KR101808845B1 - Envelope structure which drone is separated and can fly - Google Patents
Envelope structure which drone is separated and can fly Download PDFInfo
- Publication number
- KR101808845B1 KR101808845B1 KR1020150165323A KR20150165323A KR101808845B1 KR 101808845 B1 KR101808845 B1 KR 101808845B1 KR 1020150165323 A KR1020150165323 A KR 1020150165323A KR 20150165323 A KR20150165323 A KR 20150165323A KR 101808845 B1 KR101808845 B1 KR 101808845B1
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- South Korea
- Prior art keywords
- drones
- dron
- drone
- unit
- communication unit
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- 238000000926 separation method Methods 0.000 claims abstract description 47
- 238000004891 communication Methods 0.000 claims description 84
- 230000008878 coupling Effects 0.000 claims description 38
- 238000010168 coupling process Methods 0.000 claims description 38
- 238000005859 coupling reaction Methods 0.000 claims description 38
- 238000000034 method Methods 0.000 claims description 17
- 238000007667 floating Methods 0.000 claims description 16
- 210000004712 air sac Anatomy 0.000 claims description 14
- 238000012423 maintenance Methods 0.000 claims description 14
- 238000003780 insertion Methods 0.000 claims description 13
- 230000037431 insertion Effects 0.000 claims description 13
- 230000000149 penetrating effect Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 9
- 239000007789 gas Substances 0.000 description 14
- 238000012544 monitoring process Methods 0.000 description 12
- 230000005484 gravity Effects 0.000 description 3
- 238000004804 winding Methods 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000003575 carbonaceous material Substances 0.000 description 2
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
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- 229910001120 nichrome Inorganic materials 0.000 description 2
- 238000001514 detection method Methods 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
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- 238000005516 engineering process Methods 0.000 description 1
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Images
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
- B64B1/44—Balloons adapted to maintain predetermined altitude
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
-
- 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
- B64C39/022—Tethered aircraft
-
- 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
- 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
- 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
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
-
- B64C2201/127—
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Selective Calling Equipment (AREA)
Abstract
In the present invention, when a dron is mounted on a drones mounting structure, when a dron separation signal is received by a control unit of the integrated controller, a dron is separated from the dronon mounting structure, It is then possible to carry out the mission assigned to it by flying to the target point. According to the present invention, a surveillance activity can be performed by generating a video signal around the air bag structure through a camera provided in the integrated control device, and when a problem is caught during surveillance, So that it can be quickly loaded into the target point.
Description
The present invention relates to a drones for separating drones mounted on an air bag structure and performing various tasks by flying to a target point when a problem is captured while monitoring the air bag structure around the camera through a camera provided in the integrated control device. The present invention relates to an air-
The drones were originally developed for military purposes, but nowadays they are widely used not only for military use but also for private companies such as private companies and individuals. Specifically, since the drone can fly without a pilot through radio waves, it can be used in hazardous areas where people can not access, collecting various information, or providing unmanned courier service by utilizing GPS technology to confirm its position using a satellite do.
However, in order to allow the drone to perform the assigned task smoothly by putting the drone at the desired place, the surveillance activity must be continued through the camera. At this time, the surveillance activity is performed using the camera provided in the drone There is a possibility that if a drone is needed due to power consumption, it may not be able to fly properly. In addition, in order to monitor the camera, it is necessary to attach the camera to a fixture such as a column or a wall. In the case where the camera is dismantled, the fixture remains on the ground and occupies a space unnecessarily. And efforts are required. Also, in some cases, a structure capable of easily monitoring the surroundings from a very high position from the ground is also required.
On the other hand, Patent Document 1 (Korean Patent Registration No. 10-1543542) discloses an intelligent monitoring system and method for confirming an event and tracking a moving object in real time through image sensing. However, according to the above-mentioned Patent Document 1, only the matters for remotely controlling the drone unit and monitoring the detection area using the image provided from the drone unit are disclosed, and only the camera And the fact that the drones mounted on a structure can be operated to perform a predetermined mission is not disclosed, which is different from the present invention.
