WO2017222249A1 - Gimbal assembly for drone - Google Patents
Gimbal assembly for drone Download PDFInfo
- Publication number
- WO2017222249A1 WO2017222249A1 PCT/KR2017/006360 KR2017006360W WO2017222249A1 WO 2017222249 A1 WO2017222249 A1 WO 2017222249A1 KR 2017006360 W KR2017006360 W KR 2017006360W WO 2017222249 A1 WO2017222249 A1 WO 2017222249A1
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- WIPO (PCT)
- Prior art keywords
- unit
- camera
- drone
- gimbal assembly
- lifting
- Prior art date
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- 230000003028 elevating effect Effects 0.000 claims description 7
- 238000000034 method Methods 0.000 claims description 6
- 238000010586 diagram Methods 0.000 description 5
- 230000002457 bidirectional effect Effects 0.000 description 4
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000009429 distress Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- 230000000630 rising effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
- F16M11/12—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction
- F16M11/121—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction constituted of several dependent joints
- F16M11/123—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction constituted of several dependent joints the axis of rotation intersecting in a single point, e.g. by using gimbals
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
- F16M11/12—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/20—Undercarriages with or without wheels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/20—Undercarriages with or without wheels
- F16M11/2007—Undercarriages with or without wheels comprising means allowing pivoting adjustment
- F16M11/2035—Undercarriages with or without wheels comprising means allowing pivoting adjustment in more than one direction
- F16M11/2042—Undercarriages with or without wheels comprising means allowing pivoting adjustment in more than one direction constituted of several dependent joints
- F16M11/205—Undercarriages with or without wheels comprising means allowing pivoting adjustment in more than one direction constituted of several dependent joints the axis of rotation intersecting in a single point, e.g. gimbals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M13/00—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles
- F16M13/02—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
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- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B17/00—Details of cameras or camera bodies; Accessories therefor
- G03B17/56—Accessories
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- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B17/00—Details of cameras or camera bodies; Accessories therefor
- G03B17/56—Accessories
- G03B17/561—Support related camera accessories
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/20—Transmission of mechanical power to rotors or propellers
- B64U50/23—Transmission of mechanical power to rotors or propellers with each propulsion means having an individual motor
Definitions
- the present invention relates to a gimbal assembly for drones, and more particularly, to a gimbal assembly for drones that allows the positioning of the camera mounted on the drone to be free, as well as accurate and fine positioning.
- Drones were originally unmanned aircraft developed for military use to enable reconnaissance or direct physical blows of war zones or hostile countries, but have recently been developed for a variety of purposes.
- drones are much lighter and easier to operate than airplanes, they can be used for broadcast photography as well as recently using drones for delivery of goods or mail.
- drones have recently been used for the purpose of water rescue, which can be manipulated to drop life-saving tubes to distress people.
- the prior art is to be able to tilt the camera in order to secure a wide shooting range of the camera mounted on the drone.
- the prior art has a large number of parts, complicated assembly and fastening, made of very expensive equipment, and was also inconvenient in management tasks such as immediately identifying and inspecting, repairing, or replacing failure points.
- the present invention has been invented to improve the above problems, to provide a gimbal assembly for a drone to be freely adjusted the position of the camera mounted on the drone.
- the present invention is to provide a gimbal assembly for a drone that allows the positioning of the camera according to the lifted position and tilt angle adjustment accurately and finely made.
- the present invention includes a first unit which is mounted to the flight body of the drone forward, reverse rotation, the operating space is formed in the middle; A second unit mounted to the first unit and disposed to move up and down in the working space; And a third unit mounted to the second unit and provided with a camera on one side, wherein the third unit rotates the camera with respect to one side of the second unit.
- the second unit includes the camera on an upper surface of the flying body. It is possible to provide a gimbal assembly for a drone, characterized in that it is raised upward, or lowered below the lower surface of the flight body.
- the first unit includes a ring-shaped mounting main body in which the operating space is formed in the middle, and a rotation driving unit provided in the flying main body and forward and reverse rotation of the mounting main body mounted on the flying main body. It is characterized by.
- the second unit is formed on an inner surface of the first unit forming the operating space, and the lifting unit for lifting up and down through the operating space of the first unit, and to support the reciprocation of the lifting unit And a lift support part and a camera support part reciprocally mounted to the lift part to support the camera, wherein the third unit is provided in the camera support part.
- the third unit may include a first tilting part mounted between the camera support part and the lifting part to allow the camera to rotate in a horizontal direction with respect to an up and down direction in which the second unit moves up and down, and the camera support part. And a second tilting part provided between the camera and allowing the camera to rotate in the front-rear direction with respect to the vertical direction in which the second unit moves up and down.
- the present invention is provided with a third unit capable of rotating the camera with respect to the second unit capable of lifting up and down on the first unit capable of forward and reverse rotation in the flight main body, whereby the position of the camera mounted on the drone can be freely adjusted.
- the positioning according to the lifted position and the tilt angle adjustment of the camera can be made precisely and finely.
- the present invention will not only secure a wide range of shooting, but also enable accurate positioning and focusing of the camera lens on a shooting target.
- FIG. 1 is a perspective view showing the overall appearance of a drone equipped with a gimbal assembly for a drone according to an embodiment of the present invention.
- FIG. 2 is a plan view of FIG. 1.
- FIG. 3 is a front view and a side view of a drone equipped with a gimbal assembly for a drone according to an embodiment of the present invention.
- FIG. 3 (a) is a front conceptual view illustrating a view from a direction IIIa of FIG. 2.
- 3 (b) is a view showing a side conceptual view showing what is viewed from the direction IIIb of FIG.
- FIG. 4 is a conceptual diagram illustrating various embodiments of a first unit that is a main part of a gimbal assembly for a drone according to an embodiment of the present invention.
- 5 to 7 is a perspective view of the coupling relationship of the gimbal assembly for drones according to an embodiment of the present invention from various viewpoints.
- FIG 8 and 9 is a conceptual diagram showing an operating state of the gimbal assembly for a drone according to an embodiment of the present invention.
- Figure 1 is a perspective view showing the overall appearance of a drone equipped with a gimbal assembly for a drone according to an embodiment of the present invention.
- FIG. 2 is a plan conceptual diagram of FIG. 1.
- FIG. 3 is a front view and a side view of a drone equipped with a gimbal assembly for a drone according to an embodiment of the present invention
- FIG. 3 (a) is a front conceptual view showing a view from a direction IIIa of FIG. 2.
- 3 (b) is a diagram illustrating a side conceptual view showing what is viewed from the direction IIIb of FIG. 2.
- FIG. 4 is a conceptual diagram illustrating various embodiments of a first unit that is a main part of a gimbal assembly for a drone according to an embodiment of the present invention.
- 5 to 7 are perspective views of the coupling relationship of the gimbal assembly for a drone according to an embodiment of the present invention, viewed from various viewpoints.
- FIG 8 and 9 are conceptual views illustrating an operating state of a gimbal assembly for a drone according to an embodiment of the present invention.
- the first unit 100 is mounted on the flight main body 500
- the second unit 200 is mounted on the first unit 100
- the third unit is mounted on the second unit 200. It can be seen that the unit 300 is mounted structure.
- the first unit 100 is mounted on the flight main body 500 so as to be rotated forward and backward, and an operating space 101 is formed in the middle thereof.
- the lifting unit reciprocates the third unit 200 and the third unit ( To provide a storage space of the 300 and the camera 400.
