WO2017069320A1 - Free-fall type aerial photographing device using free rotation of helicopter - Google Patents

Free-fall type aerial photographing device using free rotation of helicopter Download PDF

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Publication number
WO2017069320A1
WO2017069320A1 PCT/KR2015/012050 KR2015012050W WO2017069320A1 WO 2017069320 A1 WO2017069320 A1 WO 2017069320A1 KR 2015012050 W KR2015012050 W KR 2015012050W WO 2017069320 A1 WO2017069320 A1 WO 2017069320A1
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WIPO (PCT)
Prior art keywords
blade
body portion
aerial
ring
air
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Application number
PCT/KR2015/012050
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French (fr)
Korean (ko)
Inventor
배효길
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한국항공우주연구원
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Publication of WO2017069320A1 publication Critical patent/WO2017069320A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/28Collapsible or foldable blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • B64C27/50Blades foldable to facilitate stowage of aircraft

Definitions

  • the present invention relates to an aerial photographing apparatus, and more particularly, such as a helicopter's free-rotating method, descending from the air and lifting freely in the air at low speed in the air with the lifting force of a blade rotating by air flowing from the bottom, the ground object,
  • the present invention relates to a free-fall aerial photographing apparatus using free rotation of a helicopter for photographing facilities and terrain.
  • the present invention was created in order to solve the above problems, the object of the present invention is to simplify the accessories of the equipment can be easily taken without a separate training training and helicopters that can be used for the purpose of aerial photography in a limited range at low altitude An object of the present invention is to provide a free fall aerial photographing apparatus using free rotation.
  • a free-fall aerial photographing apparatus using a free rotation of the helicopter according to the present invention for achieving the above object has a streamlined appearance and the upper portion of the rotating shaft 111 is arranged upright body 110; A head portion 120 coupled to the rotation shaft 111 and rotatably mounted independently of the body portion 110; Blades 130 that are spaced apart at regular intervals along the circumference of the head portion 120 is mounted foldable and rotates with the head portion 120 to generate a lift; And a camera 140 disposed under the body part 110 to drive the camera 140 in a downward direction or a lateral direction.
  • the blade groove 112 extending from the upper portion to the lower portion is formed around the body portion 110, and the blade 130 is foldably mounted to the head portion 120 through the hinge portion 133.
  • the blade groove 112 may be inserted into the blade groove 112 to be in close contact with the body 110 or open to be horizontally opened.
  • the blade groove 112 is in a twisted form along the circumference of the body portion 110 so that the body portion 110 rotates in a direction opposite to the rotational direction of the blade 130 in the air flow according to the descending. Can be formed.
  • the plurality of cameras 140 may be disposed in each blade groove 112 to acquire a photographed image in a state in which the blade 130 is opened.
  • the top of the head portion 120 is equipped with a firing ring 121 is bent to form a portion of the firing means using the elastic, the body portion 110 on the outer surface of the body portion 110 Friction protrusion 113 may be formed to increase the friction between the skin of the user gripping the).
  • the blade 130 is foldably mounted around the head portion 120 through a hinge spring 133 of the hinge spring form, a ring-shaped fixing ring 131 is provided at the end of the blade 130 And, it is mounted to be pulled out of the lower portion of the body portion 110 and the lower end is placed upright to be exposed downward through the withdrawal hole 115 of the body portion 110, the fixing ring 131 is inserted into each blade 130 Take-out rod 151 for fixing a), an actuator 152 for providing a driving force necessary for the take-out rod 151 to take out, and a sensor unit 153 for detecting a fall of the body unit 110 launched into the air. And, if the falling through the sensor unit 153 is detected by driving the actuator 152 to drive the exposed lower end of the withdrawal rod 151 into the body portion 110, each blade 130 Automatic opening means 150 including a control unit 154 for automatically opening the; Can.
  • the blade 130 is foldably mounted to the head portion 120 through the hinge portion 133 of the hinge spring form, and is inserted through the inside of the body portion 110 inside the blade 130.
  • the engaging portion 132 is protruding
  • the support plate 161 is mounted so as to be liftable in the body portion 110 and supported by each engaging portion 132 to fix the folded state of the blade 130 and
  • the actuator 162 provides driving force necessary for the support plate 161 to move up and down, a sensor unit 163 for detecting a fall of the body unit 110 launched into the air, and the sensor unit 163.