The present invention monitors a structure around a structure using a camera, quickly places a dron for a place where a problem occurs (hereinafter, referred to as a "target point"), and at the same time, And to provide an airbag structure capable of smoothly performing an environment in which the airbag can be smoothly performed.
It is another object of the present invention to provide an air-bag structure capable of performing the surveillance and mission as described above, and to provide an air bag structure in which the installation and dismounting work can be easily performed.
In order to achieve the above object, according to a first embodiment of the present invention, there is provided an air bag structure capable of separating and flying a dron, A drones mounting structure, comprising: a support frame; and a fastening portion mounted on the support frame and provided with a fastening portion for holding the fastened state while lifting the dron in the air; A first communication unit for transmitting a video signal generated by the first camera to a drone manipulator, a first communication unit for receiving a dronon flight signal transmitted from the drone manipulator corresponding to a video signal generated by the first camera, A dron including a fixing portion fastened by the fastening portion; A third communication unit for transmitting the image signal generated by the second camera to the ground equipment; an exhaust valve for exhausting the gas injected into the air bag; A fourth communication unit receiving the altitude maintenance signal transmitted from the ground equipment corresponding to the video signal generated by the second camera and receiving the dron separation signal transmitted from the ground equipment; A control unit for receiving the dron separation signal transmitted from the fourth communication unit to release the engagement between the coupling unit and the fixing unit, An integrated control device including a power supply unit for supplying power; An exhaust port connecting the air cylinder and the exhaust valve; And a second connection line connecting an object located on the ground and the droning structure, and a second connection line connecting the droning structure and the integrated control device. When the control unit receives the dron separation signal , The drones are separated from the droning structure as power is supplied to the coupling unit and the coupling between the coupling unit and the fixing unit is released, and the separated drones fly according to the dron flight signal .
According to a second embodiment of the present invention, there is provided an air-bag structure capable of separating and flying a dron, the air bag including a bag for levitating the dron by a gas injected therein; A drones mounting structure, comprising: a support frame; and a fastening portion mounted on the support frame and provided with a fastening portion for holding the fastened state while lifting the dron in the air; A first communication unit for transmitting a video signal generated by the first camera to a drone manipulator, a first communication unit for receiving a dronon flight signal transmitted from the drone manipulator corresponding to a video signal generated by the first camera, A second communication unit for receiving a dron separation signal transmitted from the drone manipulator; a fixed unit coupled by the coupling unit; and a second communication unit for receiving the dron separation signal transmitted from the second communication unit, A drones for releasing the engagement between the drones and the drones, and a drones for supplying power to the drones; A third communication unit for transmitting the image signal generated by the second camera to the ground equipment; an exhaust valve for exhausting the gas injected into the air bag; A fourth communication unit for receiving an altitude maintenance signal transmitted from the ground equipment corresponding to an image signal generated by the second camera; a control unit for receiving the altitude maintenance signal transmitted from the fourth communication unit and controlling the exhaust valve; An integrated controller including a power supply unit for supplying power to the control unit; An exhaust port connecting the air cylinder and the exhaust valve; And a second connection line for connecting the droning structure and the integrated control device, wherein the first connection line connects the object located on the ground and the droning structure, and the second connection line connects the droner structure and the integrated control device, , The drones are separated from the droning structure as power is supplied to the fixing portion and the fastening between the fastening portion and the fixing portion is released, .
According to the present invention, a surveillance activity can be performed by generating a video signal around the air bag structure through a camera (that is, a second camera) provided in the integrated control device. When it is necessary to input a dron during the surveillance activity The drone mounted on the structure can be separated and flown so that the drone can be quickly inserted into the target point.
Further, according to the present invention, the surveillance activity around the air bag structure is performed through the camera (i.e., the second camera) provided in the integrated control device instead of the camera provided in the drones (i.e., the first camera) The power shortage problem that may occur when flying to a point is minimized.
In addition, since the air bag structure according to the present invention can be installed on the ground with only air bags and connecting lines, the installation of the structure and the disassembling operation can be easily performed.
