KR101843877B1 - Envelope structure with drone - Google Patents
Envelope structure with drone Download PDFInfo
- Publication number
- KR101843877B1 KR101843877B1 KR1020150154847A KR20150154847A KR101843877B1 KR 101843877 B1 KR101843877 B1 KR 101843877B1 KR 1020150154847 A KR1020150154847 A KR 1020150154847A KR 20150154847 A KR20150154847 A KR 20150154847A KR 101843877 B1 KR101843877 B1 KR 101843877B1
- Authority
- KR
- South Korea
- Prior art keywords
- fastening portion
- communication unit
- camera
- drone
- dron
- Prior art date
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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
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
-
- 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; ARRANGEMENTS 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; ARRANGEMENTS 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
-
- H02J17/00—
-
- B64C2201/127—
Abstract
The present invention allows the dron to be mounted on the drones mounting structure and perform the mission assigned to it by flying to the target point in accordance with the dron flight signal. 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 altitude maintenance apparatus, and when a problem is caught during surveillance, So that it can be quickly put into the spot.
Description
In the case where a problem is detected while the surroundings of the air bag structure are monitored through the camera provided in the altitude holding device, the dron mounted on the air bag structure according to the dron flight signal transmitted from the dron driver, Which is equipped with a drone.
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 surveillance system and method for confirming an event in real time through image sensing and tracking a moving object. 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 the dron And it is an object of the present invention to provide an air bag structure that can create an environment that 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.
It is another object of the present invention to provide an air bag structure capable of freely adjusting the altitude and monitoring the surroundings thereof.
In order to accomplish the above object, the present invention provides an air-bag structure equipped with a dron, the air bag being characterized by comprising: a bladder 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 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 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 altitude maintenance device including a power supply for supplying power to the control unit; An intake and exhaust port connecting the air cylinder and the exhaust valve; And a second connecting line connecting an object located on the ground and the dron mounting structure, and a second connecting line connecting the dron mounting structure and the altitude holding device.
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 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 gas supply tank connected to the intake and exhaust device, wherein the control unit controls the gas supply tank by receiving an altitude maintenance signal transmitted from the fourth communication unit to supply gas from the gas supply tank to the air bag .
And a pressure holding device connected to the intake and exhaust port, wherein the pressure holding device maintains the pressure of the air bladder according to a preset pressure value.
And the power supply unit is supplied with power through a power line connected from the ground.
The object located on the ground is a vehicle, and a power line is connected between the battery and the electric power supplying unit of the vehicle, and electric power is supplied from the battery to the electric power supplying unit through the electric power line .
The altitude maintenance apparatus may further include a wireless power receiving unit connected to the power supplying unit, and the power supplying unit is supplied with power transmitted wirelessly to the wireless power receiving unit.
And a winder positioned above the object located on the ground to wind or unwind the first connecting line.
Wherein the fastening portion is a fastening portion of the fastening portion connected between the support frame and the fastening portion, the fastening portion of the fastening portion is provided with a winding device, and when the dron receives a dron flight signal, And the fly is loosened while the fastening string is released.
The dron further includes a payload, and the second communication unit receives a payload separating signal transmitted from the drone manipulator, and the payload is separated from the dron according to the payload separating signal.
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 altitude maintenance apparatus. When it is necessary to input a dron during the surveillance activity By flying the dron mounted on the structure, the dron can be rapidly injected to the target point.
In addition, according to the present invention, since surveillance activities around the air bag structure are performed through a camera (i.e., a second camera) provided in the altitude maintenance device instead of the camera provided in the drone (i.e., the first camera) The power shortage problem that may occur when flying to the branch point can be 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.
According to the present invention, the control unit can easily suck and discharge the gas injected into the air bag through the control of the exhaust valve and the gas supply tank, and a winder for winding or uncoiling the first connection line is provided, You can freely adjust and monitor your activities.
1 is a schematic view of an air-bag structure equipped with a drone according to an embodiment of the present invention.
Fig. 2 is a view showing a modification of the embodiment of the present invention shown in Fig.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, an air-bag structure equipped with a 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, and are not intended to be exhaustive or to limit the invention to the precise forms disclosed. . ≪ / 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 equipped with a drone according to an embodiment of the present invention, and FIG. 2 is a view illustrating a modification of the embodiment of the present invention shown in FIG.
The present invention relates to a method for monitoring a dron for a dron according to a signal transmitted from a dronon controller (that is, a dron flight signal, which will be described later), when a problem is detected during monitoring of an air bag structure through a camera while the dron is lifted and fixed in the air , It is possible to transfer the work occurring at the target point to the drone manipulator in more detail or to separate the payload at the target point (the payload can be provided in the drone).