  • An automatic opening means 160 including a control unit 164 for automatically opening each blade 130 while releasing the supported state of each locking unit 132 by controlling the driving of the actuator 162 when the falling is sensed; It may further include.
  • a space portion 116 is provided inside the body portion 110, and disposed in the space portion 116 and adjusting the position of the weight 176 according to a control signal in a falling direction of the body portion 110.
  • Direction control unit 170 for controlling the; may further include.
  • the direction control unit 170 the horizontal ring 171 is supported on the inside of the space portion 116 is arranged horizontally rollable around the x-axis, and extends in the y-axis direction the horizontal ring 171
  • a horizontal bar 172 horizontally disposed across the center of the horizontal axis and rolled about the y axis so that both ends are hinged to the horizontal ring 171, and extend in a z-axis direction to a center of the horizontal bar 172.
  • a vertical bar 173 having an upright position and having a weight 176 mounted thereon, a first driving part 174 that pushes or pulls an upper portion of the vertical bar 173 in the x-axis direction, and the horizontal bar 172.
  • it may include a second driving unit 175 to lift or pull one side of the horizontal ring 171 in the z-axis direction.
  • a launch means such as a rubber band or a spring
  • the aerial photography is performed while free-falling. This significantly reduces the manufacturing cost of the device and simplifies the preparation for shooting.
  • the blade 130 mounted on the upper portion of the body 110 after being launched into the air to fly by the lift generated by the rotation and free fall, it is possible to shoot a stable aerial image in a balanced state and to the user It is not necessary to maneuver in the air by the public, so it can be used easily by the general public without any professional maneuvering training.
  • the blade groove 112 extending from the top to the bottom is formed around the body portion 110, the blade 130 is folded or horizontally in close contact with the body portion 110 through the hinge portion 133 Since the air can be expanded and opened, the blade 130 can be fired up to a higher position with the same firing power by minimizing air resistance when the air is launched by the launch means, and the blade 130 is folded during free fall while descending. ) To generate lift for balance.
  • the blade groove 112 is formed in a twisted form along the circumference of the body portion 110 so that the body portion 110 rotates in the opposite direction to the rotation direction of the blade 130 in the air flow according to the falling,
  • the rotational force of the blade 130 to minimize the rotational force of the body portion 110 to be rotated together can take a still aerial image.
  • the camera 140 disposed under the body part 110 and driving in a downward direction or a lateral direction is disposed in each blade groove 112 to capture a captured image in a state where the blade 130 is opened. Therefore, it is possible to minimize damage of the camera 140 when landing and effectively prevent foreign substances such as dust or moisture from entering the lens of the camera 140 when carrying or storing.
  • an aerial image of a wider area may be obtained by dividing a photographing area of each camera 140.
  • the upper end of the head portion 120 is axially coupled to the upper portion of the body portion 110 is equipped with a firing ring 121 of the bent shape, the elastic ring, such as a rubber band or spring to the firing ring 121
  • the elastic ring such as a rubber band or spring
  • the locking portion 131 formed at the end of the blade 130 is inserted into the pull-out rod 151, which is arranged to be pulled upright in the lower portion of the body portion 110, or the engaging portion protruding in the blade 130 132 is supported on the support plate 161 which is placed up and down inside the body portion 110, so that each blade 130 can be launched in a fixed state in close contact with the body portion 110, and automatically Opening means (150, 160) when the falling of the aerial shooting device 100 is launched into the air is pulled in the withdrawal rod 151 into the interior of the body portion 110 or each engaging portion by the support plate 161 ( While operating to release the supported state of the 132, each blade 130 can be controlled to be automatically opened by the elastic force of the hinge portion 133 having a hinge spring form, so that the blade 130 does not open in the air and fall as it is. Effectively break the device It can be prevented.
  • the direction control unit 170 is disposed in the space portion of the body 110 to adjust the position of the weight 176 according to the control signal to control the falling direction of the body 110 in the air Launched aerial cameras can be directed to designated drop points or can be easily positioned in the air.