- the second unit 200 is mounted to the first unit 100 in a liftable reciprocating manner, and lifts the camera 400 above the top surface of the flight body 500 or below the bottom surface of the flight body 500.
- the third unit 300 is mounted to the second unit 200 and rotates the camera 400 with respect to one side of the second unit 200.
- the third unit 300 capable of rotating the camera 400 with respect to the second unit 200 capable of lifting up and down on the first unit 100 capable of forward and reverse rotation to the flight body 500 is provided.
- the position adjustment of the camera 400 mounted on the drone is freely made, as well as the positioning according to the position and the tilt angle adjustment of the camera 400 can be precisely and finely made.
- the present invention will not only ensure a wide range of shooting, but also enable accurate positioning and focusing of the camera lens with respect to a photographing object.
- the flight main body 500 constituting the drone includes a first plate 510 having a first through hole 511 formed thereon so as to mount the first unit 100 to form an upper surface thereof, and the first unit 100.
- the second through hole 521 is formed to be mounted to form a lower surface, and includes a second plate 520 facing the first plate 510.
- the flying body 500 may include a plurality of spacers disposed between the first plate 510 and the second plate 520 so as to space the first plate 510 and the second plate 520 at regular intervals ( 530 and a support rod 540 mounted to the spacer 530 and mounted with a rotatable flying blade 600 at an end thereof.
- first unit 100, the second unit 300, and the third unit 300 to be described later may move manually or automatically.
- the first unit 100 is provided with a ring-shaped mounting body 110 in which the operating space 101 is formed in the middle, and the flying body 500, and the mounting body mounted on the flying body 500 ( It may include a rotation drive unit 120 for forward and reverse rotation 110.
- the rotation drive unit 120 as shown in Figure 4 (a), the drive motor 121 is built in the flight main body 500, the drive gear 122 is mounted to the drive shaft end of the drive motor 121, and mounting Embodiments of a structure including a driven gear 123 formed along the outer circumferential surface of the main body 110 and a drive transmission belt 124 connecting the drive gear 122 and the driven gear 123 to each other may be applicable.
- the rotation driving unit 120 may apply an embodiment of a structure in which the driving gear 122 and the driven gear 123 formed along the outer circumferential surface of the mounting body 110 are directly engaged. Of course you can.
- the second unit 200 will be described in more detail with reference to FIGS. 5 to 7, and it can be understood that the second unit 200 includes a lift unit 210, a lift support unit 220, and a camera support unit 230.
- the lifting unit 210 moves up and down through the operating space 101 of the first unit 100, that is, the mounting body 110.
- the lifting support 220 is formed on the inner side of the mounting body 110 forming the operating space 101 to support the reciprocation of the lifting unit 210.
- the camera support 230 is mounted to the lifting unit 210 so as to reciprocately support the camera 400.
- the third unit 300 to be described later is provided in the camera support 230.
- the first tilting part 310 is mounted between the camera support part 230 of the second unit 200 and the lifting part 210 of the second unit 200, so that the second unit (as shown in FIG. It is to allow the camera 400 to rotate in the left and right directions with respect to the vertical direction in which the 200 moves up and down.
- the second tilting part 320 is provided between the camera support part 230 and the camera 400 so that the camera 400 can move forward and backward with respect to the vertical direction in which the second unit 200 moves up and down as shown in FIG. 3B. It is to allow the meeting.
- the lifting unit 210 of the second unit 200 may have an upper frame 211 and a lower frame 212 disposed below the upper frame 211. And, the upper end is coupled to the upper frame 211, the lower end is coupled to the lower frame 212, it can be seen that it includes a plurality of lifting rods 213 that the lifting operation is supported by the lifting support 220. .
- the lifting unit 210 the upper end is coupled to the upper frame 211, the lower end is coupled to the lower frame 212, the first screw rod 214 and the thread (not shown) formed along the outer circumferential surface and It may include a first linear motor 215 connected to the first screw rod 214 so as to be mounted forward and reversely and disposed on the lower frame 212.
- the camera support 230 to be described later can be lifted and reciprocated along the plurality of lifting rods 213.
- the lifting support 220 of the second unit 200 at least one is formed on each of both sides of the inner surface of the ring-shaped mounting body 110, the operating space 101 is formed in the middle of the first unit 100, respectively
- the lifting rods 213 of the lifting unit 210 include a plurality of linear guides 221 supporting lifting up and down.
- the camera support part 230 of the second unit 200 is arranged on the front and rear surfaces of the elevating piece 231 and the elevating piece 231, which elevate and reciprocate along the plurality of elevating rods 213.
- Both sides of the 400 may include a support bracket 232 rotatably coupled.
- the camera support 230 has an upper end coupled to the upper frame 211, a lower end coupled to the lower frame 212, and a second screw rod 234 having a thread formed along an outer circumferential surface thereof, and a second screw rod. It may include a second linear motor 235 connected to the 234 so as to be mounted in a forward and reverse rotation and disposed on the elevating piece 231.
- the third unit 300 is formed on the lifting piece 231 and the support bracket 232.
- the first tilting portion 310 of the third unit 300, the lifting piece 231 and the front surface of the lifting piece 231 of the camera support portion 230 capable of lifting up and down along the lifting bar 213. It may include a first rotating motor 311 disposed between the center of the support bracket 232 is disposed.
- the first rotational motor 311 rotates the support bracket 232 forward and backward on the lifting piece 231 as shown in FIG. 3 (a) using the center of the support bracket 232 as the rotation shaft.
- the second tilting part 320 of the third unit 300 is provided on both ends of the support bracket 232 of the camera support 230, the support piece 233a for rotatably supporting both sides of the camera 400 It may include a second rotation motor 321 disposed between the support piece 233b of one side of the 233b and one side of the camera 400.
- the second rotation motor 321 rotates the camera 400 forward and reverse with respect to the support piece 233b with the end of the support piece 233b as the rotation shaft.
- the second tilting part 320 may further include an adjustment slot 233s to penetrate each of the support pieces 233a and 233b to a predetermined length so as to adjust a position where both sides of the camera 400 are coupled.
- an adjustment slot 233s to penetrate each of the support pieces 233a and 233b to a predetermined length so as to adjust a position where both sides of the camera 400 are coupled.
- the linear guide of the driving force of the first and second linear motors 215 and 235 is transmitted to the lifting bar 213 and the lifting piece 231 through the first and second screw rods 214 and 234.
- the operator can perform the operation of the first, second, third unit (100, 200, 300) with the existing remote controller, as well as a receiver provided on one side of the flight main body 500 (hereinafter referred to as H) and the first, second, and third units 100, 200, and 300 electrically connected to each other, and are used as a substitute for a remote controller that communicates with a portable terminal of an operator such as a smartphone, a portable PC or a tablet PC, and the aforementioned receiver. It is also possible to utilize.
- FIGS. 8 and 9 An operation process of the gimbal assembly for a drone according to the present invention as described above will be described with reference to FIGS. 8 and 9, and reference numerals not shown in FIGS. 8 and 9 refer to FIGS. 1 to 7.
- the user drives the flight blade 600 of the flight body 500 by using a portable terminal or a remote controller (hereinafter, 'operator') to fly the flight body 500.
- a portable terminal or a remote controller hereinafter, 'operator'
- the lifting rods 213 are linear guides ( 221 is lowered, and the lower frame 212 is disposed on the lower side of the second plate 520 as shown in FIG.
- the operator operates the first rotation motor 311 to secure the proper left and right inclination angles for the left and right pivoting operation (see the bidirectional circular arrow on the lower side of FIG. 3 (a)) with respect to the up and down direction of the camera 400. do.
