KR101302442B1 - Camera Polding system - Google Patents

Camera Polding system Download PDF

Info

Publication number
KR101302442B1
KR101302442B1 KR1020110109602A KR20110109602A KR101302442B1 KR 101302442 B1 KR101302442 B1 KR 101302442B1 KR 1020110109602 A KR1020110109602 A KR 1020110109602A KR 20110109602 A KR20110109602 A KR 20110109602A KR 101302442 B1 KR101302442 B1 KR 101302442B1
Authority
KR
South Korea
Prior art keywords
link
camera
fixed
bracket
rotation axis
Prior art date
Application number
KR1020110109602A
Other languages
Korean (ko)
Other versions
KR20130045122A (en
Inventor
김성남
신진욱
김태균
윤성준
Original Assignee
김성남
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 김성남 filed Critical 김성남
Priority to KR1020110109602A priority Critical patent/KR101302442B1/en
Publication of KR20130045122A publication Critical patent/KR20130045122A/en
Application granted granted Critical
Publication of KR101302442B1 publication Critical patent/KR101302442B1/en

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/08—Arrangements of cameras
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • 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
    • G03B15/00—Special procedures for taking photographs; Apparatus therefor
    • G03B15/006—Apparatus mounted on flying objects
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Accessories Of Cameras (AREA)

Abstract

본 발명은 무인항공기 카메라 폴장치에 관한 것으로, 더욱 상세하게는 기체가 순항 비행시에는 카메라를 동체안으로 집어 넣어 항력감소 및 양향비를 증대하고, 이착륙 또는 추락시 카메라가 동체안으로 접혀들어가 있어 고가의 영상장비를 보호할 수 있도록 함과 동시에 영상 취득시에는 카메라를 90도 각도로 틸팅하여 원활한 시야를 확보하도록 한 것이다.The present invention relates to an unmanned aerial vehicle camera device, more specifically, to put the camera into the fuselage during cruising flight to increase drag reduction and lift ratio, and the camera is folded into the fuselage during take-off or landing, expensive In addition to protecting video equipment, the camera can be tilted at an angle of 90 degrees to ensure a smooth field of view.

Description

무인항공기 카메라 폴딩장치{Camera Polding system}Unmanned aerial vehicle camera folding device {Camera Polding system}

본 발명은 무인항공기 카메라 폴딩장치에 관한 것으로, 더욱 상세하게는 기체가 순항 비행시에는 카메라를 동체안으로 집어 넣어 항력감소 및 양향비를 증대하고, 이착륙 또는 추락시 카메라가 동체안으로 접혀들어가 있어 고가의 영상장비를 보호할 수 있도록 함과 동시에 영상 취득시에는 카메라를 90도 각도로 틸팅하여 원활한 시야를 확보하도록 한 것이다.The present invention relates to an unmanned aerial vehicle camera folding apparatus, and more particularly, when the aircraft is cruising flight, the camera is put into the fuselage to increase drag reduction and lift ratio, and the camera is folded into the fuselage during take-off or landing. In addition to protecting video equipment, the camera can be tilted at an angle of 90 degrees to ensure a smooth field of view.

일반적으로 무인항공기는 사람이 탑승하지 않고 원격조작(遠隔操作)에 의하여 조종되는 무인 항공기를 말한다. Generally, an unmanned airplane refers to an unmanned airplane that is operated by a remote operation without being carried by a person.

이러한 무선조종항공기는 대공 미사일 추적훈련, 무인정찰 및 감시임무를 수행하므로 전세계적으로 무선조종항공기의 개발 및 운용이 활발하게 이루어지고 있다. Since these radio controlled aircraft perform anti-missile tracking training, unmanned reconnaissance and surveillance missions, the development and operation of radio controlled aircraft are being actively carried out around the world.

