KR20200121678A - Drones with morphological transformation in the air and underwater - Google Patents

Drones with morphological transformation in the air and underwater Download PDF

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KR20200121678A
KR20200121678A KR1020190044540A KR20190044540A KR20200121678A KR 20200121678 A KR20200121678 A KR 20200121678A KR 1020190044540 A KR1020190044540 A KR 1020190044540A KR 20190044540 A KR20190044540 A KR 20190044540A KR 20200121678 A KR20200121678 A KR 20200121678A
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drone
air
drone body
main
underwater
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KR1020190044540A
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Korean (ko)
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KR102200201B1 (en
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백남용
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백남용
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/14—Control of attitude or depth
    • B63G8/22—Adjustment of buoyancy by water ballasting; Emptying equipment for ballast tanks
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • B64C35/005—Flying-boats; Seaplanes with propellers, rudders or brakes acting in the water
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C37/00—Convertible aircraft
    • 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
    • B64D47/00—Equipment not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/001—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations
    • B63G2008/002—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations unmanned
    • B63G2008/005—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations unmanned remotely controlled
    • B64C2201/024—
    • B64C2201/108—
    • B64C2201/12—
    • B64C2201/146—
    • B64C2201/165—
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)

Abstract

The present invention relates to a drone which can be moved in the air and water for reconnaissance and to perform other multi-purpose missions, and more specifically, to a drone which can perform multi-purpose missions by allowing the shape to be changed in separate fields of the sky and the ocean to fly in the air and sail on and under the water by allowing a housing cover having a main rotary unit generating lift force to be provided in an openable manner to be opened and closed. In short, during the flying of the main drone body, the main rotary unit is opened to the outside to enable flying in the air, whereas, during the sailing thereof, the main rotary unit is stored in the main drone body to provide a streamlined shape suitable for sailing on the water and under the water. Therefore, the present invention provides a shape optimized for separate areas in the air and water. Consequently, the utilization of the drone can be improved by providing the shape optimized for separate areas in the air and water. To this end, the present invention comprises a main drone body, a main rotary unit, and a main rotary unit housing.

Description

공중과 수중에서의 형태적 변환을 갖는 드론{omitted}Drone with morphological transformation in the air and underwater{omitted}

본 발명은 공중과 수중에서의 이동 및 정찰, 기타 다목적 임무수행이 가능한 드론에 관한 것으로, 상세하게는 양력을 발생시키는 주회전부가 구비된 하우징 덮개를 여닫이 방식으로 개방과 폐쇄를 가능하게 함으로서 공중에서의 비행과 수면 및 수중에서의 항해주행 같은 창공과 해양의 각 영역에서 형태적 변환을 가능하게 함으로서 다목적 임무수행이 가능한 드론에 관한 것이다.The present invention relates to a drone capable of moving, reconnaissance, and other multi-purpose missions in the air and underwater, and in detail, by opening and closing a housing cover equipped with a main rotating part that generates lift, It relates to a drone capable of performing multi-purpose missions by enabling morphological transformation in each area of the sky and ocean, such as flight and navigation on the surface and underwater.

현재 드론은 군사, 기업, 개인등등 전영역의 광대한 범위에서 활용되고 있다.Currently, drones are used in a wide range of fields such as military, corporate, and individual.

보통 일반적으로 알고 있는 드론은 공중을 비행하여 사용되고 있고 일부 수중에서 특화된 수중용 드론도 개발되어 사용되고 있다. 현재 드론은 사용목적에 따라 첩보, 상업, 취미뿐만 아니라 재난지역 등 사람의 접근이 곤란한 지역까지, 특수한 지역으로까지 다목적 용도로서 사용용도가 확대되고 있다.Commonly known drones are used by flying in the air, and some underwater drones specialized in underwater have also been developed and used. Depending on the purpose of use, drones are expanding their use as multi-purpose to special areas, not only for espionage, commerce, and hobbies, but also areas where human access is difficult, such as disaster areas.

그런데 지금까지의 드론은 공중 및 수중의 어느 특정 영역에서만 사용용도가 제한적이거나 혹은 이 둘의 기능 겸용성을 가진 개발이 간혹 이루어지고는 있으나 공, 수중 모두의 기능을 최적화 시키지는 못하여 실제적 활용성은 여전히 떨어진다.However, until now, the use of drones is limited only in certain areas in the air and in water, or development with the function of both is sometimes developed, but the practical utility is still inferior because it cannot optimize the functions of both air and water.