- the operator operates the second rotation motor 321 for the forward and backward rotational motion (refer to the bidirectional circular arrow on the lower left side of FIG. 3 (b)) with respect to the vertical direction of the camera 400. You can shoot while securing.
- the second unit 200 and the third unit 300 with the manipulator in order to take a picture and video of the object in the view of the operator looking up at a high place while flying the flight main body 500 from the lower side of the bridge plate or structure.
- the upper frame 211 is disposed on the upper side of the first plate 510 as shown in FIG.
- the operator operates the first rotation motor 311 to secure the proper left and right inclination angles for the left and right pivoting operation (see the bidirectional circular arrow on the lower side of FIG. 3 (a)) with respect to the up and down direction of the camera 400. do.
- the operator operates the second rotation motor 321 for the forward and backward rotational motion (refer to the bidirectional circular arrow on the lower left side of FIG. 3 (b)) with respect to the vertical direction of the camera 400. You can shoot while securing.
- the present invention has as its basic technical idea to provide a drone gimbal assembly for allowing the positioning of the camera mounted on the drone to be freely performed, as well as to accurately and precisely position the camera.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
Abstract
The present invention relates to a gimbal assembly for a drone, comprising: a first unit mounted on a flight body of a drone to be able to rotate forward/backward, an operation space being formed in the middle of the first unit; a second unit mounted on the first unit and arranged in the operation space to be able to make upward/downward reciprocating movements; and a third unit that is mounted on the second unit and has a camera mounted on one side thereof such that the camera is rotated with regard to one side of the second unit, wherein the second unit lifts the camera above the upper surface of the flight body or lowers the camera below the lower surface of the flight body such that not only the position of the camera mounted on the drone can be adjusted freely, but the position can be determined accurately and precisely.
Description
본 발명은 드론용 짐벌 어셈블리에 관한 것으로, 더욱 상세하게는 드론에 장착되는 카메라의 위치 조정이 자유로이 이루어짐은 물론, 위치 결정이 정확하고 미세하게 이루어질 수 있도록 한 드론용 짐벌 어셈블리에 관한 것이다.The present invention relates to a gimbal assembly for drones, and more particularly, to a gimbal assembly for drones that allows the positioning of the camera mounted on the drone to be free, as well as accurate and fine positioning.
드론(drone)은 원래 전쟁 지역이나 적성국의 정찰 또는 직접적인 물리적 타격이 가능하도록 하는 군사용도로 개발된 무인 비행체이지만, 최근에는 이러한 군사용 목적에 한정되지 않고 다양한 용도로 개발되고 있다.Drones were originally unmanned aircraft developed for military use to enable reconnaissance or direct physical blows of war zones or hostile nations, but have recently been developed for a variety of purposes.
이를테면, 드론은 비행기에 비하여 훨씬 가볍고 조작이 간편하기 때문에 방송 촬영용으로도 활용될 수 있음은 물론, 최근에는 물품이나 우편의 배달용으로 드론을 활용하는 사례도 보고되고 있다.For example, since drones are much lighter and easier to operate than airplanes, they can be used for broadcast photography as well as recently using drones for delivery of goods or mail.
또한, 드론은 최근 구명용 튜브를 조난자에게 투하할 수 있도록 조작 가능한 수상 인명 구조의 용도로도 활용되고 있다.In addition, drones have recently been used for the purpose of water rescue, which can be manipulated to drop life-saving tubes to distress people.
이와 같이 사용자의 활용도에 맞게 다양한 도구들을 드론에 장착함으로써, 드론의 활용 범위를 넓히고자 하는 시도 또한 계속 진행되고 있으며, 상기와 같은 관점에서 등록특허 제10-1302442호의 "무인항공기 카메라 폴딩장치"(이하 '선행기술')와 같은 것을 들 수 있다.As described above, attempts to broaden the range of use of the drone are also ongoing by mounting various tools to the user's utilization, and in view of the above, the "unmanned aerial vehicle camera folding device" of Patent No. 10-1302442 ( The following may be mentioned as 'prior art').
선행기술은 무인항공기에 탑재된 카메라의 넓은 촬영 범위를 확보하기 위하여 카메라를 틸팅시킬 수 있도록 한 것이다.The prior art is to be able to tilt the camera in order to secure a wide shooting range of the camera mounted on the drone.
그러나 선행기술은 크기가 매우 큰 무인항공기에 적용되는 것으로, 카메라의 상하 회동 범위가 제한적이어서 교량의 하부나 협소한 지역의 구조물 진단 검사를 위한 소규모의 드론에 탑재하여 촬영하기에는 무리가 있었다.However, the prior art is applied to a very large unmanned aerial vehicle, because the range of the vertical tilt of the camera is limited, it was difficult to mount on a small drone for the diagnostic inspection of the structure of the lower or narrow area of the bridge.
특히, 선행기술은 부품 갯수가 많고 조립 및 체결이 복잡하며 매우 고가의 장비로 이루어지고, 고장 발생 개소를 즉각적으로 파악하여 점검하고 수리하거나 교체하는 등의 관리 작업에도 불편함이 있었던 것이다.In particular, the prior art has a large number of parts, complicated assembly and fastening, made of very expensive equipment, and was also inconvenient in management tasks such as immediately identifying and inspecting, repairing, or replacing failure points.
본 발명은 상기와 같은 문제점을 개선하기 위하여 발명된 것으로, 드론에 장착되는 카메라의 위치 조정이 자유로이 이루어지도록 하는 드론용 짐벌 어셈블리를 제공하기 위한 것이다. 또한, 본 발명은 카메라가 승강된 위치 및 경사각 조절에 따른 위치 결정이 정확하고 미세하게 이루어질 수 있도록 하는 드론용 짐벌 어셈블리를 제공하기 위한 것이다.The present invention has been invented to improve the above problems, to provide a gimbal assembly for a drone to be freely adjusted the position of the camera mounted on the drone. In addition, the present invention is to provide a gimbal assembly for a drone that allows the positioning of the camera according to the lifted position and tilt angle adjustment accurately and finely made.
상기와 같은 목적을 달성하기 위하여, 본 발명은 드론의 비행 본체에 정, 역회전 가능하게 장착되며, 중간에 작동 공간이 형성되는 제1 유닛; 상기 제1 유닛에 장착되어 상기 작동 공간에 승강 왕복 가능하게 배치되는 제2 유닛; 및 상기 제2 유닛에 장착되어 일측에 카메라가 구비되며, 상기 카메라를 상기 제2 유닛의 일측에 대하여 회동시키는 제3 유닛을 포함하고, 상기 제2 유닛은, 상기 카메라를, 상기 비행 본체의 상면보다 위로 상승시키거나, 상기 비행 본체의 하면보다 아래로 하강시키는 것을 특징으로 하는 드론용 짐벌 어셈블리를 제공할 수 있다.In order to achieve the above object, the present invention includes a first unit which is mounted to the flight body of the drone forward, reverse rotation, the operating space is formed in the middle; A second unit mounted to the first unit and disposed to move up and down in the working space; And a third unit mounted to the second unit and provided with a camera on one side, wherein the third unit rotates the camera with respect to one side of the second unit. The second unit includes the camera on an upper surface of the flying body. It is possible to provide a gimbal assembly for a drone, characterized in that it is raised upward, or lowered below the lower surface of the flight body.