무인정찰 또는 무인촬영을 위한 카메라 장치는 비행기 동체안에 카메라가 지상을 촬영할 수 있도록 노출하거나 또는 모터의 작동에 의하여 회전되는 원리의 카메라 장치를 장착하고 있다.The camera device for unmanned reconnaissance or unmanned photographing is equipped with a camera device of the principle that the camera is exposed to photograph the ground in the airplane body or rotated by the operation of the motor.

종래의 카메라 틸팅장치는 모터와 링크기구를 이용하여 일정각도 통상 90도 각도로 회전시켜 지상을 촬영하도록 하고 있으며 이때 카메라는 자체의 하중에 의하여 흔들리는 것을 방지하기 위하여 항상 서보 모터에 전원을 인가한 상태로 고정하여 사용되므로 모터에 부하가 걸리게 되는 폐단이 발생하는 문제점이 있었다.Conventional camera tilting device rotates at a constant angle of 90 degrees by using a motor and a link mechanism to photograph the ground, and at this time, the camera always applies power to the servo motor to prevent it from being shaken by its own load. Since it is used to fix the motor, there is a problem in that a closed end of the load is applied to the motor.

본 발명은 상기한 종래의 문제점을 해결하기 위하여 안출한 것으로서, 본 발명의 목적은 기체가 순항 비행시에는 카메라를 동체안으로 집어 넣어 항력감소 및 양향비를 증대하고, 이착륙 또는 추락시 카메라가 동체안으로 접혀들어가 있어 고가의 영상장비를 보호할 수 있도록 함과 동시에 영상 취득시에는 카메라를 90도 각도로 틸팅된 상태에서 자동적으로 락이 걸리게하여 원활한 시야를 확보하도록 한 것이다.The present invention has been made to solve the above-mentioned conventional problems, the object of the present invention is to put the camera into the fuselage when the aircraft is cruising flight to increase the drag reduction and lift ratio, the camera is taken into the fuselage during take-off or landing It is folded to protect expensive video equipment, and at the same time, the camera is automatically locked by tilting the camera at a 90-degree angle to secure a smooth field of view.

상기한 목적을 달성하기 위한 본 발명은 카메라의 자중에 의한 카메라 수직방향으로의 이력발생시 링크기구로 연결된 회전축의 중심점을 카메라가 90도 틸팅위치에서 링크가 자동적으로 락이 되도록하여 서보 모터에 걸리는 부하를 차단하고, 서보 모터 전원 차단시에도 카메라가 쳐지지 않음으로서 안전성이 증대되도록 한 틸팅장치를 제공하는데 있다.The present invention to achieve the above object is to load the load on the servo motor by the camera automatically locks the link at the center point of the rotation axis connected to the link mechanism when the history in the vertical direction of the camera due to the weight of the camera automatically tilted 90 degrees The present invention provides a tilting device that cuts off and the camera does not fall even when the servo motor is turned off.

본 발명에 따른 무인항공기용 카메라 틸팅장치는 카메라가 90도 각도 틸팅위치에서 링크기구가 자체적으로 락이 걸리게되어 서보 모터에 부하를 차단하여 전력소모율의 감소를 노릴 수있으며, 서버 모터 차단시에도 락이 걸려있어 카메라가 아래로 쳐지지 않음으로서 안정성이 증대되는 효과를 가진다.In the camera tilting device for an unmanned aerial vehicle according to the present invention, the link mechanism is locked by itself at a 90 degree angle tilting position of the camera, thereby blocking the load on the servo motor, thereby reducing the power consumption rate, and locking occurs even when the server motor is blocked. There is an effect that the stability is increased by the camera does not fall down.