본 발명은 상기한 종래기술의 문제점을 해결하기 위한 것으로, 드론본체의 비행주행시에는 주회전부를 외부로 개방시켜 공중비행이 가능하도록 하고, 항해주행시에는 주회전부를 드론본체 내부로 수납시킴과 동시에 수상 및 수중항해에 적합한 유선형의 형태를 제공하여 공중과 수중에서의 각 영역에서 최적화된 형태를 제공하고자 한다.The present invention is to solve the problems of the prior art described above, when flying the drone body, the main rotation part is opened to the outside so that air flight is possible, and during navigation, the main rotation part is stored inside the drone body and at the same time And by providing a streamlined shape suitable for underwater navigation, it is intended to provide an optimized shape in each area in the air and underwater.

본 발명은 상기한 목적을 달성하기 위한 수단으로, 상기 드론본체에 형성되어 있는 다수개의 개방과 폐쇄가 가능한 상기 주회전부하우징; 상기 주회전부하우징의 내측면에는 양력을 발생시키는 주모터(Main Motor)와 주날개(Main Propeller)를 포함하는 상기 주회전부가 구비되며, 상기 주회전부하우징은 여닫이방식(폴딩)의 개방과 폐쇄가 되는 구조를 갖는다. 상기 주회전부하우징이 펼쳐져 완전히 개방되면 상기 주회전부하우징의 내측면에 구비되어 있는 상기 주회전부가 외부로 드러나기 때문에 상기 주회전부의 회전운동에 의해 양력이 발생되어 공중으로의 비행이 가능하며, 반대로 상기 주회전부하우징들의 양측면이 서로가 맞닿아 완전히 접혀 폐쇄가 되면 주회전부하우징 내측에 구비된 주회전부는 자연히 상기 드론본체 내부에 수납이 됨과 동시에 상기 드론본체는 수상 및 수중에서의 항해주행에 적합한 유선형의 모습으로 형태적 변환이 이루어지는 특징을 갖는다.The present invention is a means for achieving the above object, the main rotating load housing that is capable of opening and closing a plurality of the drone body; The main rotating part including a main motor and a main propeller for generating lift is provided on the inner side of the main rotating load housing, and the main rotating load housing is capable of opening and closing the opening and closing method (folding). It has a structure to be When the main rotational load housing is unfolded and completely opened, the main rotational part provided on the inner side of the main rotational load housing is exposed to the outside, so that lift is generated by the rotational motion of the main rotational part, allowing flight in the air. When both sides of the main rotating load housings are in contact with each other and are completely folded and closed, the main rotating part provided inside the main rotating load housing is naturally housed inside the drone body, and the drone body is a streamlined type suitable for sailing in water and underwater. It has the characteristic that morphological transformation takes place into a figure.

상기 드론본체 하단부에 구비되어 있는 보조모터(Sub Motor)및 보조날개(Sub Propeller)를 포함하는 보조회전부; 상기 보조회전부는 상기 드론본체의 수상 및 수중의 항해주행을 위해 쓰이며 혹은 선택적으로 공중비행에서도 주회전부와 같이 보조적으로 쓰이는 것 역시 가능하다. 이와 함께 항해시 방향조정을 위한 방향타및 방향타회전축등이 포함된 방향장치부가 드론본체에 구비된다. 상기 드론본체가 잠수와 부상을 할 수 있도록 구비된 부력장치부; 상기 부력장치부는 압축공기실과 압축기가 구비되며, 상기 주회전부하우징이 폐쇄되어 내측에 형성된 공간은 물이 입수되고 배출되는 부력실로서 사용되어 상기 드론본체의 잠수와 부상을 가능하게 한다.An auxiliary rotation unit including a sub motor and a sub propeller provided at the lower end of the drone body; The auxiliary rotating part is used for navigation on the water and underwater of the drone body, or it is also possible to be used as an auxiliary part in the air flight as well as the main rotating part. Along with this, a direction device including a rudder and a rudder rotation axis for direction adjustment during navigation is provided on the drone body. A buoyancy device provided so that the drone body can dive and float; The buoyancy device unit is provided with a compressed air chamber and a compressor, and the space formed inside the main rotating load housing is closed is used as a buoyancy chamber through which water is received and discharged, thereby enabling the dive and float of the drone body.

