KR101863157B1 - Folding-type Unmanned Aerial Vehicle able to be carried by the portable Bag - Google Patents

Abstract

The present invention relates to an unmanned aerial vehicle including: a main body having a set height in an up-down direction to be capable of accommodating a control unit for controlling and supplying power to the unmanned aerial vehicle including a battery; a plurality of arms coupled with the main body to be capable of supporting a foldable propeller and a drive unit driving the propeller; and a landing unit coupled with each arm for landing of the main body, in which the arm is provided with a fixed arm coupled with the main body and a folding arm extending from the fixed arm and the folding arm includes an arm folding unit coupled with the folding arm and the fixed arm to be sequentially folded toward the adjacent fixed arm. According to the present invention, a folding-type unmanned aerial vehicle can be provided that can be stored and carried in a portable bag after the configuration of the unmanned aerial vehicle is folded in a simpler and more convenient manner.

Description

BACKGROUND OF THE INVENTION 1. Field of the Invention [0001] The present invention relates to a Folding-type Unmanned Aerial Vehicle

The present invention relates to a folding unmanned aerial vehicle, and more particularly, to a foldable unmanned aerial vehicle structure for unmanned aerial vehicles capable of accommodating unmanned aerial vehicles in a portable bag for the convenience of the user in the course of transporting or storing a mountain area, And a folding unmanned aerial vehicle.

A small flying object that can be adjusted using radio waves is called a 'unmanned aerial vehicle' and is called a 'dragon'. Unmanned aerial vehicles are equipped with cameras, various sensors, communication systems, etc. They are small to large and various sizes. Unmanned aerial vehicles were first created for military use, but recently they have been expanded to high-end shooting and delivery. Unmanned aerial vehicles can also spray pesticides or pick fruits in high positions. It is also used to provide information such as weather to visitors who visit mountains in mountainous areas, such as Korea, to control visitors to controlled areas, to check the progress of forest fires during the occurrence of forest fires, and to control personnel. The unmanned aerial vehicle utilized for this purpose is provided with a broadcasting module including a speaker.

In the prior art, a broadcasting module and a sensor sensitive to an electromagnetic wave are mounted on an unmanned aerial vehicle together with a speaker which must overcome a noise of a propeller and generate a high-output sound wave, so that electromagnetic waves generated from a high- There is a possibility of affecting.

In addition, the unmanned aerial vehicle is required to have a propeller for flight, and a plurality of such propellers are attached to the end portion of the arm, and thus the propeller tends to be bulky as a whole. Such large-volume unmanned aerial vehicles require large packaging containers and large spaces for transportation and storage.

Accordingly, the unmanned aerial vehicle can block the electromagnetic waves generated by the broadcasting module while broadcasting more easily, and can reduce the size when not carrying the portable or storing the air, so that it is easy to carry, store and transport, .

[Related literature]

Patent Registration No. 10-1804333 (Announcement of Dec. 4, 2017)

SUMMARY OF THE INVENTION It is an object of the present invention to provide a folding unmanned aerial vehicle capable of folding the configuration of an unmanned aerial vehicle in a simple and convenient manner and storing the same in a portable bag.

Another object of the present invention is to provide a folding unmanned aerial vehicle that requires simple, convenient, and less space for transportation, storage, and movement of the unmanned aerial vehicle.

An object of the present invention is to provide an unmanned aerial vehicle including a main body having a height set vertically so as to accommodate a control unit for controlling and powering the unmanned aerial vehicle including a battery; A plurality of arms coupled to the main body to support a folding propeller and a driving unit for driving the propeller; A landing coupled to each arm for allowing the body to land; and an arm comprising: a fixed arm coupled to the body; and a folding arm extending from the fixed arm, And an arm folding unit coupled to the folding arm and the fixed arm so as to be sequentially folded toward the rear side.

The landing folding unit may further include a landing folding unit coupled to the fixing arm such that a pair of the landing units facing each other is folded while intersecting the lower side of the main body.

The arm folding unit may include an arm hinge member coupled to one side of the arm such that the folding arm is rotatable with respect to the fixed arm and a folding position where the folding arm is rotated with respect to the fixed arm, And an arm clamp member coupled to the other side of the arm so as to be movable.

The landing part includes four landing parts. The two landing parts of the opposite landing parts cross each other and are folded on the lower side of the main body. When the landing parts of the landing part are folded in an intersecting manner, To the arm.