또한 순항시에는 고가의 카메라 장치를 동체안으로 집어넣어 항력감소, 양항비가 증대되고, 영상 취득시에만 90도 각도로 틸팅하여 영상을 취득하여 이착륙 또는 불시착이 고가의 카메라 장비를 보호할 수 있는 효과를 가진다.When cruising, the expensive camera device is inserted into the fuselage to increase drag reduction and lifting ratio, and by only tilting the camera at an angle of 90 degrees when acquiring images, it is possible to protect expensive camera equipment by taking off or landing. Have

도 1은 본 발명에 따른 틸팅장치의 사시도.
도 2는 본 발명의 카메라가 접혀져 있는 상태의 측면도.
도 3은 본 발명의 카메라가 90도 각도로 틸팅된 상태의 측면도.
본 4는 본 발명의 배면 사시도.
도 5는 비행기 동체와 결합되어 90도 각도로 틸팅된 상태의 측면도.1 is a perspective view of a tilting device according to the present invention.
2 is a side view of a state in which the camera of the present invention is folded.
Figure 3 is a side view of the camera of the present invention tilted at a 90 degree angle.
4 is a rear perspective view of the present invention.
Figure 5 is a side view of the state coupled to the aircraft fuselage tilted at an angle of 90 degrees.

본 발명에 따른 무인항공기 카메라 틸팅장치는 카메라의 자중에 의한 카메라 수직방향으로의 이력발생시 링크기구로 연결된 회전축의 중심점을 카메라가 90도 틸팅위치에서 카메라 수직 방향으로 모멘트가 발생하여 링크가 자동적으로 락이 되도록 한 것을 특징으로 한다.In the unmanned aerial vehicle tilting device according to the present invention, when the hysteresis of the camera in the vertical direction due to the camera's own weight, the moment is generated in the vertical direction of the camera from the tilting position of the camera to the center point of the rotation axis connected by the link mechanism, the link is automatically locked It is characterized by one.

이하 첨부된 도면을 참조하여 본 발명의 바람직한 실시예를 상세하게 설명하도록 한다. 첨부된 도면은 축척에 의하여 도시되지 않았으며, 각 도면의 동일한 참조 번호는 동일한 구성 요소를 지칭한다.Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. The accompanying drawings are not drawn to scale and wherein like reference numerals in the various drawings refer to like elements.

도 1은 본 발명에 따른 틸팅장치의 사시도, 도 2는 본 발명의 카메라가 접혀져 있는 상태의 측면도, 도 3은 본 발명의 카메라가 90도 각도로 틸팅된 상태의 측면도이다.1 is a perspective view of a tilting apparatus according to the present invention, FIG. 2 is a side view of a state in which the camera of the present invention is folded, and FIG. 3 is a side view of a state of the camera of the present invention tilted at a 90 degree angle.

도 1 내지 도 3에 따른 본 발명의 제 1실시예는, 항공기 동체에 고정되는 고정브라켓(1), 상기 고정브라켓(1)의 좌우 측면 회전축(A)을 중심으로 회전가능하도록 설치되는 틸팅브라켓(3), 상기 틸팅브라켓(3)의 회전축(B)을 중심으로 회전하는 타이밍풀리(7)와, 상기 타이밍풀리(7)에 고정되어 연동 회전하는 링크(5) 및 고정브라켓(1)에 고정되어 상기 링크(5)에 연결되어 관절 형식으로 꺽여지면서 연동되어 틸팅브라켓(3)을 90도 각도로 접히도록하는 링크(8)를 구성하고, 상기 틸팅브라켓에 서보 모터(9)를 고정하여 이에 타이밍풀리(4)를 연결하여 타이밍벨트(6)를 타이밍풀리(4)(7)에 착설하여 회전력을 전달하도록 구성한 것이다.The first embodiment of the present invention according to Figures 1 to 3, a fixed bracket (1) fixed to the aircraft body, the tilting bracket is installed to be rotatable around the left and right side rotation axis (A) of the fixed bracket (1) (3), the timing pulley (7) rotates about the rotation axis (B) of the tilting bracket (3), and the link (5) and the fixed bracket (1) fixed to the timing pulley (7) and interlocked rotation Fixed to form a link (8) connected to the link (5) to be bent in a joint form to fold the tilting bracket (3) at an angle of 90 degrees, and to fix the servo motor (9) to the tilting bracket Thus, the timing pulley 4 is connected to the timing belt 6 so as to be installed on the timing pulleys 4 and 7 so as to transmit rotational force.