FIG. 1 is a schematic view of an air-bag structure capable of separating and flying a dron according to a first embodiment of the present invention.
FIGS. 2 to 4 are views for explaining how the drone is separated from the drone mounting structure in the air bag structure according to the first embodiment of the present invention.
FIG. 5 is a schematic view of an air-bag structure capable of separating and flying a dron according to a second embodiment of the present invention.
6 to 8 are views for explaining how the drones are separated from the drone mounting structure in the air bag structure according to the second embodiment of the present invention.
Fig. 9 is a view showing a modification of the first embodiment of the present invention.
10 is a view showing a state in which a plurality of auxiliary drones are connected to an auxiliary frame.
11 is a view schematically showing a structure in which a dust container is installed in an air bag structure.
Hereinafter, an air bag structure capable of separating and flying the drones according to the present invention will be described in detail with reference to the accompanying drawings. It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory and are intended to provide further explanation of the invention as claimed. Lt; / RTI > The detailed description of known functions and configurations that may unnecessarily obscure the gist of the present invention will be omitted.
FIG. 1 is a schematic view of an air-bag structure capable of separating and flying a dron according to a first embodiment of the present invention.
In the air bag structure according to the first embodiment of the present invention, when a problem is detected while monitoring the surroundings of the air bag structure through the camera while the dron is lifted and fixed in the air, After the drones are separated, the drones are flown to the target point according to the dron flight signal transmitted from the dronron manipulator, so that the work performed at the target point is transmitted to the dronon controller in more detail, Which is capable of separating a plurality of objects from each other.
To this end, the air bag structure according to the first embodiment of the present invention includes an
The
The
The
The fastening
The
The
The
Here, the video signal transmitted to the drone manipulator means an image captured by the
It may be considered to monitor the circumference of the air bag structure using the
The
The integrated
The integrated
The
The
The
Here, the ground equipment includes a video receiver capable of receiving an image signal generated by the
Here, the image signal generated by the
And an altitude maintenance signal transmitted from the ground equipment means a signal provided by a person who controls the ground equipment through the ground equipment in order to keep the air bag at a desired altitude while watching an image signal generated by the
The dron separation signal transmitted from the terrestrial equipment is transmitted to the terrestrial equipments when a subject controlling the terrestrial equipment performs a surveillance activity through a video signal generated by the
The
The
The
The
The
2 to 4 are views for explaining a state in which the drone is separated from the drone mounting structure. Hereinafter, referring to FIGS. 2 to 4, the
2, the
The
When the
3, the fixing
3B, the
When the
4, the
The
Thereafter, when the
FIG. 5 is a schematic view of an air-bag structure capable of separating and flying a dron according to a second embodiment of the present invention.
In the air bag structure according to the second embodiment of the present invention, when a problem is detected while the surroundings of the air bag structure are monitored through the camera while the dron is lifted and fixed in the air, according to the dron separation signal transmitted from the dron controller After the drones are separated, the drones are flown to the target point according to the dron flight signal transmitted from the dronron manipulator, so that the work performed at the target point is transmitted to the dronon controller in more detail, Which may be provided in the main body of the apparatus. That is, the air bag structure according to the second embodiment of the present invention is different from the air bag structure according to the first embodiment in that a dron separation signal is transmitted from the dron controller to the drone.
The air bag structure according to the second embodiment of the present invention includes the
The
The
The
The
The
The
The
Here, the video signal transmitted to the drone manipulator means an image captured by the
It may be considered to monitor the circumference of the air bag structure using the
Meanwhile, in the air bag structure according to the second embodiment of the present invention, the
The fixing
The
The
The
The
The
The
The
Here, the ground equipment includes a video receiver capable of receiving an image signal generated by the
Here, the image signal generated by the
And an altitude maintenance signal transmitted from the ground equipment means a signal provided by a person who controls the ground equipment through the ground equipment in order to keep the air bag at a desired altitude while watching an image signal generated by the
The
The
The
6 to 8 are views for explaining how the drones are separated from the droning structure in the air bag structure according to the second embodiment of the present invention. 300 are fastened to the
6, the
The
Thereafter, when the
7, the
The
Thereafter, when the
8, the
The
Thereafter, when the
The following description will be made in order to avoid duplication of the first embodiment and the second embodiment of the present invention. In the first embodiment, However, it goes without saying that it can be applied to the second embodiment of the present invention.