상기 드론본체 외부에는 관측기가 구비되어 창공과 해양에서의 외부환경을 정찰하고, 관측기에서 정찰된 외부환경정보를 사용자에게 송수신을 하기 위해 통신모뎀과 안테나를 포함하는 통신장치부가 구비된다. 그리고 상기 서술한 주회전부, 보조회전부, 방향타장치부, 부력장치들을 원격으로 조정하기 위한 중앙제어부와 전력을 공급하는 배터리가 구비된다.A communication device including a communication modem and an antenna is provided outside the drone body to reconnaissance of the external environment in the sky and the sea, and to transmit/receive external environment information scouted by the observer to a user. In addition, a central control unit for remotely controlling the above-described main rotation unit, auxiliary rotation unit, rudder device unit, and buoyancy device and a battery supplying power are provided.

이로서 본 발명에 의해, 주회전부가 설치된 주회전부하우징을 여닫이식으로 개방과 폐쇄가 가능함에 따라 공중에서는 주회전부에 의해 비행을 할 수 있게 되고, 반대로 주 회전부하우징의 양측면들을 서로 맞물려 폐쇄시키면 항해에 적합한 유선형의 형태를 제공함으로서 창공과 항해등 각 환경에 최적화된 형태를 제공하게 되어 관측과 기타 다목적 용도로 사용할 수 있게 된다.Accordingly, according to the present invention, as the main rotating load housing installed with the main rotating part can be opened and closed in an opening and closing manner, it is possible to fly by the main rotating part in the air. On the contrary, if the two sides of the main rotating load housing are engaged and closed, it will By providing an appropriate streamlined shape, it can be used for observation and other multi-purpose purposes by providing a shape optimized for each environment such as expanse and navigation.

도면 1은 본 발명에 따른 공중과 수중에서의 형태적 변환을 갖는 드론의 공중 비행시의 상면도이다.
도면 2는 본 발명에 따른 공중과 수중에서의 형태적 변환을 갖는 드론의 공중비행시의 측면도과 주 회전부하우징의 접힘 부분을 설명한 구조도 이다.
도면 3은 본 발명에 따른 공중과 수중에서의 형태적 변환을 갖는 드론의 수상 및 수중항해를 보인 측면도이다.
도면 4는 본 발명에 따른 공중과 수중에서의 형태적 변환을 갖는 드론의 유선전선 사용시 잠수선과의 연결사용을 보인 개략도이다.
도면 5는 본 발명에 따른 공중과 수중에서의 형태적 변환을 갖는 드론의 내부 구조도이다.1 is a top view of a drone having a morphological transformation in the air and underwater according to the present invention during aerial flight.
FIG. 2 is a structural diagram illustrating a side view of a drone having morphological transformation in the air and in water according to the present invention, and a folded portion of the main rotating load housing.
Figure 3 is a side view showing the surface and underwater navigation of a drone having morphological transformation in the air and underwater according to the present invention.
Figure 4 is a schematic diagram showing the use of connection with a submarine when using a wired wire of a drone having morphological transformation in the air and underwater according to the present invention.
FIG. 5 is an internal structure diagram of a drone having morphological transformation in air and underwater according to the present invention.

본 발명의 특징 및 장점 그리고 그것들을 수행하여 달성하는 방법은 첨부되는 도면과 함께 상세하게 후술되어 있는 실시 예를 참조하면 본 발명의 실제적 구현화는 명확해진다. 물론 본 발명에서 구체적으로 실시되는 것은 하기에서 설명하는 실시예들에는 다른 종래의 기술들로서도 구현이 가능하다. 아래 설명하는 구체적 실시예들은 발명의 사상을 한정하려는 것이 아니라, 본 발명 사상을 실시하는 하나의 일례로서 이해되어야 하고, 이들에 대한 모든 변경, 균등물 내지 대체물을 포함하는 것을 염두해 두어야 한다. 그리고 본 출원에서 사용한 용어는 단지 특정한 실시 예를 설명하기 위해 사용된 것으로 감안해야 할 것이다.For the features and advantages of the present invention, and a method of performing them, referring to the embodiments described below in detail with reference to the accompanying drawings, the actual implementation of the present invention will become clear. Of course, what is specifically implemented in the present invention can be implemented as other conventional techniques in the embodiments described below. The specific embodiments described below are not intended to limit the spirit of the invention, but should be understood as one example of implementing the spirit of the present invention, and it should be kept in mind that all changes, equivalents, and substitutes for them are included. And it should be considered that the terms used in the present application are only used to describe specific embodiments.