상기한 링크(5)(8) 기구는 고정브라켓(1)의 회전축(D)과 타이밍풀리(4)의 회전축(B)에 회전자재케 축설되어 회전축(C)으로 연결되어 카메라 자중에 의한 수직방향으로의 외력발생시 회전축(C)과 회전축(D)의 중심점을 연결한 선 위쪽의 회전축(B)이 위치하여 카메라 중심의 수직방향(F방향)으로 모멘트가 발생하여 자동적으로 링크가 락이 되는 것이다.The above-mentioned link 5 and 8 mechanisms are pivotally arranged on the rotating shaft D of the fixing bracket 1 and the rotating shaft B of the timing pulley 4, and are connected to the rotating shaft C to be perpendicular to the camera's own weight. When the external force occurs in the direction, the rotation axis (B) above the line connecting the rotation axis (C) and the center point of the rotation axis (D) is located, and the moment is generated in the vertical direction (F direction) of the camera center, and the link is automatically locked. .

또한 링크기구는 고정브라켓에 고정된 링크(8)가 타이밍풀리에 고정된 링크(5) 안쪽으로 매립되는 상태로 작동하여 접히거나 펴질때 링크 안쪽에서 자동적으로 락이 걸리게 되는 것이다.In addition, the link mechanism is operated in a state in which the link 8 fixed to the fixing bracket is embedded into the link 5 fixed to the timing pulley to automatically lock on the inside of the link when folded or unfolded.

상기한 타이밍풀리(4)(7)는 서보모터(9)에 연결되는 풀리는 소구경의 풀리로 틸팅브라켓 회전축(B)에 연결되는 풀리는 대구경의 풀리로 구성하여 타이밍벨트를 착설하여 원하는 감속비를 얻어 정확한 동작을 유도하는 것이다.The timing pulley (4) (7) is a pulley of the small diameter pulley connected to the servo motor (9) consists of a pulley of the large diameter pulley connected to the tilting bracket rotation axis (B) to install the timing belt to obtain the desired reduction ratio To induce correct behavior.

이때 타이밍벨트의 중간지점 틸팅브라켓(3)에 벨트 텐셔너(20)를 설치하여 벨트의 장력조절과 벨트의 처짐을 방지하는 것이다.At this time, the belt tensioner 20 is installed on the intermediate point tilting bracket 3 of the timing belt to prevent tension of the belt and sagging of the belt.

상기한 틸팅브라켓(3)에는 카메라 및 영상처리장치(2)가 설치되는 것이다.The tilting bracket 3 is provided with a camera and an image processing apparatus 2.

상기와 같이 구성된 본 발명의 동작상태를 도면을 참조하여 설명하면 도2는 카메라가 접혀진 상태로 이 상태에서 전원이 인가되면 서보모터(9)가 작동되고 서보 모터에 연결된 타이밍풀리(7)가 회전한다.Referring to the operation state of the present invention configured as described above with reference to the drawings Figure 2 is a state in which the camera is folded when the power is applied in this state the servo motor 9 is activated and the timing pulley 7 connected to the servo motor rotates do.

이때 타이밍풀리는 시계방향으로 히전되고 이에 축설된 타이밍벨트(6) 또한 시계방향으로 회전되고 타이밍벨트에 착설된 타이밍풀리(4) 또한 시계방향으로 회전되면서 회전축(A)을 중심으로 틸팅브라켓(3)이 회전되는 것이다.At this time, the timing pulley is rotated in the clockwise direction and the timing belt 6 installed therein is also rotated in the clockwise direction, and the timing pulley 4 mounted on the timing belt is also rotated in the clockwise direction, and the tilting bracket 3 is rotated about the rotation axis A. Will be rotated.

