilt mechanism to the at least one arm is actuated by sense the threat pertaining to the captured one or more target, one or more motors or a servomotor drive train. FIGS. 3a-3b and further the sensor unit programmed in order to initiate are illustrating a fuselage 300 having a forward cockpit 302 at least one of a semi-autonomous decision, and an autono to house a second plurality of tranquilizer, in accordance mous decision. The second communication unit to commu with at least one embodiment. FIGS. 3c-3d are exemplary nicate the sensed data received from the sensor unit. operational views of a second unmanned aerial vehicle Examples of the sensor unit includes but not limited to stereo (UAV) for managing a crisis environment and controlling sensors, ultrasonic sensors, infrared sensors, multispectral one or more target, in accordance with at least one embodi sensors, optical flow sensors, and volatile organic compound ment. sensors. The aforementioned sensors are provided for intel 0037 FIG. 4 is a flowchart that illustrates a method 400 ligent positioning, collision avoidance, media capturing, for managing a crisis environment and controlling one or Surveillance, and monitoring. more target through an unmanned aerial vehicle (UAV), in 0032. In an exemplary implementation, the unmanned accordance with at least one embodiment. The flowchart 400 aerial vehicle 100 further includes a memory unit to store the is described in conjunction with FIG. 1, FIG. 2, and FIG. 3. geographical location data pertaining to the target, itinerary The method starts at step 402. data of the unmanned aerial vehicle, and decision data. The 0038. At step 402, capturing an image of one or more unmanned aerial vehicle 100 further includes a notification target through a camera unit. At step 404, receiving the unit to receive the sensed data from the second communi image of the target through a first communication unit cation unit to notify one or more authority. integrated with the camera unit. At step 406, tracking 0033. The unmanned aerial vehicle 100 further includes geographical location of the one or more target, and further a speaker unit to announce a pre-recorded message in order tracking the itinerary of the unmanned aerial vehicle. At step to initiate a voice command. The unmanned aerial vehicle 408, analyzing the crisis environment through a crisis detec 100 is operated by a remote unit. The remote unit includes tion unit. US 2017/0073070 A1 Mar. 16, 2017

0039. At step 410, controlling the movement of the present disclosure not be limited to the particular embodi unmanned aerial vehicle based on the received geographical ment disclosed, but that the present disclosure will include location data of the target and itinerary data from the GPS all embodiments falling within the scope of the appended unit through a processing unit. At step 412, sensing the threat claims. pertaining to the captured one or more target through a 0048. The above detailed description of embodiments of sensor unit having pre-stored instructions. the invention is not intended to be exhaustive or to limit the 0040. At step 414, initiating at least one of a semi invention to the precise form disclosed above. While specific autonomous decision, and an autonomous decision through embodiments of, and examples for, the invention are the sensor unit. At step 416, communicating the sensed data described above for illustrative purposes, various equivalent received from the sensor unit through a second communi modifications are possible within the scope of the invention, cation unit. At step 418, receiving the analyzed data from the as those skilled in the relevant art will recognize. For crisis detection unit and initiates an action in order to sedate example, while steps are presented in a given order, alter one or more target through a first plurality of tranquilizer native embodiments may perform routines having steps in a gun. different order. The teachings of the invention provided 0041 At step 420 storing the geographical location data herein can be applied to other systems, not only the systems pertaining to the target, itinerary data of the unmanned aerial described herein. The various embodiments described herein vehicle, and decision data through a memory unit. At step can be combined to provide further embodiments. These and 422, receiving the sensed data from the second communi other changes can be made to the invention in light of the cation unit to notify one or more authority through a detailed description. notification unit. 0049 All the above references and U.S. patents and 0.042 At step 424, announcing a pre-recorded message in applications are incorporated herein by reference. Aspects of order to initiate a voice command through a speaker unit. At the invention can be modified, if necessary, to employ the step 426, operating the UAV by a remote unit. At step 428, systems, functions and concepts of the various patents and establishing a communication with the remote unit in order applications described above to provide yet further embodi to transmit the notification to the one or more authority ments of the invention. through a wireless unit. What is claimed is: 0043. At step 430, housing a second