WO2017222249A1 - Ensemble cardan destiné à un drone - Google Patents

Ensemble cardan destiné à un drone Download PDF

Info

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
Authority
WO
WIPO (PCT)
Prior art keywords
unit
camera
drone
gimbal assembly
lifting
Prior art date
Application number
PCT/KR2017/006360
Other languages
English (en)
Korean (ko)
Inventor
정우철
Original Assignee
주식회사 엠지아이티
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 주식회사 엠지아이티 filed Critical 주식회사 엠지아이티
Publication of WO2017222249A1 publication Critical patent/WO2017222249A1/fr

Links

Images

Classifications

    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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
    • 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.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Remote Sensing (AREA)
  • Accessories Of Cameras (AREA)
  • Studio Devices (AREA)

Abstract

La présente invention concerne un ensemble cardan destiné à un drone, comprenant : une première unité montée sur un corps de vol d'un drone de façon à pouvoir tourner vers l'avant/l'arrière, un espace de manœuvre étant formé au milieu de la première unité ; une seconde unité montée sur la première unité et disposée dans l'espace de manœuvre de façon à pouvoir effectuer des mouvements alternatifs vers le haut/vers le bas ; et une troisième unité qui est montée sur la deuxième unité et qui comporte une caméra montée sur un côté de cette dernière de sorte que la caméra tourne par rapport à un côté de la deuxième unité. La deuxième unité élève la caméra au-dessus de la surface supérieure du corps de vol ou abaisse la caméra au-dessous de la surface inférieure du corps de vol de sorte que non seulement la position de la caméra montée sur le drone puisse être réglée librement, mais également que cette position puisse être déterminée de manière exacte et précise.
PCT/KR2017/006360 2016-06-20 2017-06-16 Ensemble cardan destiné à un drone WO2017222249A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR10-2016-0076431 2016-06-20
KR1020160076431A KR101689197B1 (ko) 2016-06-20 2016-06-20 드론용 짐벌 어셈블리

Publications (1)

Publication Number Publication Date
WO2017222249A1 true WO2017222249A1 (fr) 2017-12-28

Family

ID=57736089

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/KR2017/006360 WO2017222249A1 (fr) 2016-06-20 2017-06-16 Ensemble cardan destiné à un drone

Country Status (2)

Country Link
KR (1) KR101689197B1 (fr)
WO (1) WO2017222249A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109050917A (zh) * 2018-09-04 2018-12-21 天津微旋风科技有限公司 一种带跟随系统的多功能摄录无人机
US10175693B2 (en) * 2015-09-11 2019-01-08 Sz Dji Osmo Technology Co., Ltd. Carrier for unmanned aerial vehicle
CN109555959A (zh) * 2018-11-22 2019-04-02 四川西华通用航空股份有限公司 一种高速航空摄影云台
CN114845045A (zh) * 2022-03-24 2022-08-02 安徽超清科技股份有限公司 一种基于5g的高速视频巡检装置
CN116902244A (zh) * 2023-09-08 2023-10-20 成都庆龙航空科技有限公司 一种无人机机载侦查吊舱

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107117324B (zh) * 2017-04-07 2019-08-20 清远市巨劲科技有限公司 一种环形无人机及其航拍装置
KR101848690B1 (ko) 2017-08-11 2018-04-13 최종필 가상현실용 카메라 짐벌을 갖는 무인비행기
KR101865280B1 (ko) * 2018-02-14 2018-06-07 중앙항업(주) 항공촬영용 드론에 설치되는 승강장치
KR101976671B1 (ko) * 2019-02-01 2019-05-09 주식회사 고산자 무인비행장치용 다각도 멀티 카메라 장착구
KR102170907B1 (ko) * 2019-05-09 2020-10-28 주식회사 이쓰리 무인항공기를 이용한 미세먼지 측정장치
KR102313437B1 (ko) 2020-02-18 2021-10-19 단국대학교 산학협력단 초분광영상을 이용한 하천 지형측량 방법
KR102313438B1 (ko) 2020-02-18 2021-10-18 단국대학교 산학협력단 초분광영상을 이용한 하상 변동속도 측정 방법
KR102472036B1 (ko) * 2020-10-28 2022-11-29 (주)비씨디이엔씨 짐벌 장치
KR102583857B1 (ko) 2021-11-23 2023-10-04 동아대학교 산학협력단 멀티스펙트럴 카메라 흔들림 방지 기능을 갖는 식생정보 취득용 드론
KR20230139923A (ko) 2022-03-28 2023-10-06 주식회사 유시스 드론용 스마트폰 짐벌