90도 각도로 회전한 후 도 3과 같은 상태를 유지하고 이때 링크(8)가 링크(5) 안쪽에 매립된 상태로 자동적으로 락이 걸리게 되는 것이다.After rotating at an angle of 90 degrees, the state as shown in FIG. 3 is maintained. At this time, the link 8 is automatically locked in a state in which the link 8 is embedded in the link 5.

동체에 내장할 때에는 전술한 동작을 역방향으로 수행하면 도 2와 같은 상태가 되며 이 상태에서는 링크(8)가 회전축(B)에 지지되므로 자동적으로 락이 걸리게 되는 것이다.When embedded in the fuselage, if the above operation is performed in the reverse direction, the state becomes as shown in FIG. 2, and in this state, the link 8 is supported by the rotation shaft B, thereby automatically locking.

따라서 동체에 집어넣을때나 90도 각도로 틸팅할경우 견고한 상태로 고정하여 카메라가 흔들리는 현상이 전혀 없는 것이다.Therefore, when inserting it into the fuselage or tilting at an angle of 90 degrees, the camera is not shaken by fixing it in a solid state.

지금까지 설명한 바와 같이, 본 발명에 따른 무인항공기용 카메라 틸팅장치의 구성 및 작용을 상기 설명 및 도면에 표현하였지만 이는 예를 들어 설명한 것에 불과하여 본 발명의 사상이 상기 설명 및 도면에 한정되지 않으며, 본 발명의 기술적 사상을 벗어나지 않는 범위 내에서 다양한 변화 및 변경이 가능함은 물론이다.As described so far, the configuration and operation of the camera tilting apparatus for the unmanned aerial vehicle according to the present invention have been expressed in the above description and the drawings, which are merely examples, and the spirit of the present invention is not limited to the above description and the drawings. Various changes and modifications are possible without departing from the technical spirit of the present invention.

1: 고정브라켓 3: 틸팅브라켓
4, 7 타이밍풀리 5,8: 링크1: Fixed Bracket 3: Tilting Bracket
4, 7 timing pulley 5,8: link

Claims (3)