plurality of tranquil 1. An amphibious vertical takeoff and landing unmanned izer through a fuselage having a forward cockpit. At step device with artificial intelligence (AI) for managing a crisis 432, providing a DC power supply to the crisis detection unit environment and controlling one or more target, the through a power supply unit. At step 434, enabling the UAV unmanned aerial vehicle comprising: to taking off and landing through plurality of landing gear. a camera unit to capture an image of one or more target; At step 436, of observing one or more weather condition. a first communication unit integrated with the camera unit 0044. At step 438, powering the crisis detection unit to receive the image of the target; through a solar panel. At step 440, powering the crisis a GPS unit configured with the first communication unit detection unit through a wind turbine unit. At step 442, to track geographical location of the one or more target, enhancing the speed of the unmanned aerial vehicle through and further tracks the itinerary of the unmanned aerial a rear propeller. At step 444, measuring the distance of the vehicle: target from the unmanned aerial vehicle through a measur a crisis detection unit to analyze the crisis environment, ing unit. At step 446, displaying the images being taken by the crisis detection unit comprising: the camera unit through a display unit. a processing unit to control the movement of the 0045. A person skilled in the art will understand that the unmanned aerial vehicle based on the received geo UAV 100 is described herein for illustrative purposes and graphical location data of the target and itinerary should not be construed to limit the scope of the disclosure. data from the GPS unit; Various embodiments of the disclosure encompass numer a sensor unit having pre-stored instructions to sense the ous advantages including apparatuses, methods and systems threat pertaining to the captured one or more target, for managing a crisis environment and controlling one or and further the sensor unit programmed in order to more target through an unmanned aerial vehicle (UAV). initiate at least one of a semi-autonomous decision, 0046. A person with ordinary skills in the art will appre and an autonomous decision; and ciate that the apparatuses, systems, modules, and Sub-mod a second communication unit to communicate the ules have been illustrated and explained to serve as sensed data received from the sensor unit; examples and should not be considered limiting in any a first plurality of tranquilizer gun to receive the analyzed manner. It will be further appreciated that the variants of the data from the crisis detection unit and initiates an action above disclosed system elements, modules, and other fea in order to sedate one or more target. tures and functions, or alternatives thereof, may be com a propulsion system including a coaxial propulsion sys bined to create other different apparatuses, systems or appli tem, wherein the propulsion system comprises a plu cations. rality of motors and rotors associated with the plurality 0047 While the present disclosure has been described of motors, wherein the rotors are selected from a group with reference to certain embodiments, it will be understood comprising: clockwise rotors, counterclockwise rotors, by those skilled in the art that various changes may be made and variable pitch rotors; and equivalents may be substituted without departing from a rotor protection system; at least one wing; a landing the scope of the present disclosure. In addition, many system that conforms to a landing Surface, the landing modifications may be made to adapt a particular situation or system including at least a chassis; one or more control material to the teachings of the present disclosure without Surfaces selected from a group comprising: a rudder, an departing from its scope. Therefore, it is intended that the aileron, a flap, and an elevator, an onboard air com US 2017/0073070 A1 Mar. 16, 2017

pressor, an onboard electrolysis system; at least one associated with a brushless electric motor operable to waterproof through-body wire orantenna feed-through; spin the electric-drive impeller to provide at least one a tilt wing device; a door connected to the modular and air accelerator ring with compressed forced air thrust. expandable waterproof body, wherein the door is 2. The unmanned aerial vehicle according to claim 1 Selected from a group comprising: a gull wing door and further including a memory unit to store the geographical a falcon wing door; at least one tilt rotor device; location data pertaining to the target, itinerary data of the a power distribution board comprising one or more of the unmanned aerial vehicle, and decision data, wherein the following: a flight controller, electronic speed control modular and expandable waterproof body has a back portion lers, a buzzer, an on Screen display telemetry device, a and a front portion, wherein the amphibious VTOL video transmitter, and a receiver, wherein unmanned device is configured to be launched from a body the rotors include at least a first rotor and a second of a user, wherein the amphibious VTOL unmanned device rotor, the first rotor being operable to