Fig. 9 is a view showing a modification of the first embodiment of the present invention.
The supporting
9, the
A
The
Meanwhile, the air bag structure according to the present invention may further include a
The
Here, the
Alternatively, the
On the other hand, the
When one end of the
A
On the other hand, the
Here, the payload separation signal is generated by the main body driving the drone manipulator, flying the
For example, the control subject of the ground equipment may include a video signal generated by the
The dron separation signal transmitted to the
Alternatively, the dron separation signal may be transmitted to the
The
FIG. 10 is a view showing a state where a plurality of auxiliary drones are connected to an auxiliary frame. Referring to FIG. 10, an
Specifically, the at least one
The
An example in which the
As an example in which the
As another example in which the
The
FIG. 11 is a schematic view of the air bag structure having a drone-filled portion. Referring to FIG. 11, a
The
For example, when the
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 exemplary embodiments, but, on the contrary, And variations are possible. Accordingly, it is intended that the technical scope of the present invention be defined only by the appended claims, and all equivalent or equivalent variations thereof fall within the technical scope of the present invention.
100: airbag
200: Structure for drone mounting
210: support frame 220: fastening part
300: Drones 310: First camera
320: first communication unit 330: second communication unit
340: Fixing portion 350: Drone control device
360: Drone battery unit 370:
400: Integrated control device
410: second camera 420: third communication section
430: exhaust valve 440: fourth communication section
450: control unit 460: power supply unit
500: Exhaust
610: first connection line 620: second connection line
700: Pressure holding device 800: Winder
900: Power line 1000: Drone landing plate
1100: Drone charging part
Claims (17)
An air bag for levitating the drones by gas injected therein;
A drones mounting structure, comprising: a support frame; and a fastening portion mounted on the support frame and provided with a fastening portion for holding the fastened state while lifting the dron in the air;
A first communication unit for transmitting a video signal generated by the first camera to a drone manipulator, a first communication unit for receiving a dronon flight signal transmitted from the drone manipulator corresponding to a video signal generated by the first camera, A dron including a fixing portion fastened by the fastening portion;
A third communication unit for transmitting the image signal generated by the second camera to the ground equipment; an exhaust valve for exhausting the gas injected into the air bag; A fourth communication unit receiving the altitude maintenance signal transmitted from the ground equipment corresponding to the video signal generated by the second camera and receiving the dron separation signal transmitted from the ground equipment; A control unit for receiving the dron separation signal transmitted from the fourth communication unit to release the engagement between the coupling unit and the fixing unit, An integrated control device including a power supply unit for supplying power;
An exhaust port connecting the air cylinder and the exhaust valve; And
A first connecting line connecting an object located on the ground and the droning structure, and a second connecting line connecting the droning structure and the integrated controller,
When the control unit receives the dron separation signal, power is supplied to the coupling unit to release the coupling between the coupling unit and the fixing unit, so that the drones are separated from the droning structure, Wherein the airplane is adapted to fly according to the dragon flight signal.
The support frame includes:
An upper support frame having first insertion grooves formed at both ends thereof;
A lower support frame having second insertion grooves formed at both ends thereof;
A frame connection line inserted at a corresponding position of the first insertion groove and the second insertion groove, respectively; And
And a connection line fixing device connected to both ends of the frame connection line to prevent the frame connection line from escaping into the first insertion slot and the second insertion slot.
And a pressure holding device connected to the exhaust port,
Wherein the pressure holding device maintains the pressure of the air bladder in accordance with a preset pressure value according to an altitude of the air bag.
Wherein the power supply unit is supplied with electric power through a power line connected from the ground.
The object located on the ground is a vehicle,
Wherein a power line is connected between the battery and the power supply unit of the vehicle so that power is supplied to the power supply unit from the battery provided in the vehicle through the power line.