  • FIG. 1 is a perspective view and a bottom view showing the external configuration of the aerial shooting apparatus according to a preferred embodiment of the present invention
  • Figure 2 is a perspective view and a bottom view showing the principle of operation of free-falling while the aerial shooting device is flying while the blade is opened in accordance with a preferred embodiment of the present invention
  • Figure 3 is a partial cross-sectional side view and bottom view showing the configuration of the automatic opening means using the fixing ring and the pull-out rod according to an embodiment of the present invention
  • Figure 4 is a side cross-sectional view showing the configuration of the automatic opening means using the engaging portion and the support plate according to a preferred embodiment of the present invention
  • FIG. 5 is a schematic view and a perspective view showing the configuration of the direction control unit according to a preferred embodiment of the present invention.
  • the free-falling aerial photographing apparatus 100 using the free rotation of the helicopter is a shooting device that is launched into the air by the firing means free-falling and photographing objects, facilities and terrain of the ground, etc.
  • the body part 110, the head part 120, the blade 130, and the camera 140 are provided.
  • the body 110 is a member that forms a main body of the aerial photographing apparatus 100 and acts as a weight to allow the aerial photographing apparatus 100 to stand upright during free fall, and has a streamlined shape such as an egg shape. It has an external shape and is provided with a space portion 116 for mounting various components therein, and the rotary shaft 111 for mounting the head portion 120 is placed upright.
  • the body portion 110 has a streamlined appearance to minimize the air resistance when firing can be launched to a higher position with the same firing power.
  • the head part 120 is a member for rotating the blade 130 and is axially coupled to the rotation shaft 111 so as to be independently rotatable with respect to the body part 110.
  • the rotation shaft 111 is provided with a rotation support member for reducing the frictional force due to the relative rotational movement between the body 110 and the head 120, such as a ball bearing, the rotational force of the head portion 120 by the frictional force
  • a portion of the body portion 110 is preferably provided to be able to reduce the force to be rotated together while the body portion 110.
  • the upper surface of the head portion 120 is preferably formed in a rounded streamline as shown in the figure to minimize the friction with air during launch or rotation.
  • the blade 130 is a member that provides lifting force so that the aerial shooting apparatus 100 maintains a balance, and the air flows from the lower portion as it descends while being mounted at a predetermined interval along the circumference of the head part 120. By rotating with the head portion 120 to generate a lift.
  • the generated lift is used to increase the time that the aerial photographing apparatus 100 stays in the air and maintain the balance in the upright state of the body part 110, and the aerial photographing apparatus 100 is moved due to the tilt of the lifting axis. Used to steer.
  • the camera 140 is a photographing means for acquiring an aerial image.
  • the camera 140 is disposed under the body 110 and drives the camera 140 in a lower direction and a side direction.
  • the captured image is stored in a separate memory or transmitted to the ground by wireless communication.
  • the upper end of the head portion 120 is equipped with a firing ring 121 of a shape bent to hang a portion of the firing means using the elastic, the firing ring 121 is elastic, such as a rubber band or a spring It is possible to provide a launch means at low cost because it can be launched into the air by walking a part of the launch means using.
  • the friction protrusion 113 protrudes from the outer surface of the body part 110 to increase the frictional force with the user's skin holding the body part 110, it is aimed while sliding due to sweat or dry skin condition. Misalignment or misfire can be prevented beforehand, resulting in more accurate firing.
  • the firing means uses elasticity of an elastic member such as a rubber band or a compression spring, and fixes one side of the elastic member, such as a slingshot, to a separate support gripped by the user or the firing ring 121 on the other side of the elastic member.
  • an elastic member such as a rubber band or a compression spring
  • the aerial photographing apparatus 100 may be launched to a desired aerial position by using the force of the elastic restoring force of the elastic member by removing the pulling force.
  • a signal firing device used for military purposes such as a pistol-shaped muzzle is inserted into the air shooting device 100 and by pulling the trigger can be fired to the aerial position using the combustion power of gunpowder, flight It is also possible to drop the aerial shooting device 100 to the desired point in the aircraft in flight.
  • a blade groove 112 extending from the upper portion to the lower portion is formed around the body portion 110, and the blade 130 has a head portion through a hinge portion 133. 120 may be inserted into the blade groove 112 while being foldably attached to the blade groove 112 to be in close contact with the body portion 110 or to be horizontally opened.
  • the blade 130 when the air is launched by the launch means, the blade 130 can be folded to minimize the air resistance, so that it can be shot to a higher position with the same firing power, and when the free fall falls, the folded blade 130 is opened to balance. It can generate lift for.
  • the blade groove 112 is along the circumference of the body portion 110 so that the body portion 110 rotates in a direction opposite to the rotation direction of the blade 130 in the air flow according to the aerial shooting device 100 descends. It is preferably formed in a twisted form.