항공기 동체에 고정되는 고정브라켓(1), 상기 고정브라켓(1)의 좌우 측면 회전축(A)을 중심으로 회전가능하도록 설치되는 틸팅브라켓(3), 상기 틸팅브라켓(3)의 회전축(B)을 중심으로 회전하는 타이밍풀리(7)와, 상기 타이밍풀리(7)에 고정되어 연동 회전하는 링크(5) 및 고정브라켓(1)에 고정되어 상기 링크(5)에 연결되어 관절 형식으로 꺽여지면서 연동되어 틸팅브라켓(3)을 90도 각도로 접히도록하는 링크(8)를 구성하고, 상기 틸팅브라켓에 서보 모터(9)를 고정하여 이에 타이밍풀리(4)를 연결하여 타이밍벨트(6)를 타이밍풀리(4)(7)에 착설하여 회전력을 전달하도록 한 무인항공기 카메라 폴딩장치에 있어서, 상기한 링크(5)(8) 기구는 고정브라켓(1)의 회전축(D)과 타이밍풀리(4)의 회전축(B)에 회전자재케 축설되어 회전축(C)으로 연결되어 카메라 자중에 의한 수직방향으로의 외력발생시 회전축(C)과 회전축(D)의 중심점을 연결한 선 위쪽의 회전축(B)이 위치하여 카메라 중심의 수직방향(F방향)으로 모멘트가 발생하여 자동적으로 링크가 락이 되도록 구성한 것을 특징으로 하는 무인항공기 카메라 폴딩장치.Fixing bracket (1) fixed to the aircraft fuselage, the tilting bracket (3) installed so as to be rotatable about the left and right side rotating shaft (A) of the fixing bracket (1), the rotating shaft (B) of the tilting bracket (3) It is fixed to the timing pulley (7) rotated to the center, and the link (5) and the fixed bracket (1) which is fixed to the timing pulley (7) and interlocked rotation is connected to the link (5) and bent in a joint form Link (8) is configured to fold the tilting bracket (3) by 90 degrees in conjunction with, and the servo motor (9) is fixed to the tilting bracket to connect the timing pulley (4) to the timing belt (6) In the unmanned aerial vehicle camera folding apparatus mounted on the timing pulleys (4) and (7) to transmit rotational force, the above-described link (5) mechanism (8) has a rotation shaft (D) and a timing pulley (4) of the fixing bracket (1). Rotational material is built up on the rotation axis (B) of) and connected to the rotation axis (C) Rotation axis (B) above the line connecting the rotation axis (C) and the center point of the rotation axis (D) when the external force is generated in the direction is positioned so that the moment occurs in the vertical direction (F direction) of the camera center, the link is automatically locked Unmanned aerial vehicle camera folding apparatus, characterized in that. 삭제delete 제 1항에 있어서, 상기 링크기구는 고정브라켓에 고정된 링크(8)가 타이밍풀리에 고정된 링크(5) 안쪽으로 매립되는 상태로 작동하여 접히거나 펴질때 링크 안쪽에서 자동적으로 락이 걸리게 되도록 구성한 것을 특징으로 하는 무인항공기 카메라 폴딩장치
2. The link mechanism according to claim 1, wherein the link mechanism is configured to operate in a state in which the link 8 fixed to the fixing bracket is embedded in the link 5 fixed to the timing pulley so that the link is automatically locked inside the link when folded or unfolded. Unmanned aerial vehicle camera folding device, characterized in that
KR1020110109602A 2011-10-25 2011-10-25 Camera Polding system KR101302442B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1020110109602A KR101302442B1 (en) 2011-10-25 2011-10-25 Camera Polding system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020110109602A KR101302442B1 (en) 2011-10-25 2011-10-25 Camera Polding system

Publications (2)

Publication Number Publication Date
KR20130045122A KR20130045122A (en) 2013-05-03
KR101302442B1 true KR101302442B1 (en) 2013-09-02

Family

ID=48657382

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020110109602A KR101302442B1 (en) 2011-10-25 2011-10-25 Camera Polding system

Country Status (1)

Country Link
KR (1) KR101302442B1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104085537A (en) * 2014-06-27 2014-10-08 嘉兴安行信息科技有限公司 Remote sensing unmanned aerial vehicle frame
KR101689197B1 (en) 2016-06-20 2016-12-23 주식회사 엠지아이티 Gimbal assembly for drone
KR20170142414A (en) * 2016-06-17 2017-12-28 (주)충청에스엔지 기술사사무소 Camera protecting device for unmanned aerial vehicle
KR102443071B1 (en) 2021-10-20 2022-09-13 주식회사 아고스 Drone With Broadcast Camera
KR102672046B1 (en) 2024-02-15 2024-06-04 (주)웨이버스 Aerial photography system linked to GPS

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015100038A1 (en) * 2015-01-05 2016-07-07 Huf Hülsbeck & Fürst Gmbh & Co. Kg Image acquisition system with flexible transfer element
CN105083577A (en) * 2015-08-05 2015-11-25 北京韦加航通科技有限责任公司 Holder steering lifting system for narrow load cabin of unmanned aerial vehicle and unmanned aerial vehicle
CN106019799B (en) * 2016-07-26 2018-11-13 广州市红鹏直升机遥感科技有限公司 A kind of double-axle rotation inclined camera
CN109969420B (en) * 2017-12-28 2024-02-09 昆山合朗航空科技有限公司 Steering engine driven folding cradle head
CN207773518U (en) * 2018-01-05 2018-08-28 深圳市大疆创新科技有限公司 CCD camera assembly and unmanned plane
CN109159905A (en) * 2018-10-31 2019-01-08 上海歌尔泰克机器人有限公司 A kind of holder and the unmanned plane with the holder