rotate about a first is operable to perform an automatic landing and an auto axis and tilt about a second axis between a helicopter matic takeoff, wherein the amphibious VTOL unmanned mode and an aeroplane mode, wherein the first rotor device is configured in a form of one of the following: a comprises a shaft operable to rotate about the first axis people-carrying vehicle, a cargo-carrying vehicle, a radio and tilt about the second axis between the helicopter controlled toy, an autonomous vehicle, a multi-blade ducted mode and the aeroplane mode; the first axis being fan roadable electric aircraft, an , a driv transversal to a longitudinal direction of the amphibi erless car, a self-driving car, an unmanned aerial vehicle, a ous VTOL unmanned device in the helicopter mode drone, a robotic car, a commercial goods and passenger and being Substantially parallel to the longitudinal carrying vehicle, and a private self-drive vehicle; wherein direction in the aeroplane mode, and the second rotor the autonomous vehicle is configured to sense environmen being operatively connected to the shaft of the first tal conditions, navigate without human input, and perform rotorian electrical power storage device, wherein the autopiloting; wherein the sensing is performed via one or electrical power storage device includes at least a more of the following: the ultrasonic radar sensor, the lidar, battery, wherein a shape of the battery conforms to an the GPS module, and a computer vision module; wherein the interior profile of the modular and expandable water environmental sample processor is operable to interpret proof body; sensory information to identify navigation paths, obstacles an electrical machine comprising a stator and an onboard and signage; wherein the autonomous vehicle is operable to electricity generator, the stator being electrically con update maps based on sensory input to keep track of a nected to the electrical power storage device, wherein position when conditions change or when uncharted envi the onboard electricity generator is selected from a ronments are entered; and wherein the multi-blade ducted group comprising: a plurality of solar cells, one or more fan roadable electric aircraft is propelled by the plurality of wind turbines, and one or more hydroelectric genera motors using electrical energy stored in the electrical power tors; wherein the electrical machine acts as an electric storage device. motor for driving rotation of the first rotor by using the 3. The unmanned aerial vehicle according to claim 1 electrical power storage device, and wherein the elec further including a notification unit to receive the sensed trical machine acts as an electrical power generator for data from the second communication unit to notify one or re-charging the electrical power storage device by more authority. causing the rotation of the second rotor under action of 4. The unmanned aerial vehicle according to claim 1 a wind current; wherein the plurality of motors includes further including a speaker unit to announce a pre-recorded at least a solar turbine powered impeller motor, the message in order to initiate a voice command. Solar turbine powered impeller motor being disposed 5. The plurality of tranquilizer gun according to claim 1 centrally in the amphibious VTOL unmanned device, filled with at least one of a sedative chemical; an anesthetic the Solar turbine powered impeller motor comprising an agent; and a paralytic agent. electric-drive impeller contained in a compression 6. The unmanned aerial vehicle according to claim 1 is chamber and having an axis of rotation oriented per operated by a remote unit, further establishing a communi pendicularly to an axis of the amphibious VTOL cation with the remote unit in order to transmit the notifi unmanned device, the solar turbine powered impeller cation to the one or more authority through a wireless unit. motor being powered by the plurality of solar cells 7. The unmanned aerial vehicle according to claim 1 when the plurality of solar cells is used, the plurality of further includes a wireless unit to establish a communication Solar cells comprising at least a solar film, the Solar film with the remote unit in order to transmit the notification to being integrated on one or more of the following: an the one or more authority. upper surface of the amphibious VTOL unmanned 8. The unmanned aerial vehicle according to claim 1 device; and further includes a fuselage having a forward cockpit to alidar, and an ultrasonic radar sensor; wherein the at least house a second plurality of tranquilizer, further includes the one wing includes a left forward Swept wing and a right step of housing a second plurality of tranquilizer through a forward swept wing, the left forward swept wing and fuselage having a forward cockpit,wherein the modular and the right forward Swept wing being mounted on the expandable waterproof body has a back portion and a front chassis, and wherein the rotors further include a first portion, wherein the amphibious VTOL unmanned device is brushless ducted fan and a second brushless ducted fan configured to be launched from a body of a user, wherein the integrated left and right of the chassis, the first brush amphibious VTOL unmanned device is operable to perform less ducted fan and the second brushless ducted fan an automatic landing and an automatic takeoff, wherein the being powered by the solar film, the first brushless amphibious VTOL unmanned device is configured in a form ducted fan and the second brushless ducted fan being of one of the following: a people-carrying vehicle, a cargo US 2017/0073070 A1 Mar. 16, 2017