여기서, 상기 제1 유닛은, 상기 작동 공간이 중간에 형성되는 링 형상의 장착 본체와, 상기 비행 본체에 구비되며, 상기 비행 본체에 장착된 상기 장착 본체를 정, 역회전시키는 회전 구동부를 포함하는 것을 특징으로 한다.Here, the first unit includes a ring-shaped mounting main body in which the operating space is formed in the middle, and a rotation driving unit provided in the flying main body and forward and reverse rotation of the mounting main body mounted on the flying main body. It is characterized by.
이때, 상기 제2 유닛은, 상기 제1 유닛의 작동 공간을 관통하여 상하로 승강 왕복하는 승강부와, 상기 작동 공간을 형성하는 상기 제1 유닛의 내측면에 형성되어 상기 승강부의 왕복을 지지하는 승강 지지부와, 상기 승강부에 왕복 가능하게 장착되어 상기 카메라를 지지하는 카메라 지지부를 포함하며, 상기 제3 유닛은 상기 카메라 지지부에 구비되는 것을 특징으로 한다.In this case, the second unit is formed on an inner surface of the first unit forming the operating space, and the lifting unit for lifting up and down through the operating space of the first unit, and to support the reciprocation of the lifting unit And a lift support part and a camera support part reciprocally mounted to the lift part to support the camera, wherein the third unit is provided in the camera support part.
또한, 상기 제3 유닛은, 상기 카메라 지지부와 상기 승강부 사이에 장착되어 상기 제2 유닛이 승강 왕복하는 상하 방향에 대하여 좌우 방향으로 상기 카메라의 회동을 허용하는 제1 틸팅부와, 상기 카메라 지지부와 상기 카메라 사이에 구비되어 상기 제2 유닛이 승강 왕복하는 상하 방향에 대하여 전후 방향으로 상기 카메라의 회동을 허용하는 제2 틸팅부를 포함하는 것을 특징으로 한다.The third unit may include a first tilting part mounted between the camera support part and the lifting part to allow the camera to rotate in a horizontal direction with respect to an up and down direction in which the second unit moves up and down, and the camera support part. And a second tilting part provided between the camera and allowing the camera to rotate in the front-rear direction with respect to the vertical direction in which the second unit moves up and down.
상기와 같은 구성의 본 발명에 따르면, 다음과 같은 효과를 도모할 수 있다.According to the present invention having the above configuration, the following effects can be achieved.
우선, 본 발명은 비행 본체에 정, 역회전 가능한 제1 유닛에 상하로 승강 가능한 제2 유닛에 대하여 카메라의 회동 동작이 가능한 제3 유닛을 구비함으로써, 드론에 장착되는 카메라의 위치 조정이 자유로이 이루어짐은 물론, 카메라가 승강된 위치 및 경사각 조절에 따른 위치 결정이 정확하고 미세하게 이루어질 수 있게 된다.First, the present invention is provided with a third unit capable of rotating the camera with respect to the second unit capable of lifting up and down on the first unit capable of forward and reverse rotation in the flight main body, whereby the position of the camera mounted on the drone can be freely adjusted. Of course, the positioning according to the lifted position and the tilt angle adjustment of the camera can be made precisely and finely.
따라서, 본 발명은 폭넓은 촬영 범위의 확보가 가능함은 물론, 촬영 대상물에 대한 카메라 렌즈의 정확한 위치 선정 및 포커싱이 가능하게 될 것이다.Therefore, the present invention will not only secure a wide range of shooting, but also enable accurate positioning and focusing of the camera lens on a shooting target.
도 1은 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리가 장착된 드론의 전체적인 외관을 나타낸 사시도이다.1 is a perspective view showing the overall appearance of a drone equipped with a gimbal assembly for a drone according to an embodiment of the present invention.
도 2는 도 1의 평면 개념도이다.FIG. 2 is a plan view of FIG. 1.
도 3은 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리가 장착된 드론의 정면 및 측면에서 바라본 것을 나타낸 것으로, 도 3(a)는 도 2의 IIIa 방향에서 바라본 것을 도시한 정면 개념도를, 도 3(b)는 도 2의 IIIb 방향에서 바라본 것을 도시한 측면 개념도를 각각 나타낸 도면이다.FIG. 3 is a front view and a side view of a drone equipped with a gimbal assembly for a drone according to an embodiment of the present invention. FIG. 3 (a) is a front conceptual view illustrating a view from a direction IIIa of FIG. 2. 3 (b) is a view showing a side conceptual view showing what is viewed from the direction IIIb of FIG.
도 4는 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리의 주요부인 제1 유닛의 다양한 실시예를 도시한 개념도이다.4 is a conceptual diagram illustrating various embodiments of a first unit that is a main part of a gimbal assembly for a drone according to an embodiment of the present invention.
도 5 내지 도 7은 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리의 결합 관계를 다양한 시점에서 바라본 사시도이다.5 to 7 is a perspective view of the coupling relationship of the gimbal assembly for drones according to an embodiment of the present invention from various viewpoints.
도 8 및 도 9는 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리의 작동 상태를 나타낸 개념도이다.8 and 9 is a conceptual diagram showing an operating state of the gimbal assembly for a drone according to an embodiment of the present invention.
본 발명의 이점 및 특징, 그리고 그것들을 달성하는 방법은 첨부되는 도면과 함께 상세하게 후술되는 실시예를 참조하면 명확해질 것이다.Advantages and features of the present invention, and methods for achieving them will be apparent with reference to the embodiments described below in detail in conjunction with the accompanying drawings.
그러나, 본 발명은 이하에서 개시되는 실시예로 한정되는 것이 아니라 서로 다른 다양한 형태로 구현될 것이다.However, the present invention is not limited to the embodiments disclosed below, but may be implemented in various different forms.
본 명세서에서 본 실시예는 본 발명의 개시가 완전하도록 하며, 본 발명이 속하는 기술 분야에서 통상의 지식을 가진 자에게 발명의 범주를 완전하게 알려주기 위해 제공되는 것이다.In this specification, the embodiments are provided so that the disclosure of the present invention may be completed and the scope of the present invention may be completely provided to those skilled in the art.
그리고 본 발명은 청구항의 범주에 의해 정의될 뿐이다.And the present invention is only defined by the scope of the claims.
따라서, 몇몇 실시예에서, 잘 알려진 구성 요소, 잘 알려진 동작 및 잘 알려진 기술들은 본 발명이 모호하게 해석되는 것을 피하기 위하여 구체적으로 설명되지 않는다.Thus, in some embodiments, well known components, well known operations and well known techniques are not described in detail in order to avoid obscuring the present invention.
또한, 명세서 전체에 걸쳐 동일 참조 부호는 동일 구성 요소를 지칭하고, 본 명세서에서 사용된(언급된) 용어들은 실시예를 설명하기 위한 것이며 본 발명을 제한하고자 하는 것은 아니다.In addition, the same reference numerals throughout the specification refer to the same components, and the terminology (discussed) used herein is for the purpose of describing the embodiments are not intended to limit the invention.
본 명세서에서, 단수형은 문구에서 특별히 언급하지 않는 한 복수형도 포함하며, '포함(또는, 구비)한다'로 언급된 구성 요소 및 동작은 하나 이상의 다른 구성요소 및 동작의 존재 또는 추가를 배제하지 않는다.As used herein, the singular forms "a", "an" and "the" include plural unless the context clearly dictates otherwise, and the elements and acts referred to as 'comprises' or 'do' not exclude the presence or addition of one or more other components and acts. .