이하, 첨부된 도면을 참조하여 본 발명에 따른 공, 수중 가변드론에 대한 바람직한 실시예를 상세하게 설명한다.Hereinafter, with reference to the accompanying drawings will be described in detail a preferred embodiment of the air, underwater variable drone according to the present invention.

도면 1과 도면 2를 설명하자면, 본 발명의 특징인 주날개(21)와 주모터(22)가 포함된 상기 주회전부(20)가 상기 주회전부하우징(30)의 내측면에 구비된다. 상기 도면 1과 상기 도면 2는 상기 드론본체(10)가 공중비행시의 형태적 특징을 보인 상면도와 측면도이다. 도면에서 보는 바와 같이 상기 드론본체(10)가 공중비행시에는 상기 주회전부(20)가 구비되어 있는 다수개의 상기 주회전부하우징(30)의 내측면이 외부로 완전히 드러나게 개방한다. 이때 상기 주회전부하우징(30) 하단의 드론본체(10)와의 연결 부분은 여닫이방식(폴딩)으로 개방과 폐쇄가 가능하다. 도면 3은 종래의 웜 기어(Worm Gear)에 의한 구현된 원격제어시의 상기 주회전부하우징(30)의 개방과 폐쇄의 구조도이다. 물론 이것은 상기 주회전부하우징(30)의 개방과 폐쇄를 원격제어에 의한 여닫이 방식을 구현한 일례이며 다른 방식인 유압식, 공압식 혹은 서모모터를 이용하는 방식등의 다양한 종래의 기술들이 존재한다. 다만 여기서는 여러방식중 기어방식을 사용하여 발명의 사상을 구현하였다.Referring to Figs. 1 and 2, the main rotor 20 including the main blade 21 and the main motor 22, which are features of the present invention, is provided on the inner side of the main rotation load housing 30. 1 and 2 are a top view and a side view showing the morphological characteristics of the drone body 10 during aerial flight. As shown in the drawing, when the drone main body 10 is in midair, the inner surfaces of the plurality of main rotating load housings 30 provided with the main rotating part 20 are completely exposed to the outside. At this time, the connection portion with the drone body 10 at the bottom of the main rotating load housing 30 can be opened and closed by an opening and closing method (folding). 3 is a structural diagram of opening and closing of the main rotating load housing 30 during remote control implemented by a conventional worm gear. Of course, this is an example of implementing the opening and closing method by remote control of the opening and closing of the main rotating load housing 30, and there are various conventional techniques such as a hydraulic type, a pneumatic type, or a method using a thermomotor, which is another method. However, here, the idea of the invention was implemented by using a gear method among several methods.

상기 주회전부하우징(30)의 내측면이 외부로 완전히 드러나게 되면 자동적으로 상기 주회전부(20) 역시 외부로 완전히 개방이 되는 구조이기 때문에 상기 주회전부(20)는 회전구동이 가능하여 양력을 발생시킬 수 있다. 즉 공중에서는 통상적인 회전익 드론의 형태를 갖추게 되어 상기 드론본체(10)는 공중으로의 비행이 가능한 것이다.When the inner surface of the main rotational load housing 30 is completely exposed to the outside, the main rotational part 20 is also completely open to the outside, so the main rotational part 20 can be rotated to generate lift. I can. That is, in the air, the drone body 10 is capable of flying in the air because it has the form of a conventional rotorcraft drone.