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20120115059A (ko) * 2011-04-07 2012-10-17 구해원 카메라 제어장치
JP2015523930A (ja) * 2011-09-09 2015-08-20 エスゼット ディージェイアイ テクノロジー カンパニー，リミテッド 無人航空機に使用するための２軸架台、無人航空機に使用するための３軸架台、および多重回転子航空機
KR101598411B1 (ko) * 2015-10-20 2016-02-29 제주대학교 산학협력단 3차원 사진측량용 무인항공기 짐벌시스템
KR101617808B1 (ko) * 2014-11-12 2016-05-03 이정숙 카메라 균형제어 기능을 갖는 헬리캠용 짐벌 장치
KR101619836B1 (ko) * 2016-02-05 2016-05-11 (주)아세아항측 드론을 이용한 초분광 원격모니터링 시스템

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101302442B1 (ko) 2011-10-25 2013-09-02 김성남 무인항공기 카메라 폴딩장치

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20120115059A (ko) * 2011-04-07 2012-10-17 구해원 카메라 제어장치
JP2015523930A (ja) * 2011-09-09 2015-08-20 エスゼット ディージェイアイ テクノロジー カンパニー，リミテッド 無人航空機に使用するための２軸架台、無人航空機に使用するための３軸架台、および多重回転子航空機
KR101617808B1 (ko) * 2014-11-12 2016-05-03 이정숙 카메라 균형제어 기능을 갖는 헬리캠용 짐벌 장치
KR101598411B1 (ko) * 2015-10-20 2016-02-29 제주대학교 산학협력단 3차원 사진측량용 무인항공기 짐벌시스템
KR101619836B1 (ko) * 2016-02-05 2016-05-11 (주)아세아항측 드론을 이용한 초분광 원격모니터링 시스템

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10175693B2 (en) * 2015-09-11 2019-01-08 Sz Dji Osmo Technology Co., Ltd. Carrier for unmanned aerial vehicle
US11262760B2 (en) 2015-09-11 2022-03-01 Sz Dji Osmo Technology Co., Ltd. Carrier for unmanned aerial vehicle
CN109050917A (zh) * 2018-09-04 2018-12-21 天津微旋风科技有限公司 一种带跟随系统的多功能摄录无人机
CN109555959A (zh) * 2018-11-22 2019-04-02 四川西华通用航空股份有限公司 一种高速航空摄影云台
CN114845045A (zh) * 2022-03-24 2022-08-02 安徽超清科技股份有限公司 一种基于5g的高速视频巡检装置
CN114845045B (zh) * 2022-03-24 2023-08-29 安徽超清科技股份有限公司 一种基于5g的高速视频巡检装置
CN116902244A (zh) * 2023-09-08 2023-10-20 成都庆龙航空科技有限公司 一种无人机机载侦查吊舱

Also Published As

Publication number Publication date
KR101689197B1 (ko) 2016-12-23

Similar Documents

Publication Publication Date Title
WO2017222249A1 (fr) Ensemble cardan destiné à un drone
US11927877B2 (en) Interchangeable mounting platform
US10670183B2 (en) Systems and methods for payload stabilization
CN206147927U (zh) 无人机的遥控器结构
CN104019348A (zh) 手持三轴自稳拍摄云台
WO2013033925A1 (fr) Tête à rotule à deux axes pour utilisation dans un petit aéronef sans pilote et tête à rotule à trois axes pour utilisation dans un petit aéronef sans pilote
CN111578081A (zh) 云台、遥控车辆及遥控运载系统
WO2010005203A2 (fr) Véhicule volant de type pale de fond rotationnelle
CN103672340A (zh) 一种手持三轴拍摄云台
CN104859857A (zh) 一种单镜头全景无人机系统
KR102069240B1 (ko) 함상 드론 착륙장치 및 이를 이용한 함상 드론 착륙 제어방법
CN203940203U (zh) 手持三轴自稳拍摄云台
WO2018023328A1 (fr) Tête de logement et aéronef sans pilote
WO2019062140A1 (fr) Véhicule aérien sans pilote
WO2018223742A1 (fr) Tête à berceau, dispositif de prise de vues pourvu de ladite tête à berceau et véhicule aérien sans pilote
WO2019041188A1 (fr) Appareil de détection el pour ensemble photovoltaïque et véhicule aérien sans pilote
WO2019100824A1 (fr) Véhicule aérien sans pilote
CN210852902U (zh) 一种新型的多旋翼无人机结构
CN211176005U (zh) 集成相机机身的云台组件和拍摄设备
KR20170087268A (ko) 드론 장착용 촬영장치
CN210725068U (zh) 智能摄影系统
CN217706272U (zh) 一种具有全景镜头模组的无人机
CN212435792U (zh) 一种摄像头模组的组装设备
CN211364976U (zh) 一种无人机云台照明装置
CN218343747U (zh) 一种倾斜摄影相机总成

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 17815662

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC (EPO FORM 1205A DATED 27.03.2019)

122 Ep: pct application non-entry in european phase

Ref document number: 17815662

Country of ref document: EP

Kind code of ref document: A1