The apparatus may further include an arm end fixing member for fixing the end side of the folding arm in a state where the folding arm is folded toward the adjacent fixed arm side.

Preferably, the landing folding unit includes a landing clamp coupled to the fixed arm, and a landing hinge coupled to the landing unit, the landing unit having one side rotatably coupled to the landing clamp and the other side coupled to the landing unit.

The apparatus may further include a camera and a broadcast facility provided integrally with the main body so as to be detachable from the main body, wherein the arm is folded by the arm folding unit to fix the main body to the side of the main body and folds the landing unit into the landing folding unit, A folding unmanned aerial vehicle receiving portion for receiving the folded unmanned aerial vehicle fixed; An emergency battery other than the battery, and a component accommodating portion for accommodating the component including the camera and the broadcast facility detachable from the main body; A user can be accommodated in a portable bag which is partitioned by a user and accommodated in a portable storage bag which can be carried by the user while the unmanned aerial vehicle is partitioned into a manipulator accommodating portion in which a manipulator capable of adjusting and manipulating operations including landing and flying is accommodated desirable.

According to the present invention, it is possible to provide a folding unmanned aerial vehicle that can fold and fold the configuration of an unmanned aerial vehicle more easily and conveniently, and can be carried and stored in a portable bag.

In addition, it is possible to provide a folding unmanned aerial vehicle that requires simple, convenient, and less space for transportation, storage, and movement of the unmanned aerial vehicle.

FIG. 1A is a perspective view of an unmanned aerial vehicle according to an exemplary embodiment of the present invention,
FIG. 1B is a perspective view of FIG. 1A,
FIG. 2 is an enlarged perspective view of a folding part which is a substantial part of FIG. 1A;
FIGS. 3A and 3B are a perspective view of the landing folding unit and a perspective view of the landing hinge block,
3C is a perspective view illustrating a rotating process of the landing folding unit,
FIG. 3D is a view for explaining a state in which the landing portion is inclined at an angle set in the vertical direction,
4A is a view showing an arm folding portion,
4B is a perspective view for explaining the rotation process of the arm folding unit,
FIGS. 5A and 5B are a perspective view of the folding unmanned aerial vehicle, which is a folded unmanned aerial vehicle,
FIG. 5c is a photograph showing a folded state of the propeller and the arm of the unmanned aerial vehicle according to another embodiment,
6 is a perspective view showing a state in which a folding unmanned aerial vehicle, parts, and a regulator are accommodated in a portable bag.

A folding unmanned aerial vehicle (hereinafter referred to as 'unmanned air vehicle') which can be carried by a portable bag according to an embodiment of the present invention and other embodiments will be described in detail with reference to FIGS. 1A to 6B.

1A is a perspective view of an unmanned aerial vehicle according to an embodiment of the present invention. FIG. 1B is a perspective view of the unmanned aerial vehicle according to the present invention. FIG. 3C is a perspective view for explaining the rotation process of the landing folding unit, FIG. 3D is a view for explaining a state in which the landing unit is inclined at a predetermined angle in the vertical direction, FIG. 4A 5A and 5B are perspective views of a folding unmanned aerial vehicle, which is a folded unmanned aerial vehicle, as viewed from above and from below, and FIG. 5C is a perspective view showing another embodiment FIG. 6 is a photograph showing the folded unmanned aerial vehicle, the parts and the regulator being housed in a portable bag; FIG. Degrees.

The unmanned aerial vehicle 100 according to an embodiment of the present invention includes a main body 111 for receiving a control unit (not shown) for controlling and powering the unmanned aerial vehicle including a battery, Wow; An arm 130 coupled to the main body 111 and extending from the main body 111 so as to be able to support a driving part 117 for driving the propeller 113 and the propeller 113; A landing part 150 coupled to each arm 130 so that the main body 111 can land on the ground or the like; the arm 130 includes a fixed arm 133 coupled to the main body 111, The folding arm 134 is extended from the fixed arm 133 so that the folding arm 134 is folded along the main body 111 toward the adjacent fixed arm 133, And an arm folding part 135 coupled to the fixed arm 133. [ The unmanned air vehicle 100 further includes a broadcasting module (not shown) including a speaker 115 detachably coupled to the main body 111 and capable of broadcasting, and a camera (not shown) .