도면 3과 도면 4는 반대로, 다수개의 상기 주회전부하우징(30)의 양측면들이 서로가 맞닿게 되어 접혀지면서 완전히 폐쇄가 이루어지면 상기 주회전부하우징(30)의 내측면에 구비되어 있는 상기 주회전부(20)는 상기 드론본체(10) 내부로 자연스럽게 수납이 이루어진다. 그리고 상기 드론본체(10)는 항해에 적합한 잠수함이나 어뢰같은 형태적 변환이 이루어지기 때문에 수상이나 수중같은 항해주행에 적합하게 된다.3 and 4 are opposite to each other, when both sides of the plurality of main rotating load housings 30 come into contact with each other and are folded and completely closed, the main rotating part provided on the inner surface of the main rotating load housing 30 ( 20) is naturally received inside the drone body 10. In addition, the drone body 10 is suitable for sailing, such as water or underwater, because the form of a submarine or torpedo suitable for navigation is made.

상기 드론본체(10) 내부에는 압축공기실(61), 공기압축기(62)를 포함하는 상기 부력장치부(60)가 구비된다. 상기 주회전부하우징(30)의 폐쇄로 형성된 내부공간은 항해주행시 부상과 잠수를 위한 상기 부력실(63)로서 외부의 물을 입수및 배출할 수 있는 공간으로서 활용이 가능하다. 상기 드론본체(10)는 잠수와 부상을 가능하게 한다. 상기 드론본체(10) 하단에는 보조날개(41)와 보조모터(42)를 포함하는 보조회전부(40)의 회전에 의해 항해에서의 추력을 발생시키고 항해의 방향조정을 위한 상기 방향타(51)와 상기 방향타회전축(52)이 포함된 상기 방향장치부(50)가 구비되어 상기 드론본체(10)의 수상 및 수중의 항해주행을 가능하게 한다. 드론본체(10) 외부에 구비된 상기 관측기(90)는 창공 및 해양에서 정찰을 가능하게 하고 상기 관측기(90)에서 관측된 정보를 전송하고, 제어신호를 수신하기 위해 통상적인 드론에서 일반적으로 사용되고 있는 모뎀 및 안테나장치를 포함하는 통신장치부(80)가 구비된다. 그리고 상기 서술한 장치들의 사용자 원격제어를 위해 중앙제어부(100)가 드론본체(10)에 구비된다.Inside the drone body 10, the buoyancy device unit 60 including a compressed air chamber 61 and an air compressor 62 is provided. The inner space formed by the closing of the main rotational load housing 30 can be utilized as a space for receiving and discharging external water as the buoyancy chamber 63 for injuries and diving during sailing. The drone body 10 enables diving and injury. At the lower end of the drone body 10, the rudder 51 and the rudder 51 for adjusting the direction of navigation and generating thrust in the voyage are generated by the rotation of the auxiliary rotating part 40 including the auxiliary wing 41 and the auxiliary motor 42. The directional device 50 including the rudder rotation shaft 52 is provided to enable the drone body 10 to navigate in water and underwater. The observer 90 provided outside the drone body 10 is generally used in a typical drone to enable reconnaissance in the sky and the sea, to transmit the information observed by the observer 90, and to receive control signals. A communication device unit 80 including a modem and an antenna device is provided. In addition, the central control unit 100 is provided in the drone body 10 for remote control of the user of the above-described devices.

도면 5를 간략히 설명하자면,Briefly explaining Figure 5,

상기 드론본체(10)가 잠수선의 수직발사관 및 수평발사관을 통해 무선으로의 제어가 아닌 유선전선을 연결하여 드론사용이 이루어지면 드론본체(10)내부의 배터리(70) 및 부력장치들은 선택적으로 설치 유무의 변경이 가능하다. 그리고 잠수선 내부에 구비된 드론회수기로 전선을 감아서 사용한다면 수중에서도 드론의 회수가 용이해지기 때문에 드론의 지속적인 재사용이 가능하다.When the drone body 10 connects wired wires rather than wirelessly through the vertical and horizontal launch tubes of the diving ship and the drone is used, the battery 70 and buoyancy devices inside the drone body 10 are selectively installed. It is possible to change the presence or absence. In addition, if the wires are wound with a drone retrieval device provided inside the submarine, the drone can be easily recovered even underwater, so that the drone can be reused continuously.