The integrated controller further includes a wireless power receiver connected to the power supply,
Wherein the power supply unit is supplied with electric power wirelessly transmitted to the wireless power receiving unit.
Further comprising a winder positioned above the object located on the ground to wind or unwind the first connecting line.
The drone further includes a payload, and the second communication unit receives a payload separating signal transmitted from the drone manipulator,
Wherein the payload is separated from the drones according to the payload separation signal.
Wherein the coupling portion comprises a servo motor, a servo arm connected to the servo motor, and a wire connected between the servo motor and the power supply portion,
The servo arm is fastened to the fixing portion to maintain the drones fixed in the air while being floated,
When the control unit receives the dron separation signal, a current flows through the wire to drive the servo motor, and as the servo arm is disengaged from the fixed unit by driving the servo motor, Wherein the drones are separated from the droning structure.
Wherein the fixing portion comprises a first rectilinear portion, a second rectilinear portion spaced apart in parallel to the first rectilinear portion, and a connecting portion connecting the first rectilinear portion and the second rectilinear portion,
Wherein the engaging portion includes an electromagnet moving bar contact portion protruding from the supporting frame, an electromagnet moving portion having a coil and being spaced apart from and parallel to the electromagnet moving bar contacting portion, one end contacting the electromagnet moving bar contact portion, An electromagnet movement rod accommodated in the movable portion, and a wire connected between the electromagnet movable portion and the electric power supply portion,
The connection portion is fastened in the form of being hooked on the electromagnet movement rod, so that the dron is held in a floating state while floating in the air,
When the control unit receives the dron separation signal, a current flows through the wire, a magnetic force is generated in the coil incorporated in the moving part of the electromagnet, and the electromagnet moving bar is moved by the magnetic force generated in the coil, Wherein the drones are separated from the drone mounting structure.
Wherein the fastening portion has a through-hole structure in which the second connecting line, the through-hole having the through-hole formed therein, through which the second connecting line passes, and the electric line connected to the through- Wire,
The second connection line is fastened to the fixing part to keep the drones floating in the air,
When the control unit receives the dronesignal signal, current flows through the wire, heat is generated in the electric wire provided in the through hole, and the heat generated in the electric wire causes the second connection wire Wherein the drones are separated from the droning structure by cutting the drones of the drones.
At least one auxiliary frame connected to the first connection line or the second connection line;
A separation device connected to the at least one auxiliary frame, respectively; And
Further comprising an auxiliary dron fastened by said separating device,
Wherein the fourth communication unit receives the auxiliary dron separation signal transmitted from the ground equipment and transmits the auxiliary dron separation signal to the control unit,
Wherein when the control unit receives the auxiliary dron separation signal, power is supplied from the power supply unit to the separation device to separate the auxiliary drones from the separation device as the separation between the separation device and the auxiliary drones is released, Wherein the separated auxiliary drones fly according to an auxiliary dron signal transmitted from the dronron controller through a communication unit of the auxiliary drones.
A dron landing plate connected to the first connecting line or the second connecting line, and at least one dron charging unit provided on the dron landing plate,
Wherein the drones are charged when the drones are landed on the at least one drone-filled portion.
An air bag for levitating the drones by gas injected therein;
A drones mounting structure, comprising: a support frame; and a fastening portion mounted on the support frame and provided with a fastening portion for holding the fastened state while lifting the dron in the air;
A first communication unit for transmitting a video signal generated by the first camera to a drone manipulator, a first communication unit for receiving a dronon flight signal transmitted from the drone manipulator corresponding to a video signal generated by the first camera, A second communication unit for receiving a dron separation signal transmitted from the drone manipulator; a fixing unit for fixing the fixing unit to the fixing unit; and a second communication unit for receiving the dron separation signal transmitted from the second communication unit, A drones for releasing the engagement of the drones, and a drones for supplying power to the drones;
A third communication unit for transmitting the image signal generated by the second camera to the ground equipment; an exhaust valve for exhausting the gas injected into the air bag; A fourth communication unit for receiving an altitude maintenance signal transmitted from the ground equipment corresponding to an image signal generated by the second camera; a control unit for receiving the altitude maintenance signal transmitted from the fourth communication unit and controlling the exhaust valve; An integrated controller including a power supply unit for supplying power to the control unit;
An exhaust port connecting the air cylinder and the exhaust valve; And
A first connecting line connecting an object located on the ground and the droning structure, and a second connecting line connecting the droning structure and the integrated controller,
When the drones control device receives the dron separation signal, power is supplied to the fixing part to release the fastening between the fastening part and the fixing part, so that the drones are separated from the dron mounting structure, Wherein the drones fly according to the dragon flight signal.