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06166399A (en) * 1992-12-02 1994-06-14 Shin Meiwa Ind Co Ltd Retractable device for aerial photographing camera for airplane
KR100823346B1 (en) * 2007-03-16 2008-04-18 (주)엔에스에이치 Pilotless helicopter for filming

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06166399A (en) * 1992-12-02 1994-06-14 Shin Meiwa Ind Co Ltd Retractable device for aerial photographing camera for airplane
KR100823346B1 (en) * 2007-03-16 2008-04-18 (주)엔에스에이치 Pilotless helicopter for filming

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104085537A (en) * 2014-06-27 2014-10-08 嘉兴安行信息科技有限公司 Remote sensing unmanned aerial vehicle frame
KR20170142414A (en) * 2016-06-17 2017-12-28 (주)충청에스엔지 기술사사무소 Camera protecting device for unmanned aerial vehicle
KR102310731B1 (en) 2016-06-17 2021-10-15 (주)충청에스엔지 기술사사무소 Camera protecting device for unmanned aerial vehicle
KR101689197B1 (en) 2016-06-20 2016-12-23 주식회사 엠지아이티 Gimbal assembly for drone
KR102443071B1 (en) 2021-10-20 2022-09-13 주식회사 아고스 Drone With Broadcast Camera
KR102672046B1 (en) 2024-02-15 2024-06-04 (주)웨이버스 Aerial photography system linked to GPS

Also Published As

Publication number Publication date
KR20130045122A (en) 2013-05-03

Similar Documents

Publication Publication Date Title
KR101302442B1 (en) Camera Polding system
CN205989812U (en) Many rotor wing unmanned aerial vehicles
US11542000B2 (en) Flight control for an unmanned aerial vehicle
US20170247098A1 (en) Drone with folding linking arms
US20170247106A1 (en) Drone provided with foldable drone supports
KR101456035B1 (en) The rotor arm device of multi-rotor type drone
JP3217820U (en) Drone
JP6473244B1 (en) Rotorcraft
EP3400171B1 (en) Multirotor aircraft
EP3345831B1 (en) Drone capable of varying propeller arrangement shape
WO2019129304A1 (en) Undercarriage and unmanned aerial vehicle having same
KR101654544B1 (en) A unmanned aircraft having landing and retention capabilities
WO2019128446A1 (en) Undercarriage and unmanned aerial vehicle having same
KR101823782B1 (en) Ball Type Drone
WO2019024541A1 (en) Arm and unmanned aerial vehicle
WO2018095214A1 (en) Unmanned aerial vehicle and landing gear device thereof
JP6332706B2 (en) Aerial wing aircraft
EP3564119B1 (en) Multi-rotor unmanned aerial vehicle
CN211918999U (en) Unmanned vehicles and image device
WO2018095238A1 (en) Unmanned aerial vehicle and undercarriage device thereof
CN109383775A (en) The dedicated photographic device of unmanned plane
WO2019137078A1 (en) Unmanned aerial vehicle
CN113525671A (en) Undercarriage and unmanned aerial vehicle
KR102134174B1 (en) Unmanned flying device and portable terminal using the same
CN112543734A (en) Unmanned aerial vehicle and operation method thereof, imaging device and operation method thereof

Legal Events

Date Code Title Description
A201 Request for examination
E902 Notification of reason for refusal
E701 Decision to grant or registration of patent right
GRNT Written decision to grant
FPAY Annual fee payment

Payment date: 20160620

Year of fee payment: 4

FPAY Annual fee payment

Payment date: 20170619

Year of fee payment: 5

FPAY Annual fee payment

Payment date: 20180927

Year of fee payment: 6

FPAY Annual fee payment

Payment date: 20190611

Year of fee payment: 7