다른 정의가 없다면, 본 명세서에서 사용되는 모든 용어(기술 및 과학적 용어를 포함)는 본 발명이 속하는 기술 분야에서 통상의 지식을 가진 자에게 공통적으로 이해될 수 있는 의미로 사용될 수 있을 것이다.Unless otherwise defined, all terms (including technical and scientific terms) used in the present specification may be used in a sense that can be commonly understood by those skilled in the art.
또 일반적으로 사용되는 사전에 정의되어 있는 용어들은 정의되어 있지 않은 한 이상적으로 또는 과도하게 해석되지 않는다.In addition, the terms defined in the commonly used dictionary are not ideally or excessively interpreted unless they are defined.
이하, 첨부된 도면을 참고로 본 발명의 바람직한 실시예에 대하여 설명한다.Hereinafter, with reference to the accompanying drawings will be described a preferred embodiment of the present invention.
우선, 도 1은 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리가 장착된 드론의 전체적인 외관을 나타낸 사시도이다.First, Figure 1 is a perspective view showing the overall appearance of a drone equipped with a gimbal assembly for a drone according to an embodiment of the present invention.
그리고, 도 2는 도 1의 평면 개념도이다.2 is a plan conceptual diagram of FIG. 1.
그리고, 도 3은 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리가 장착된 드론의 정면 및 측면에서 바라본 것을 나타낸 것으로, 도 3(a)는 도 2의 IIIa 방향에서 바라본 것을 도시한 정면 개념도를, 도 3(b)는 도 2의 IIIb 방향에서 바라본 것을 도시한 측면 개념도를 각각 나타낸 도면이다.3 is a front view and a side view of a drone equipped with a gimbal assembly for a drone according to an embodiment of the present invention, and FIG. 3 (a) is a front conceptual view showing a view from a direction IIIa of FIG. 2. 3 (b) is a diagram illustrating a side conceptual view showing what is viewed from the direction IIIb of FIG. 2.
그리고, 도 4는 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리의 주요부인 제1 유닛의 다양한 실시예를 도시한 개념도이다.4 is a conceptual diagram illustrating various embodiments of a first unit that is a main part of a gimbal assembly for a drone according to an embodiment of the present invention.
그리고, 도 5 내지 도 7은 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리의 결합 관계를 다양한 시점에서 바라본 사시도이다.5 to 7 are perspective views of the coupling relationship of the gimbal assembly for a drone according to an embodiment of the present invention, viewed from various viewpoints.
또한, 도 8 및 도 9는 본 발명의 일 실시예에 따른 드론용 짐벌 어셈블리의 작동 상태를 나타낸 개념도이다.8 and 9 are conceptual views illustrating an operating state of a gimbal assembly for a drone according to an embodiment of the present invention.
본 발명은 도시된 바와 같이, 비행 본체(500)에 제1 유닛(100)이 장착되고, 제1 유닛(100)에 제2 유닛(200)이 장착되며, 제2 유닛(200)에 제3 유닛(300)이 장착된 구조임을 파악할 수 있다.As shown, the first unit 100 is mounted on the flight main body 500, the second unit 200 is mounted on the first unit 100, and the third unit is mounted on the second unit 200. It can be seen that the unit 300 is mounted structure.
제1 유닛(100)은 비행 본체(500)에 정, 역회전 가능하게 장착되며, 중간에 작동 공간(101)이 형성되는 것으로, 후술할 제2 유닛(200)의 승강 왕복 및 제3 유닛(300)과 카메라(400)의 수납 공간을 제공하기 위한 것이다.The first unit 100 is mounted on the flight main body 500 so as to be rotated forward and backward, and an operating space 101 is formed in the middle thereof. The lifting unit reciprocates the third unit 200 and the third unit ( To provide a storage space of the 300 and the camera 400.
제2 유닛(200)은 제1 유닛(100)에 승강 왕복 가능하게 장착되며, 비행 본체(500)의 상면보다 위로 또는 비행 본체(500)의 하면보다 아래로 카메라(400)를 승강시키는 것이다.The second unit 200 is mounted to the first unit 100 in a liftable reciprocating manner, and lifts the camera 400 above the top surface of the flight body 500 or below the bottom surface of the flight body 500.
제3 유닛(300)은 제2 유닛(200)에 장착되며, 카메라(400)를 제2 유닛(200)의 일측에 대하여 회동시키는 것이다.The third unit 300 is mounted to the second unit 200 and rotates the camera 400 with respect to one side of the second unit 200.
따라서, 본 발명은 비행 본체(500)에 정, 역회전 가능한 제1 유닛(100)에 상하로 승강 가능한 제2 유닛(200)에 대하여 카메라(400)의 회동 동작이 가능한 제3 유닛(300)을 구비함으로써, 드론에 장착되는 카메라(400)의 위치 조정이 자유로이 이루어짐은 물론, 카메라(400)가 승강된 위치 및 경사각 조절에 따른 위치 결정이 정확하고 미세하게 이루어질 수 있게 된다.Therefore, according to the present invention, the third unit 300 capable of rotating the camera 400 with respect to the second unit 200 capable of lifting up and down on the first unit 100 capable of forward and reverse rotation to the flight body 500 is provided. By providing, the position adjustment of the camera 400 mounted on the drone is freely made, as well as the positioning according to the position and the tilt angle adjustment of the camera 400 can be precisely and finely made.
즉, 본 발명은 폭넓은 촬영 범위의 확보가 가능함은 물론, 촬영 대상물에 대한 카메라 렌즈의 정확한 위치 선정 및 포커싱이 가능하게 될 것이다.That is, the present invention will not only ensure a wide range of shooting, but also enable accurate positioning and focusing of the camera lens with respect to a photographing object.
본 발명은 상기와 같은 실시예의 적용이 가능하며, 다음과 같은 다양한 실시예의 적용 또한 가능함은 물론이다.The present invention can be applied to the above embodiments, and of course, the following various embodiments are also applicable.
우선, 드론을 구성하는 비행 본체(500)는, 제1 유닛(100)이 장착되도록 제1 통공(511)이 형성되어 상면을 형성하는 제1 플레이트(510)와, 제1 유닛(100)이 장착되도록 제2 통공(521)이 형성되어 하면을 형성하며 제1 플레이트(510)와 상호 대면하는 제2 플레이트(520)를 포함한다.First, the flight main body 500 constituting the drone includes a first plate 510 having a first through hole 511 formed thereon so as to mount the first unit 100 to form an upper surface thereof, and the first unit 100. The second through hole 521 is formed to be mounted to form a lower surface, and includes a second plate 520 facing the first plate 510.
그리고, 비행 본체(500)는, 제1 플레이트(510)와 제2 플레이트(520)를 일정 간격으로 이격시키도록 제1 플레이트(510)와 제2 플레이트(520) 사이에 배치되는 복수의 스페이서(530)와, 스페이서(530)에 장착되며, 단부에 회전 가능한 비행용 블레이드(600)가 장착되는 지지 로드(540)를 포함한다.The flying body 500 may include a plurality of spacers disposed between the first plate 510 and the second plate 520 so as to space the first plate 510 and the second plate 520 at regular intervals ( 530 and a support rod 540 mounted to the spacer 530 and mounted with a rotatable flying blade 600 at an end thereof.
또한, 후술할 제1 유닛(100)과 제2 유닛(300) 및 제3 유닛(300)은 수동 또는 자동으로 움직일 수 있을 것이다.In addition, the first unit 100, the second unit 300, and the third unit 300 to be described later may move manually or automatically.