The main body 111 includes a battery (not shown) for supplying power to the inside of a general unmanned aerial vehicle, a GPS function basically required for flight, a posture function, a speed function, a pivot function, (Not shown) and a control unit for controlling, controlling, and communicating functions related to the operation of the control unit (not shown), low voltage, forced return of the take-off point, The main body 111 is disposed at the center of the UAV 100 to maintain the overall balance.

The main body 111 may further include an imaging module (not shown) including a camera capable of photographing a desired point or place while flying, and a broadcasting module (not shown) capable of broadcasting if necessary . With this broadcasting module, it is possible to transmit desired contents to a relatively wide place or a large number of target persons required by the user.

The propeller 113 is driven by a driving unit 117 including a motor so that the unmanned air vehicle 100 can fly and provides lifting force to the unmanned air vehicle 100. The propeller 113 is coupled to the main body 111, (Not shown). In this embodiment, a total of four propellers 113 are provided in the direction of 90 degrees. Here, the propeller 113 according to an embodiment of the present invention preferably has a known folded shape.

In addition, it is preferable that the material of the unmanned aerial vehicle 100 includes carbon, aluminum, or an alloy thereof having a high strength while reducing weight. For example, a pipe, a bracket, a block, and the like included in the arm 130 and the folding device (the arm folding part 135 and the landing folding part 170) are preferably made of a carbon material or an aluminum material. Bolts, It is preferable to include stainless steel having high corrosion resistance.

The driving unit 117 includes a motor for driving the propeller 113 and a control unit for driving the motor and is coupled to the end of the arm 130 to rotate the propeller 113, And is electrically connected and operated through electric wires through the internal space of the arm 130 and the like.

The arm 130 is coupled to the main body 111 and is provided at four, for example, in a direction of 90 degrees, and has a structure in which the propeller 113 and the driving unit 117 can be supported on the end side. The arm pipe 1210, which is a rod-shaped long support of the arm 130, is, for example, a circular pipe and its material is preferably carbon.

The arm 130 includes a fixed arm 133 fixed to a bracket not shown in the main body 111 and a folding arm 134 coupled to and extending from the fixed arm 133 to support the propeller 113 at an end thereof. . The fixed arm 133 and the folding arm 134 are coupled by the arm folding portion 135 so that the folding arm 134 can be folded toward the adjacent fixed arm 133 side.

4A and 4B, the arm folding section 135 includes a fixed arm bracket 135a coupled to a pipe-shaped outer end of the fixed arm 133, and a fixed arm bracket 135b coupled to the fixed arm bracket 135a and the arm hinge And a folding arm bracket 135b coupled to the pipe-shaped inner end of the folding arm so as to be rotatably hinged to the fixed arm 133 by the fixing arms 135c.

The arm folding section 135 is formed with clamping protrusions 135a1 protruding from opposite sides of the arm hinges 135c of the fixed arm bracket 135a and the folding arm bracket 135b. And an arm clamp 135d coupled to the clamp projection 135a1 so that the fixed arm 133 can be fixed to the folding arm 134 at one end.

The arm clamp 135d includes a clamp bolt 135d1 that is hingedly coupled to the clamp projection 135a1 of the folding arm bracket 135b in the form of a bolt and a clamp bolt 135d1 that is hinged to the clamp projection 135a1 of the folding arm bracket 135b. And a clamp fixing member 135d2 having a cam shape and having a clamping structure by rotating when the clamp bolt 135d1 is fixed to the clamp protrusion 135a1.

The arm folding part 135 is connected to the landing clamp 173 so as to fix the folding arm 134 folded toward the adjacent fixed arm 133 in a folded state as shown in FIG. It is preferable that the folding arm fixing member 137 is further included. The folding arm fixing member 137 can have an elastic deformable shape of 'C' to the extent that the pipe of the folding arm 134 is engaged so that the folding arm 134 can not be pulled out unless the user applies a force, thereby stably fixing the folding arm 134.

With this structure, the process of folding the arm folding part 135 in the clockwise direction as shown in FIG. 5A toward the adjacent arm 130 along the side surface of the main body 111 will be described with reference to FIGS. 4A and 4B Then,

4A and 4B is a state in which the folding arm 134 is fixed by the arm clamp 135d coupled to the fixed arm 133, And the shape center axis is 'Y3').