Wherein the fixed portion comprises a servo motor, a servo arm connected to the servo motor, and a wire connected between the servo motor and the drone battery portion,
The servo arm is fastened to the coupling portion to keep the drones floating and floating in the air,
When the drone control device receives the dronesignal signal, a current flows through the wire to drive the servomotor. As the servo arm is disengaged from the coupling portion by driving the servo motor, Wherein the drones are separated from the droning structure.
Wherein the fixed portion includes an electromagnet moving bar contact portion and an electromagnet moving portion including a coil and spaced apart from and parallel to the electromagnet moving bar contact portion and an electromagnet moving portion whose one end is in contact with the electromagnet moving rod contact portion, And a wire connected between the electromagnet moving part and the drone battery part,
The fastening portion is fastened in the form of being hooked on the electromagnet moving bar, so that the dron is kept floating while being floated in the air,
When the drone control device receives the dronesignal signal, a current flows through the wire, a magnetic force is generated in the coil incorporated in the moving part of the electromagnet, and the electromagnet moving bar is moved by the magnetic force generated in the coil, Wherein the drones are separated from the droning structure.
The fastening portion is the second connection line,
Wherein the fixing portion includes a rod portion through which the second connecting line is wound, a through structure having a through hole having an electric wire therein, the through-hole penetrating through the second connecting line, And a wire connected between the drone battery sections,
When the drone control device receives the dronesignal signal, a current flows through the wire, heat is generated in the electric wire provided in the through hole, and heat generated in the electric wire causes the electric current flowing through the through- Wherein the drones are separated from the drone mounting structure by cutting the two connecting lines.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR1020150165323A KR101808845B1 (en) | 2015-11-25 | 2015-11-25 | Envelope structure which drone is separated and can fly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR1020150165323A KR101808845B1 (en) | 2015-11-25 | 2015-11-25 | Envelope structure which drone is separated and can fly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| KR20170060763A KR20170060763A (en) | 2017-06-02 |
| KR101808845B1 true KR101808845B1 (en) | 2017-12-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| KR1020150165323A KR101808845B1 (en) | 2015-11-25 | 2015-11-25 | Envelope structure which drone is separated and can fly |
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| KR (1) | KR101808845B1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11008101B2 (en) | 2018-10-26 | 2021-05-18 | Ford Global Technologies, Llc | Systems, methods, and devices for package delivery using unmanned aerial vehicles |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107521690A (en) * | 2017-07-04 | 2017-12-29 | 北京大工科技有限公司 | The pending flight control method and device of a kind of fixed-wing unmanned plane |
| CN110979753B (en) * | 2019-11-01 | 2022-09-09 | 中国科学院空天信息创新研究院 | Aerostat carries on planet sampling reentry module and retrieves experimental electrical system |
| KR102405606B1 (en) * | 2021-11-30 | 2022-06-07 | 베셀에어로스페이스 주식회사 | Detachable tethering drone system |
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| KR200452737Y1 (en) | 2008-10-17 | 2011-03-24 | 김종열 | radio-controlled airship |
| KR101543542B1 (en) | 2014-11-06 | 2015-08-10 | 김경숙 | Intelligent surveillance system and method of monitoring using the same |
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| US11008101B2 (en) | 2018-10-26 | 2021-05-18 | Ford Global Technologies, Llc | Systems, methods, and devices for package delivery using unmanned aerial vehicles |
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