한편, 제1 유닛(100)은, 작동 공간(101)이 중간에 형성되는 링 형상의 장착 본체(110)와, 비행 본체(500)에 구비되며, 비행 본체(500)에 장착된 장착 본체(110)를 정, 역회전시키는 회전 구동부(120)를 포함할 수 있다.On the other hand, the first unit 100 is provided with a ring-shaped mounting body 110 in which the operating space 101 is formed in the middle, and the flying body 500, and the mounting body mounted on the flying body 500 ( It may include a rotation drive unit 120 for forward and reverse rotation 110.
여기서, 회전 구동부(120)는 도 4(a)와 같이, 비행 본체(500)에 내장되는 구동모터(121)와, 구동모터(121)의 구동축 단부에 장착되는 구동기어(122)와, 장착 본체(110)의 외주면을 따라 형성된 피동기어(123)와, 구동기어(122)와 피동기어(123)를 상호 연결하는 구동전달 벨트(124)를 포함하는 구조의 실시예를 적용할 수 있다.Here, the rotation drive unit 120, as shown in Figure 4 (a), the drive motor 121 is built in the flight main body 500, the drive gear 122 is mounted to the drive shaft end of the drive motor 121, and mounting Embodiments of a structure including a driven gear 123 formed along the outer circumferential surface of the main body 110 and a drive transmission belt 124 connecting the drive gear 122 and the driven gear 123 to each other may be applicable.
이때, 회전 구동부(120)는 도 4(b)와 같이, 구동기어(122)와, 장착 본체(110)의 외주면을 따라 형성된 피동기어(123)가 직접 맞물리도록 하는 구조의 실시예를 적용할 수도 있음은 물론이다.In this case, as shown in FIG. 4 (b), the rotation driving unit 120 may apply an embodiment of a structure in which the driving gear 122 and the driven gear 123 formed along the outer circumferential surface of the mounting body 110 are directly engaged. Of course you can.
한편, 제2 유닛(200)은, 도 5 내지 도 7을 참조하여 더욱 구체적으로 살펴보면, 승강부(210)와 승강 지지부(220) 및 카메라 지지부(230)를 포함하는 구조임을 파악할 수 있다.Meanwhile, the second unit 200 will be described in more detail with reference to FIGS. 5 to 7, and it can be understood that the second unit 200 includes a lift unit 210, a lift support unit 220, and a camera support unit 230.
승강부(210)는 제1 유닛(100), 즉 장착 본체(110)의 작동 공간(101)을 관통하여 상하로 승강 왕복하는 것이다.The lifting unit 210 moves up and down through the operating space 101 of the first unit 100, that is, the mounting body 110.
승강 지지부(220)는 작동 공간(101)을 형성하는 장착 본체(110)의 내측면에 형성되어 승강부(210)의 왕복을 지지하는 것이다.The lifting support 220 is formed on the inner side of the mounting body 110 forming the operating space 101 to support the reciprocation of the lifting unit 210.
카메라 지지부(230)는 승강부(210)에 왕복 가능하게 장착되어 카메라(400)를 지지하는 것이다.The camera support 230 is mounted to the lifting unit 210 so as to reciprocately support the camera 400.
여기서, 후술할 제3 유닛(300)은 카메라 지지부(230)에 구비되는 것을 알 수 있다.Here, it can be seen that the third unit 300 to be described later is provided in the camera support 230.
한편, 제3 유닛(300)은, 도 3(a)와 같은 회동 동작을 허용하는 제1 틸팅부(310)와, 도 3(b)와 같은 회동 동작을 허용하는 제2 틸팅부(320)를 포함하는 것을 알 수 있다.On the other hand, the third unit 300, the first tilting unit 310 to allow the rotational operation as shown in Figure 3 (a), and the second tilting unit 320 to allow the rotational operation as shown in Figure 3 (b). It can be seen that it includes.
즉, 제1 틸팅부(310)는 제2 유닛(200)의 카메라 지지부(230)와 제2 유닛(200)의 승강부(210) 사이에 장착되어 도 3(a)와 같이 제2 유닛(200)이 승강 왕복하는 상하 방향에 대하여 좌우 방향으로 카메라(400)의 회동을 허용하는 것이다.That is, the first tilting part 310 is mounted between the camera support part 230 of the second unit 200 and the lifting part 210 of the second unit 200, so that the second unit (as shown in FIG. It is to allow the camera 400 to rotate in the left and right directions with respect to the vertical direction in which the 200 moves up and down.
제2 틸팅부(320)는 카메라 지지부(230)와 카메라(400) 사이에 구비되어 도 3(b)와 같이 제2 유닛(200)이 승강 왕복하는 상하 방향에 대하여 전후 방향으로 카메라(400)의 회동을 허용하는 것이다.The second tilting part 320 is provided between the camera support part 230 and the camera 400 so that the camera 400 can move forward and backward with respect to the vertical direction in which the second unit 200 moves up and down as shown in FIG. 3B. It is to allow the meeting.
이하, 제2 유닛(200) 및 제3 유닛(300)의 각부에 대하여 더욱 구체적으로 살펴보고자 한다.Hereinafter, each part of the second unit 200 and the third unit 300 will be described in more detail.
우선, 제2 유닛(200)의 승강부(210)는, 다시 도 5 내지 도 7을 참조하면, 상부 프레임(211)과, 상부 프레임(211)과 이격하여 하부에 배치되는 하부 프레임(212)과, 상부 프레임(211)에 상단부가 결합되고, 하부 프레임(212)에 하단부가 결합되며, 승강 지지부(220)에 의하여 승강 동작이 지지되는 복수의 승강봉(213)을 포함하는 것을 알 수 있다.First, referring to FIGS. 5 to 7 again, the lifting unit 210 of the second unit 200 may have an upper frame 211 and a lower frame 212 disposed below the upper frame 211. And, the upper end is coupled to the upper frame 211, the lower end is coupled to the lower frame 212, it can be seen that it includes a plurality of lifting rods 213 that the lifting operation is supported by the lifting support 220. .
그리고, 승강부(210)는, 상부 프레임(211)에 상단부가 결합되고, 하부 프레임(212)에 하단부가 결합되며, 외주면을 따라 나사산(이하 미도시)이 형성된 제1 스크류봉(214)과, 제1 스크류봉(214)과 연결되어 정, 역회전 가능하게 장착되고, 하부 프레임(212)에 배치되는 제1 리니어 모터(215)를 포함할 수 있다.And, the lifting unit 210, the upper end is coupled to the upper frame 211, the lower end is coupled to the lower frame 212, the first screw rod 214 and the thread (not shown) formed along the outer circumferential surface and It may include a first linear motor 215 connected to the first screw rod 214 so as to be mounted forward and reversely and disposed on the lower frame 212.
여기서, 후술할 카메라 지지부(230)는 복수의 승강봉(213)을 따라 승강 왕복 가능한 것을 알 수 있다.Here, it can be seen that the camera support 230 to be described later can be lifted and reciprocated along the plurality of lifting rods 213.
한편, 제2 유닛(200)의 승강 지지부(220)는, 제1 유닛(100) 중 작동 공간(101)이 중간에 형성되는 링 형상의 장착 본체(110) 내측면 양측에 적어도 하나 이상 각각 형성되며, 승강부(210)의 승강봉(213)들이 승강 왕복하는 것을 지지하는 복수의 리니어 가이드(221)를 포함하는 것을 파악할 수 있다.On the other hand, the lifting support 220 of the second unit 200, at least one is formed on each of both sides of the inner surface of the ring-shaped mounting body 110, the operating space 101 is formed in the middle of the first unit 100, respectively In addition, it can be seen that the lifting rods 213 of the lifting unit 210 include a plurality of linear guides 221 supporting lifting up and down.