4B, the user unlocks the clamp fixing member 135d2 of the arm clamp 135d from the clamp bolt 135d1 to rotate the folding arm 134 in the clockwise direction with respect to the arm hinge 135c with respect to the fixed arm 133 The folding arm 134 rotates toward the adjacent fixed arm 133 and the pipe of the folding arm 134 can be engaged and fixed to the folding arm fixing member 137 of the adjacent fixed arm 133 Y3 'to' Y4 ').

Each of the folding arms 134 may be folded along the side surface of the main body 111 in the clockwise direction toward the adjacent fixed arms 133 by the arm folding unit 135 to be in a state as shown in FIG. 5A. Here, the propeller 113 does not hold the folded state at first.

The lateral and longitudinal outline dimensions of the folding unmanned aerial vehicle, which is the unmanned flying vehicle 100 folded by this structure, can be close to the outer dimensions formed by the arm 130.

The landing unit 150 includes a rod-shaped landing pipe 181 having a hollow centered on a carbon material and a landing pipe 181 coupled to the fixed arm 133 so that the main body 111 can land on the ground or the like And a landing folding portion 170 having a structure that can be folded into a folding position that is folded inward from the flying position to the inside of the lower portion of the main body 111. [

The landing folding section 170 includes a landing hinge 175 which is coupled to the landing pipe 181 and allows the landing pipe 181 to be folded as shown in Figures 3A to 3D, 175 and the other side is coupled to a fixed arm 133 to provide a landing clamp 173 for supporting the landing hinge 175. [

The landing clamp 173 includes a pair of arm fixing clamps 173a penetrating through the center and engaged to surround the fixing arm 133 and two parallel arm fixing clamps 173a coupled to the respective side walls of the pair of arm fixing clamps 173a. And a landing folding bracket 173b in the form of a plate.

The landing folding bracket 173b is rotatably coupled to a landing hinge block 175a to be described later. The landing folding bracket 173b is provided in a shape of two parallel plates. The landing folding bracket 173b includes a fixed hinge shaft hole 173b1, 173b1, a folding rotation guide 173b3, and a folding position guide groove 173b4.

The stationary hinge shaft hole 173b1 is coupled with a fixed hinge shaft 175a1 which serves as a rotation center of a landing hinge block 175a described later.

The fixed position guide groove 173b1 is formed at one side of the folding rotation guide 173b3 so that the floating hinge shaft 175a2 is engaged with the landing pipe 181 so that the landing pipe 181 can be held at a flying position where the landing hinge block 175a is rotated .

The folding rotation guide 173b3 is provided with a cutting circumferential shape capable of guiding the turning hinge shaft 175a2 in the course of folding and unfolding of the landing pipe 181 with a turning radius set so as to be movable with respect to the fixed hinge shaft 175a1 .

The fixed position guide groove 173b1 is provided on the other side of the fixed position guide groove 173b1 of the folding rotation guide 173b3 so as to maintain the folded state of the landing pipe 181 in the lower side of the main body 111, The folding rotation guide 173b3 is closed so as to prevent the folding guide 173b3 from being further folded.

With this structure, the landing hinge block 175a can rotate more smoothly and reliably between the flying position and the folding position, so that the landing pipe 181 can be stably folded and unfolded.

The landing hinge 175 may be coupled between the landing clamps 173 to fold and unfold the landing pipe 181 as shown in Figures 3A and 3B and may include a fixed hinge shaft 175a1, 175a2, a flow elastic member 175a3, a flow slot 175a4, and a landing pipe fixing plate 175b.

The landing hinge block 175a has two rectangular hexahedral shapes and is coupled to each of the landing folding brackets 173b and includes a fixed hinge shaft 175a1, a flow hinge shaft 175a2, a flow elastic member 175a3, (175a4) and the landing pipe fixing plate (175b).

One side of the fixed hinge axis 175a1 is coupled to the landing hinge block 175a and the other side including the landing hinge block 175a is rotatable relative to the landing folding bracket 173b while the other side is connected to the landing hinge block 175a And is coupled to the fixed hinge shaft hole 173b1. The fixed hinge shaft 175a1 is fixed to the fixed hinge shaft hole 173b1 so that the fixed hinge shaft 175a1 does not come out of the fixed hinge shaft hole 173b1 and the space for maintaining the space between the component and the two landing hinge blocks 175a And the like will not be described in more detail, and the flow hinge shaft 175a2 is also the same in the following.