10 : 드론본체
20 : 주회전부
21 : 주날개
22 : 주모터
30 : 주회전부하우징
40 : 보조회전부
41 : 보조날개
42 : 보조모터
50 : 방향장치부
60 : 부력장치부
61 : 압축공기실
62 : 공기압축기
63 : 부력실
70 : 배터리
80 : 통신장치부
90 : 관측기
100 : 중앙제어부10: drone body
20: main rotating part
21: main wing
22: main motor
30: main rotating load housing
40: auxiliary rotating part
41: auxiliary wing
42: auxiliary motor
50: direction device
60: buoyancy device unit
61: compressed air chamber
62: air compressor
63: buoyancy chamber
70: battery
80: communication device unit
90: observer
100: central control unit

Claims (5)

공중 비행 및 수상, 수중에서의 항해가 가능한 드론에 있어서;
상기 드론본체(10)에 형성되는 다수개의 상기 주회전부하우징(30); 상기 주회전부하우징(30)의 내측면으로 주회전부(20)가 각각 대응되어 구비되고, 상기 주회전부하우징(30)이 여닫이 방식으로 펼쳐져 완전한 개방이 되는 경우, 상기 주회전부하우징(30)의 내측면에 구비되어 있는 상기 주회전부(20) 역시 자동적으로 외부로 개방됨에 따라 상기 드론본체(10)은 비행주행에 적합한 형태를 제공하여 공중에서의 비행이 가능하고, 반대로 다수개의 상기 주회전부하우징(30)의 양측면이 서로가 맞닿으면서 완전히 접혀져 폐쇄가 될시, 상기주회전부(20)가 드론본체(10)내부로의 수납이 되면서, 상기 드론본체(10)는 항해주행에 적합한 유선형으로의 형태적 변환이 이루어지는 특징을 가지는 공중과 수중에서의 형태적 변환을 이루는 드론.In the drones capable of air flight, sea and underwater navigation;
A plurality of main rotating load housings 30 formed on the drone body 10; When the main rotation part 20 is provided correspondingly to the inner surface of the main rotation load housing 30, and the main rotation load housing 30 is unfolded in an opening/closing manner to be completely opened, the inner side of the main rotation load housing 30 As the main rotation unit 20 provided on the side is also automatically opened to the outside, the drone body 10 provides a form suitable for flight operation, allowing flight in the air, and conversely, a plurality of the main rotation load housings ( When both sides of 30) are completely folded and closed while being in contact with each other, the main rotating part 20 is accommodated inside the drone body 10, and the drone body 10 is in a streamlined shape suitable for navigation. A drone that achieves morphological transformation in the air and underwater with the characteristic of morphological transformation. 청구항 1에 있어서 상기 드론본체(10)의 하단부에는 항해시 추력을 발생시키는 상기 보조날개(41)와 상기 보조모터(42)를 포함하는 상기 보조회전부(40)가 구비되고 항해주행시 방향조정을 위한 상기 방향타장치부(50)가 구비되며 상기 드론본체(10) 내부에는 상기 드론본체의 잠수와 부상을 위한 상기 부력장치부(60)가 구비되는 것을 특징으로 하는 공중과 수중에서의 형태적 변환을 이루는 드론.The method according to claim 1, wherein the lower end of the drone body 10 is provided with the auxiliary blade 41 and the auxiliary rotating unit 40 including the auxiliary motor 42 for generating thrust during navigation, and for direction adjustment during navigation The rudder device unit 50 is provided, and the drone body 10 is provided with the buoyancy device unit 60 for diving and injuries of the drone body. A drone made up. 청구항 2에 있어서 상기 주회전부하우징(30)의 폐쇄된 공간은 물의 입수와 배출을 가능하게 하여 상기 드론본체의 부상과 잠수를 가능하게 하는 상기 부력실(63)로서 활용이 되는 것을 특징으로 하는 공중과 수중에서의 형태적 변환을 이루는 드론.The aerial according to claim 2, wherein the closed space of the main rotational load housing (30) is utilized as the buoyancy chamber (63) that enables the intake and discharge of water to enable the drone body to float and dive. A drone that achieves morphological transformation in and underwater. 청구항 1에 있어서 상기 드론본체(10)에 관측기를 구비하여 창공과 해양에서의 환경을 관측하고 관측기에 의해 수집된 정보를 전송하고, 제어신호를 수신하기 위해 통신장치부(80)를 구비하는 것을 특징으로 하는 공중과 수중에서의 형태적 변환을 이루는 드론.The method according to claim 1, wherein the drone body (10) is provided with an observer to observe the environment in the sky and the sea, to transmit information collected by the observer, and to provide a communication device (80) to receive a control signal. A drone that achieves morphological transformation in the air and underwater. 청구항 1, 2, 3, 4항에 있어서 상기 서술한 장치들은 드론본체(10)의 중앙제어부(100)에 의해 상기 장치들은 사용자 원격적 제어가 가능하고 공중과 수중에서의 형태적 변환을 이루는 드론.According to claim 1, 2, 3, 4, the above-described devices are remotely controlled by the user by the central control unit (100) of the drone body (10), and are drones that achieve morphological transformation in the air and underwater. .
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113459739A (en) * 2021-07-28 2021-10-01 复旦大学 Multifunctional triphibian unmanned aerial vehicle for water, land and air