*또한, 제2 유닛(200)의 카메라 지지부(230)는, 복수의 승강봉(213)을 따라 승강 왕복하는 승강편(231)과, 승강편(231)의 전방면에 배치되고, 카메라(400)의 양측면이 회동 가능하게 결합되는 지지 브라켓(232)을 포함할 수 있다.In addition, the camera support part 230 of the second unit 200 is arranged on the front and rear surfaces of the elevating piece 231 and the elevating piece 231, which elevate and reciprocate along the plurality of elevating rods 213. Both sides of the 400 may include a support bracket 232 rotatably coupled.
그리고, 카메라 지지부(230)는, 상부 프레임(211)에 상단부가 결합되고, 하부 프레임(212)에 하단부가 결합되며, 외주면을 따라 나사산이 형성된 제2 스크류봉(234)과, 제2 스크류봉(234)과 연결되어 정, 역회전 가능하게 장착되고, 승강편(231)에 배치되는 제2 리니어 모터(235)를 포함할 수 있다.In addition, the camera support 230 has an upper end coupled to the upper frame 211, a lower end coupled to the lower frame 212, and a second screw rod 234 having a thread formed along an outer circumferential surface thereof, and a second screw rod. It may include a second linear motor 235 connected to the 234 so as to be mounted in a forward and reverse rotation and disposed on the elevating piece 231.
이때, 제3 유닛(300)은 승강편(231) 및 지지 브라켓(232)에 형성되는 것을 알 수 있다.At this time, it can be seen that the third unit 300 is formed on the lifting piece 231 and the support bracket 232.
한편, 제3 유닛(300)의 제1 틸팅부(310)는, 승강봉(213)을 따라 승강 왕복 가능한 카메라 지지부(230)의 승강편(231)과, 승강편(231)의 전방면에 배치되는 지지 브라켓(232)의 중심부 사이에 배치되는 제1 회동 모터(311)를 포함할 수 있다.On the other hand, the first tilting portion 310 of the third unit 300, the lifting piece 231 and the front surface of the lifting piece 231 of the camera support portion 230 capable of lifting up and down along the lifting bar 213. It may include a first rotating motor 311 disposed between the center of the support bracket 232 is disposed.
여기서, 제1 회동 모터(311)는 지지 브라켓(232)의 중심부를 회동축으로 하여 도 3(a)와 같이 지지 브라켓(232)을 승강편(231) 상에서 정, 역회전시키는 것이다.Here, the first rotational motor 311 rotates the support bracket 232 forward and backward on the lifting piece 231 as shown in FIG. 3 (a) using the center of the support bracket 232 as the rotation shaft.
한편, 제3 유닛(300)의 제2 틸팅부(320)는, 카메라 지지부(230)의 지지 브라켓(232) 양단부에 각각 구비되어 카메라(400)의 양측면을 회동 가능하게 지지하는 지지편(233a, 233b) 중 일측의 지지편(233b)과 카메라(400)의 일측면 사이에 배치되는 제2 회동 모터(321)를 포함할 수 있다On the other hand, the second tilting part 320 of the third unit 300 is provided on both ends of the support bracket 232 of the camera support 230, the support piece 233a for rotatably supporting both sides of the camera 400 It may include a second rotation motor 321 disposed between the support piece 233b of one side of the 233b and one side of the camera 400.
여기서, 제2 회동 모터(321)는 지지편(233b)의 단부를 회동축으로 하여 카메라(400)를 지지편(233b)에 대하여 도 3(b)와 같이 정, 역회전시키는 것이다.Here, the second rotation motor 321 rotates the camera 400 forward and reverse with respect to the support piece 233b with the end of the support piece 233b as the rotation shaft.
이때, 제2 틸팅부(320)는, 지지편(233a, 233b) 각각에 일정 길이로 관통되어 카메라(400)의 양측면이 결합된 위치를 조정할 수 있도록 조절 슬롯(233s)을 더 구비할 수도 있음은 물론이다.In this case, the second tilting part 320 may further include an adjustment slot 233s to penetrate each of the support pieces 233a and 233b to a predetermined length so as to adjust a position where both sides of the camera 400 are coupled. Of course.
따라서, 제1, 2 리니어 모터(215, 235)의 구동력이 제1, 2 스크류봉(214, 234)을 통하여 승강봉(213) 및 승강편(231)에 전달되는 리니어 가이드(linear guide)의 구조를 채택함으로써, 제2 유닛(200)의 정확하고 미세한 위치 결정이 가능하게 될 것이다.Accordingly, the linear guide of the driving force of the first and second linear motors 215 and 235 is transmitted to the lifting bar 213 and the lifting piece 231 through the first and second screw rods 214 and 234. By adopting the structure, accurate and fine positioning of the second unit 200 will be possible.
특히, 본 발명은 조작자가 기존의 리모트 컨트롤러로 제1, 2, 3 유닛(100, 200, 300)의 조작을 수행할 수 있음은 물론, 비행 본체(500)의 일측에 구비된 수신부(이하 미도시)와 제1, 2, 3 유닛(100, 200, 300)을 전기적으로 연결시키고, 스마트폰이나 휴대용 PC 또는 태블릿 PC 등과 같은 조작자의 휴대용 단말기와 전술한 수신부가 상호 통신하는 리모트 컨트롤러의 대용으로 활용하는 것 또한 가능하다.In particular, the present invention, the operator can perform the operation of the first, second, third unit (100, 200, 300) with the existing remote controller, as well as a receiver provided on one side of the flight main body 500 (hereinafter referred to as H) and the first, second, and third units 100, 200, and 300 electrically connected to each other, and are used as a substitute for a remote controller that communicates with a portable terminal of an operator such as a smartphone, a portable PC or a tablet PC, and the aforementioned receiver. It is also possible to utilize.
상기와 같은 본 발명에 따른 드론용 짐벌 어셈블리의 작동 과정에 관하여 도 8 및 도 9를 참조하여 살펴보기로 하며, 도 8 및 도 9에서 표시되지 않은 도면부호는 도 1 내지 도 7을 참조한다.An operation process of the gimbal assembly for a drone according to the present invention as described above will be described with reference to FIGS. 8 and 9, and reference numerals not shown in FIGS. 8 and 9 refer to FIGS. 1 to 7.
우선, 사용자가 휴대용 단말기나 리모트 컨트롤러(이하 '조작기')로 비행 본체(500)의 비행용 블레이드(600)를 구동시켜 비행 본체(500)를 비행시킨다.First, the user drives the flight blade 600 of the flight body 500 by using a portable terminal or a remote controller (hereinafter, 'operator') to fly the flight body 500.
여기서, 조작자가 높은 곳에서 조감하는 뷰로 대상물의 사진 및 동영상을 촬영하기 위하여 조작기로 제2 유닛(200) 및 제3 유닛(300)의 하강을 조작하게 되면, 승강봉(213)들은 리니어 가이드(221)를 따라 하강하게 되며, 하부 프레임(212)은 도 8과 같이 제2 플레이트(520)의 하부측에 배치된다.Here, when the operator manipulates the descending of the second unit 200 and the third unit 300 by using the manipulator to take a picture and video of the object in a view that is viewed from a high place, the lifting rods 213 are linear guides ( 221 is lowered, and the lower frame 212 is disposed on the lower side of the second plate 520 as shown in FIG.