The flow hinge shaft 175a2 is coupled to the fixed hinge shaft 175a1 of the landing hinge block 175a and to the fixed hinge shaft 175a1 which is fixedly coupled to the fixed hinge shaft 175a1 by the flow elastic member 175a3 And has a structure capable of elastically deforming.

That is, the inside of the flow hinge shaft 175a2 is elastically deformably coupled to the flow slot 175a4 of the landing hinge block 175a by the fixed hinge shaft 175a1 and the flow elastic member 175a3, The folding rotation guide 173b3, and the folding position guide groove 173b4 of the landing folding bracket 173b.

The lower side of the pair of landing hinge blocks 175a is coupled by a single plate-shaped landing pipe fixing plate 175b and the landing pipe 181 is firmly fixed to a central region of the landing pipe fixing plate 175b have.

5B, when the landing pipe 181 is folded on the lower side of the main body 111, the landing pipes 181 of the pair of opposed or opposing landing portions 150 cross each other, The center axis (refer to 'Y1' in FIG. 3D) of the landing pipe 181 is set to a predetermined angle (see FIG. 3D) with respect to the vertical axis direction of the main body 111 or the landing folding unit 170 It is preferable that the landing pipe 181 is coupled to the landing pipe fixing plate 175b so as to be inclined to the landing pipe fixing plate 175b.

A process of folding the landing pipe 181 by this structure will be described with reference to FIG. 3C.

First, the states of FIGS. 3A and 3C are the flight positions where the unmanned air vehicle 100 can fly.

Next, when the user folds the landing folding part 170 of the landing part 150 or the landing pipe 181 to the inside of the main body 111, the user holds the landing pipe 181 near the landing folding part 170, The landing pipe 181 is forced to rotate in the direction toward the inside of the main body 111. [

The pressurized force overcomes the elastic force of the flow elastic member 175a3 that seats the flow hinge shaft 175a2 in the fixed position guide groove 173b1, so that the flow elastic member 175a3 is stretched. As the flow hinge shaft 175a2 is moved away from the fixed hinge shaft 175a1 and the flow hinge shaft 175a2 is moved out of the fixed position guide groove 173b1 along the direction of the urged force and the folding rotation guide 173b3 is rotated, Thereby rotating in the counterclockwise direction. The landing hinge block 175a, the flow elastic member 175a3, the landing pipe fixing plate 175b and the landing pipe 181 rotate in the same direction in accordance with the rotation of the flow hinge shaft 175a2. The rotating hinge shaft 175a2 which has been rotated along the folding rotation guide 173b3 is caught by the folding position guide groove 173b4 and can not be rotated any more and can be kept in a state of being collapsed on the lower side of the main body 111. [ This folded state can be maintained because the elastic force of the flow elastic member 175a3 is applied to the flow hinge shaft 175a2 to generate a frictional force between the flow hinge shaft 175a2 and the folding rotation guide 173b3.

The folded unmanned aerial vehicle folded by such a structure can maintain a very minimized height including the main body 111.

5C, which is another embodiment of the present invention, the inventors of the present invention have confirmed that the dimensions of the unmanned aerial vehicle before folding (the state in which the propeller is maximally deployed and the collapsed state can be confirmed as shown in the following table).

Before folding (cm) After folding (cm) horizontal Vertical Height horizontal Vertical Height 112.7 112.7 41.6 43 43 27.5

In the above example, it can be confirmed that the volume after folding is 9.7% of the volume before folding. It can be confirmed that the volume before folding and the volume difference after folding are very large.

On the other hand, the folding unmanned aerial vehicle of this folded state is very convenient because it can be carried and used when it is used in a rough region such as a mountainous region, a book region, and a region where a vehicle can not be moved, FIG.

That is, a detachable component is attached to and detached from the main body 111 of the camera and the speaker in the unmanned flying vehicle 100, and the entire volume (horizontal, vertical, and vertical) Height) can be accommodated in a portable bag.