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113753220B (en) * 2021-07-06 2022-10-21 南京航空航天大学 Water-air amphibious multi-rotor aircraft capable of being automatically folded and working method thereof

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060032976A1 (en) * 2004-01-20 2006-02-16 Bachmeyer Paul J Aircraft front nose landing gear and method of making an aircraft landing gear
KR20100065229A (en) * 2008-12-07 2010-06-16 김종서 Helicopter high speed propulsion auxiliary rotor.
US20150021434A1 (en) * 2013-07-19 2015-01-22 Icon Aircraft, Inc. Self-orienting aircraft landing gear
US20160016649A1 (en) * 2013-03-12 2016-01-21 Fairfield Industries Incorporated D/B/A Fairfieldnodal Autonomous Underwater Vehicle Hover Apparatus, Method, and Applications
KR20160072445A (en) * 2014-12-15 2016-06-23 한국항공우주연구원 Drone for saving a life on the sea
US20160332726A1 (en) * 2015-05-12 2016-11-17 Messier-Bugatti-Dowty Aircraft undercarriage with shimmy-damping means
US20170029101A1 (en) * 2015-06-25 2017-02-02 Riderless Technologies Inc. Unmanned aerial vehicle
KR20170111589A (en) * 2016-03-29 2017-10-12 성균관대학교산학협력단 Transformable drone
KR20180064137A (en) * 2016-12-05 2018-06-14 이충열 Quad copter with switchable camcorder handle
US20180304984A1 (en) * 2015-12-25 2018-10-25 Powervision Robot Inc. Aircraft and outer shell therefor
KR20190025790A (en) * 2017-09-01 2019-03-12 주식회사 레템 Underwater glider

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060032976A1 (en) * 2004-01-20 2006-02-16 Bachmeyer Paul J Aircraft front nose landing gear and method of making an aircraft landing gear
KR20100065229A (en) * 2008-12-07 2010-06-16 김종서 Helicopter high speed propulsion auxiliary rotor.
US20160016649A1 (en) * 2013-03-12 2016-01-21 Fairfield Industries Incorporated D/B/A Fairfieldnodal Autonomous Underwater Vehicle Hover Apparatus, Method, and Applications
US20150021434A1 (en) * 2013-07-19 2015-01-22 Icon Aircraft, Inc. Self-orienting aircraft landing gear
KR20160072445A (en) * 2014-12-15 2016-06-23 한국항공우주연구원 Drone for saving a life on the sea
US20160332726A1 (en) * 2015-05-12 2016-11-17 Messier-Bugatti-Dowty Aircraft undercarriage with shimmy-damping means
US20170029101A1 (en) * 2015-06-25 2017-02-02 Riderless Technologies Inc. Unmanned aerial vehicle
US20180304984A1 (en) * 2015-12-25 2018-10-25 Powervision Robot Inc. Aircraft and outer shell therefor
KR20170111589A (en) * 2016-03-29 2017-10-12 성균관대학교산학협력단 Transformable drone
KR20180064137A (en) * 2016-12-05 2018-06-14 이충열 Quad copter with switchable camcorder handle
KR20190025790A (en) * 2017-09-01 2019-03-12 주식회사 레템 Underwater glider

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113459739A (en) * 2021-07-28 2021-10-01 复旦大学 Multifunctional triphibian unmanned aerial vehicle for water, land and air
CN113459739B (en) * 2021-07-28 2022-06-14 复旦大学 Multifunctional triphibian unmanned aerial vehicle for water, land and air

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