To this end, the air bag structure according to the present invention includes the
The
The
The
The
2, the
A
The
As shown in FIG. 1, the
For example, the
Alternatively, the
However, 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 fixing
The
To this end, the
The
The
Here, the ground equipment includes a video receiver capable of receiving the video 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 air bag structure according to the present invention may include a
The
Meanwhile, the air bag structure according to the present invention may further include a
The
Here, the
Alternatively, the
The
An
When one end of the
A
As described above, the
When the
In the air bag structure according to the present invention, by providing such a winding
On the other hand, the
Here, the payload separation signal is generated by the main body driving the drone manipulator, flying the
Hereinafter, an embodiment of utilizing a dust bag-equipped air bag structure according to the present invention will be described as an example.
The control subject of the ground equipment is generated by the
When the drone flight signal is transmitted to the
At this time, when the winder structure is provided with the
Meanwhile, when a distressed person is caught in the surveillance activity through the
The altitude maintenance signal can be transmitted to the
When the drone flight signal is transmitted to the
Also, 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:
400: altitude maintenance device
410: second camera 420: third communication section
430: exhaust valve 440: fourth communication section
450: control unit 460: power supply unit
500: Intake and exhaust system
610: first connection line 620: second connection line
700: gas supply tank
800: Pressure maintaining device
900: Power line
1000: Winder
1100: fastening fastener
1200: winding device
Claims (12)
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 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 altitude maintenance device including a power supply for supplying power to the control unit;
An intake and 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 elevation holding device,
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 gas supply tank connected to the intake and exhaust port,
Wherein the control unit receives the altitude maintenance signal transmitted from the fourth communication unit and controls the gas supply tank so that the gas is supplied from the gas supply tank to the air bladder.
And a pressure holding device connected to the intake and exhaust port,
Wherein the pressure holding device maintains the pressure of the air bag according to a predetermined 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 a battery provided in the vehicle and the power supply unit so that electric power is supplied from the battery included in the vehicle to the power supply unit through the power line.
Wherein the altitude maintenance device further comprises a wireless power receiver coupled 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.
Wherein the fastening portion is a fastening portion of the fastening portion connected between the support frame and the fastening portion, the fastening portion of the fastening portion is provided with a winding device,
Wherein when the dron receives the dron flight signal, the dron flys while loosening the fastening fastener string wound on the winding device.
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 in accordance with the payload separation signal.
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 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 altitude maintenance device including a power supply for supplying power to the control unit;
An intake and 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 elevation holding device,
Wherein the altitude maintenance device further comprises a wireless power receiver coupled to the power supply,
Wherein the power supply unit is supplied with electric power wirelessly transmitted to the wireless power receiving unit.
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 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 altitude maintenance device including a power supply for supplying power to the control unit;
An intake and 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 elevation holding device,
Wherein the fastening portion is a fastening portion of the fastening portion connected between the support frame and the fastening portion, the fastening portion of the fastening portion is provided with a winding device,
Wherein when the dron receives the dron flight signal, the dron flys while loosening the fastening fastener string wound on the winding device.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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KR1020150154847A KR101843877B1 (en) | 2015-11-05 | 2015-11-05 | Envelope structure with drone |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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KR1020150154847A KR101843877B1 (en) | 2015-11-05 | 2015-11-05 | Envelope structure with drone |
Publications (2)
Publication Number | Publication Date |
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KR20170052834A KR20170052834A (en) | 2017-05-15 |
KR101843877B1 true KR101843877B1 (en) | 2018-03-30 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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KR1020150154847A KR101843877B1 (en) | 2015-11-05 | 2015-11-05 | Envelope structure with drone |
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KR (1) | KR101843877B1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
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CN107707031B (en) * | 2017-08-30 | 2021-07-23 | 南京邮电大学 | Aerial wireless energy transfer system adopting unmanned aerial vehicle agent |
KR101973635B1 (en) * | 2017-10-27 | 2019-05-03 | 장영규 | Life saving drone |
KR102405606B1 (en) * | 2021-11-30 | 2022-06-07 | 베셀에어로스페이스 주식회사 | Detachable tethering drone system |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110315810A1 (en) * | 2010-06-23 | 2011-12-29 | Dimitri Petrov | Airborne, tethered, remotely stabilized surveillance platform |
US20130037650A1 (en) * | 2011-03-15 | 2013-02-14 | Stephen B. Heppe | Systems and Methods for Long Endurance Airship Operations |
US20150134152A1 (en) * | 2013-11-08 | 2015-05-14 | Dow Agrosciences Llc | Integrated remote aerial sensing system |
-
2015
- 2015-11-05 KR KR1020150154847A patent/KR101843877B1/en active IP Right Grant
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110315810A1 (en) * | 2010-06-23 | 2011-12-29 | Dimitri Petrov | Airborne, tethered, remotely stabilized surveillance platform |
US20130037650A1 (en) * | 2011-03-15 | 2013-02-14 | Stephen B. Heppe | Systems and Methods for Long Endurance Airship Operations |
US20150134152A1 (en) * | 2013-11-08 | 2015-05-14 | Dow Agrosciences Llc | Integrated remote aerial sensing system |
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KR20170052834A (en) | 2017-05-15 |
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