이때, 조작자는 카메라(400)의 상하 승강 방향에 대하여 좌우 방향의 회동 동작(도 3(a) 하부측의 양방향 원호 화살표 참조)을 위해 제1 회동 모터(311)를 가동시켜 적절한 좌우 경사각을 확보한다.At this time, the operator operates the first rotation motor 311 to secure the proper left and right inclination angles for the left and right pivoting operation (see the bidirectional circular arrow on the lower side of FIG. 3 (a)) with respect to the up and down direction of the camera 400. do.
이와 동시에, 조작자는 카메라(400)의 상하 승강 방향에 대하여 전후 방향의 회동 동작(도 3(b) 하부 좌측의 양방향 원호 화살표 참조)을 위해 제2 회동 모터(321)를 가동시켜 적절한 전후 경사각을 확보하며 촬영하면 될 것이다.At the same time, the operator operates the second rotation motor 321 for the forward and backward rotational motion (refer to the bidirectional circular arrow on the lower left side of FIG. 3 (b)) with respect to the vertical direction of the camera 400. You can shoot while securing.
한편, 조작자가 교량 하판이나 구조물의 하부측에서 비행 본체(500)를 비행시키며 높은 곳을 올려다보는 뷰로 대상물의 사진 및 동영상을 촬영하기 위하여 조작기로 제2 유닛(200) 및 제3 유닛(300)의 상승을 조작하게 되면, 승강봉(213)들은 리니어 가이드(221)를 따라 상승하게 되며, 상부 프레임(211)은 도 9와 같이 제1 플레이트(510)의 상부측에 배치된다.On the other hand, the second unit 200 and the third unit 300 with the manipulator in order to take a picture and video of the object in the view of the operator looking up at a high place while flying the flight main body 500 from the lower side of the bridge plate or structure. When operating the rising of the lifting rods 213 are raised along the linear guide 221, the upper frame 211 is disposed on the upper side of the first plate 510 as shown in FIG.
이때, 조작자는 카메라(400)의 상하 승강 방향에 대하여 좌우 방향의 회동 동작(도 3(a) 하부측의 양방향 원호 화살표 참조)을 위해 제1 회동 모터(311)를 가동시켜 적절한 좌우 경사각을 확보한다.At this time, the operator operates the first rotation motor 311 to secure the proper left and right inclination angles for the left and right pivoting operation (see the bidirectional circular arrow on the lower side of FIG. 3 (a)) with respect to the up and down direction of the camera 400. do.
이와 동시에, 조작자는 카메라(400)의 상하 승강 방향에 대하여 전후 방향의 회동 동작(도 3(b) 하부 좌측의 양방향 원호 화살표 참조)을 위해 제2 회동 모터(321)를 가동시켜 적절한 전후 경사각을 확보하며 촬영하면 될 것이다.At the same time, the operator operates the second rotation motor 321 for the forward and backward rotational motion (refer to the bidirectional circular arrow on the lower left side of FIG. 3 (b)) with respect to the vertical direction of the camera 400. You can shoot while securing.
이상과 같이 본 발명은 드론에 장착되는 카메라의 위치 조정이 자유로이 이루어짐은 물론, 위치 결정이 정확하고 미세하게 이루어질 수 있도록 하는 드론용 짐벌 어셈블리를 제공하는 것을 기본적인 기술적 사상으로 하고 있음을 알 수 있다.As described above, it can be seen that the present invention has as its basic technical idea to provide a drone gimbal assembly for allowing the positioning of the camera mounted on the drone to be freely performed, as well as to accurately and precisely position the camera.
그리고, 본 발명의 기본적인 기술적 사상의 범주 내에서 당해 업계 통상의 지식을 가진 자에게 있어서는 다른 많은 변형 및 응용 또한 가능함은 물론이다.In addition, many modifications and applications are possible to those skilled in the art within the scope of the basic technical idea of the present invention.
Claims (4)
- 드론의 비행 본체에 정, 역회전 가능하게 장착되며, 중간에 작동 공간이 형성되는 제1 유닛;A first unit mounted on the flight main body of the drone so as to be forward and reverse rotation and having an operation space formed therebetween;상기 제1 유닛에 장착되어 상기 작동 공간에 승강 왕복 가능하게 배치되는 제2 유닛; 및A second unit mounted to the first unit and disposed to move up and down in the working space; And상기 제2 유닛에 장착되어 일측에 카메라가 구비되며, 상기 카메라를 상기 제2 유닛의 일측에 대하여 회동시키는 제3 유닛을 포함하고,A third unit mounted to the second unit and provided with a camera on one side, and rotating the camera with respect to one side of the second unit,상기 제2 유닛은, 상기 카메라를, 상기 비행 본체의 상면보다 위로 상승시키거나, 상기 비행 본체의 하면보다 아래로 하강시키는 것을 특징으로 하는 드론용 짐벌 어셈블리.The second unit, the gimbal assembly for a drone, characterized in that to raise the camera above the upper surface of the flying body, or lower than the lower surface of the flying body.
- 청구항 1에 있어서,The method according to claim 1,상기 제1 유닛은,The first unit,상기 작동 공간이 중간에 형성되는 링 형상의 장착 본체와,A ring-shaped mounting body in which the working space is formed in the middle,상기 비행 본체에 구비되며, 상기 비행 본체에 장착된 상기 장착 본체를 정, 역회전시키는 회전 구동부를 포함하는 것을 특징으로 하는 드론용 짐벌 어셈블리.The gimbal assembly for a drone, which is provided in the flying main body, and comprises a rotation drive unit for forward and reverse rotation of the mounting body mounted on the flying body.
- 청구항 1에 있어서,The method according to claim 1,상기 제2 유닛은,The second unit,상기 제1 유닛의 작동 공간을 관통하여 상하로 승강 왕복하는 승강부와,An elevating unit configured to reciprocate up and down through the operating space of the first unit;상기 작동 공간을 형성하는 상기 제1 유닛의 내측면에 형성되어 상기 승강부의 왕복을 지지하는 승강 지지부와,An elevating support part formed on an inner side of the first unit forming the operating space and supporting a reciprocating of the elevating part;상기 승강부에 왕복 가능하게 장착되어 상기 카메라를 지지하는 카메라 지지부를 포함하며,A camera support part mounted reciprocally on the lifting part to support the camera,상기 제3 유닛은 상기 카메라 지지부에 구비되는 것을 특징으로 하는 드론용 짐벌 어셈블리.The third unit is a gimbal assembly for a drone, characterized in that provided in the camera support.
- 청구항 3에 있어서,The method according to claim 3,상기 제3 유닛은,The third unit,상기 카메라 지지부와 상기 승강부 사이에 장착되어 상기 제2 유닛이 승강 왕복하는 상하 방향에 대하여 좌우 방향으로 상기 카메라의 회동을 허용하는 제1 틸팅부와,A first tilting part mounted between the camera support part and the lifting part to allow the camera to rotate in a left-right direction with respect to an up-down direction in which the second unit moves up and down;상기 카메라 지지부와 상기 카메라 사이에 구비되어 상기 제2 유닛이 승강 왕복하는 상하 방향에 대하여 전후 방향으로 상기 카메라의 회동을 허용하는 제2 틸팅부를 포함하는 것을 특징으로 하는 드론용 짐벌 어셈블리.And a second tilting part provided between the camera support part and the camera to allow the camera to rotate in a front-rear direction with respect to a vertical direction in which the second unit moves up and down.
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