carrying vehicle, a radio controlled toy, an autonomous a crisis environment and controlling one or more target vehicle, a multi-blade ducted fan roadable electric aircraft, through an unmanned aerial vehicle (UAV), the method an uncrewed vehicle, a driverless car, a self-driving car, an comprising the steps of: unmanned aerial vehicle, a drone, a robotic car, a commer capturing an image of one or more target through a cial goods and passenger carrying vehicle, and a private camera unit; self-drive vehicle; wherein the autonomous vehicle is con receiving the image of the target through a first commu figured to sense environmental conditions, navigate without nication unit integrated with the camera unit; human input, and perform autopiloting; wherein the sensing tracking geographical location of the one or more target, is performed via one or more of the following: the ultrasonic and further tracking the itinerary of the unmanned radar sensor, the lidar, the GPS module, and a computer aerial vehicle through a GPS unit configured with the vision module; wherein the environmental sample processor is operable to interpret sensory information to identify first communication unit; navigation paths, obstacles and signage; wherein the autono analyzing the crisis environment through a crisis detection mous vehicle is operable to update maps based on sensory unit; input to keep track of a position when conditions change or controlling the movement of the unmanned aerial vehicle when uncharted environments are entered; and wherein the based on the received geographical location data of the multi-blade ducted fan roadable electric aircraft is propelled target and itinerary data from the GPS unit through a by the plurality of motors using electrical energy stored in processing unit; the electrical power storage device. sensing the threat pertaining to the captured one or more 9. The unmanned aerial vehicle according to claim 1 target through a sensor unit having pre-stored instruc further comprising a power Supply unit to provide a DC tions; power Supply to the crisis detection unit. initiating at least one of a semi-autonomous decision, and 10. The unmanned aerial vehicle according to claim 1 an autonomous decision through the sensor unit; further comprising plurality of landing gear to enable the communicating the sensed data received from the sensor UAV to taking off and landing, further includes the step of unit through a second communication unit; and observing one or more weather condition. receiving the analyzed data from the crisis detection unit 11. The unmanned aerial vehicle according to claim 1 and initiates an action in order to sedate one or more further comprising an observing unit to observe one or more target through a first plurality of tranquilizer gun, weather condition. further includes the step of providing a DC power 12. The unmanned aerial vehicle according to claim 1 Supply to the crisis detection unit through a power further comprising a solar panel to power the crisis detection Supply unit, further includes the step of powering the unit, further includes the step of enabling the UAV to taking crisis detection unit through a solar panel, further off and landing through plurality of landing gear. includes the step of powering the crisis detection unit 13. The unmanned aerial vehicle according to claim 1 through a wind turbine unit. further includes the step of further comprising a wind turbine unit to power the crisis display the images being taken by the camera unit detection unit. through a display unit. 14. The unmanned aerial vehicle according to claim 1 18. The method according to claim 17 further includes the further comprising a rear propeller to enhance the speed of step of storing the geographical location data pertaining to the unmanned aerial vehicle. the target, itinerary data of the unmanned aerial vehicle, and 15. The unmanned aerial vehicle according to claim 1 decision data through a memory unit; further comprising a measuring unit to measure the distance 19. The method according to claim 17 further includes the of the target from the unmanned aerial vehicle. step of receiving the sensed data from the second commu 16. The unmanned aerial vehicle according to claim 1 nication unit to notify one or more authority through a further comprising a display unit to display the images being notification unit. taken by the camera unit, further includes the step of measuring the distance of the target from the unmanned 20. The method according to claim 17 further includes the aerial vehicle through a measuring unit. step of announcing a pre-recorded message in order to 17. An amphibious vertical takeoff and landing unmanned initiate a voice command through a speaker unit. device with artificial intelligence (AI) method for managing k k k k k