First, the folding unmanned air vehicle receiving unit 210, which is an area for accommodating the folding unmanned air vehicle 100, occupies the widest part, and a speaker or a camera (interfering with a landing pipe folded on the lower side of the main body, A component accommodating portion 230 capable of storing a removable and removable battery in the main body 111 and a component accommodating portion 230 for accommodating the unmanned air vehicle 100 such as flying and returning, The user can carry and move the portable bag 200 in a rugby condition necessary for the user to carry it. In addition, the portable bag 200 can be utilized not only for moving to the rough but also for moving to a vehicle or storing and transporting the unmanned air vehicle 100. [

The inventor can confirm that the volume of the portable bag 200 is 68 cm in width, 50 cm in length, and 29 cm in height, even if the volume of the bag for preventing the buffering is included, when the unmanned flying vehicle 100 is placed in the portable bag. It is possible to improve the portability of the user.

Therefore, according to the present invention, it is possible to provide a foldable unmanned aerial vehicle that can fold and fold the configuration of an unmanned aerial vehicle more easily and conveniently and can be stored in a portable bag.

In addition, it is possible to provide a folding unmanned aerial vehicle that requires simple, convenient, and less space for transportation, storage, and movement of the unmanned aerial vehicle.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is to be understood that the invention is not limited to the disclosed embodiments, but, on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the invention. The scope of the invention will be determined by the appended claims and their equivalents.

100: unmanned vehicle
111: main body 113: propeller
115: speaker 117:
130: arm 133: fixed arm
134: folding arm 135: arm folding part
135a: Fixed arm bracket 135a1: Clamp projection
135b: folding arm bracket 135c: arm hinge
135d: arm clamp 135d1: clamp bolt
135d2: clamp fixing member 137: folding arm fixing member
150:
170: Landing folding part 173: Landing clamp
173a: arm fixing clamp 173b: landing folding bracket
173b1: Fixed hinge shaft hole 173b2: Fixed position guide groove
173b3: Folding rotation guide 173b4: Folding position guide groove
175: landing hinge 175a: landing hinge block
175a1: fixed hinge shaft 175a2: floating hinge shaft
175a3: Flow elastic member 175a4: Floating slot
175b: landing pipe fixing plate 181: landing pipe
200: Portable bag 210: Folding unmanned air bag
230: parts receiving part 250:

Claims (7)

In an unmanned aerial vehicle,
A main body having a height set vertically so as to accommodate a control unit for controlling and powering the unmanned aerial vehicle including a battery;
A plurality of arms coupled to the main body to support a folding propeller and a driving unit for driving the propeller;
A landing coupled to each arm to allow the body to land;
The arm includes a locking arm coupled to the body and a folding arm extending from the locking arm, wherein the folding arm is configured to be foldably engaged with the folding arm and the arm coupled to the locking arm such that the folding arm is sequentially folded toward the adjacent locking arm. A folding unit;
And a landing folding portion coupled to the fixed arm such that a pair of opposing landing portions are folded while crossing each other at a lower side of the main body,
Wherein the landing folding unit includes a landing clamp coupled to the fixed arm and a landing hinge rotatably coupled to the landing clamp on one side and coupled to the landing unit on the other side. delete The method according to claim 1,
The arm folding unit includes:
And an arm hinge member coupled to one side of the arm such that the folding arm is rotatable with respect to the fixed arm and a folding position where the folding arm rotates with respect to the fixed arm and a folding position where the folding arm is fixed with respect to the fixed arm, And an arm clamp member coupled to the other side. The method according to claim 1,
The landing unit includes four landing units. The two landing units are mutually intersected and folded on the lower side of the main body. When the landing units are folded, the landing units are inclined in different directions with respect to the vertical direction And wherein the arm is coupled to the arm. The method according to claim 1,
Further comprising an arm end fixing member for fixing the end side of the folding arm in a state where the folding arm is folded toward the adjacent fixing arm side. delete The method according to claim 1,
Further comprising a camera and a broadcast facility provided integrally with the main body so as to be detachable from the main body,
A folding unmanned air vehicle receiving portion for receiving the folding unmanned air vehicle having the arm folded by the arm folding portion and fixed to a side surface of the main body and folding the landing portion to the lower side of the main body by the landing folding portion;
An emergency battery other than the battery, and a component accommodating portion for accommodating the component including the camera and the broadcast facility detachable from the main body;
A user can be carried by a portable bag provided separately from the unmanned aerial vehicle, the unmanned aerial vehicle being partitioned by a user-receivable portion for receiving a manipulator capable of coordinating and manipulating operations including landing and flying, Features unmanned aircraft.

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