  • the blade groove 112 is formed in a twisted shape that rotates counterclockwise as it goes downward to the drawing reference, and is caused by the air flow generated while falling.
  • the body 110 is to rotate in a counterclockwise direction.
  • the blade groove 112 is formed in a twisted form along the circumference of the body portion 110 so that the body portion 110 rotates in a direction opposite to the rotational direction of the blade 130 in the air flow according to the falling
  • the camera 140 is disposed below the body portion 110, a plurality of are disposed in each blade groove 112 is preferably provided so as to obtain a photographed image in the open state of the blade 130. Do. Therefore, it is possible to minimize the damage of the camera 140 when landing and effectively prevent the inflow of foreign matter such as dust or moisture into the lens of the camera 140 when carrying or storing.
  • an aerial image of a wider area may be obtained by dividing a photographing area of each camera 140.
  • the blade 130 is mounted to the head portion 120 foldable through the hinge portion 133, by the automatic opening means 150, 160 shown in Figures 3 and 4 When firing, it may be provided to be in close contact with the body 110 and open automatically at the moment of descending from the highest point in the air.
  • the blade 130 is foldably mounted around the head portion 120 through a hinge portion 133 having a hinge spring shape, and a ring shape is fixed to an end portion of the blade 130. Ring 131 is provided.
  • the hinge portion 133 has an elastic force acting outward so that the blade 130 is opened.
  • the automatic opening means 150 is mounted to be pulled out to the lower portion of the body portion 110 and the lower end is disposed upright so as to be exposed downward through the withdrawal hole 115 of the body portion 110 and the fixing ring ( 131 is inserted into the take-out rod for fixing each blade 130, the actuator 152 for providing the driving force required for the take-out rod 151 withdrawal operation, and the lowering of the body portion 110 launched into the air
  • the sensor unit 153 detects the fall through the sensor unit 153 and drives the actuator 152, the exposed lower end of the lead-out rod 151 is drawn into the body 110.
  • It may be provided including a control unit 154 to automatically open each blade 130 while.
  • the automatic opening means 160 the support plate 161 is mounted so as to be elevated in the body portion 110 and supported by each engaging portion 132 to fix the folded state of the blade 130.
  • an actuator 162 providing driving force necessary for the support plate 161 to move up and down, a sensor unit 163 for detecting a fall of the body unit 110 launched into the air, and the sensor unit 163.
  • the control unit 162 may be provided with a control unit 164 for automatically opening each blade 130 while releasing the supported state of each engaging portion 132 by driving control.
  • each blade 130 can be launched in a fixed state in close contact with the body portion 110,
  • the automatic opening means (150, 160) is to detect the falling of the aerial shooting device 100 launched into the air to pull the withdrawal rod 151 into the interior of the body portion 110 or each engaging portion by the support plate 161 While operating to release the supported state of 132, each blade 130 can be controlled to be automatically opened by the elastic force of the hinge portion 133 having a hinge spring form, so that the blade 130 is not opened in the air. Falling as it is, effectively destroying the device Can be prevented.
  • the aerial shooting device 100 may be provided to adjust the drop position during free fall.
  • a space portion 116 is provided inside the body portion 110, and disposed in the space portion 116 and the weight of the weight 176 according to a control signal. It may further include a direction control unit 170 for adjusting the position to control the falling direction of the body portion 110.
  • the direction adjusting part 170 is supported on the inner side of the space part 116 so that the horizontal ring 171 is horizontally arranged to be rolled around the x-axis.
  • a horizontal bar 172 extending in the y-axis direction and horizontally disposed across the center of the horizontal ring 171 and having both ends hinged to the horizontal ring 171 so as to roll about the y axis;
  • a vertical bar 173 extending in an axial direction and disposed upright in the center of the horizontal bar 172 and having a weight 176 mounted thereon, and pushing or pulling an upper portion of the vertical bar 173 in the x-axis direction.
  • the first driving unit 174 and the horizontal bar 172 or the horizontal ring 171 includes a second driving unit 175 that lifts or pulls one side in the z-axis direction.
  • the driving unit of the direction control unit 170 through the control unit 154 by using a control means using a wireless communication disposed on the ground using the direction control unit 170 by moving the weight 176 to position
  • the unbiased load in body 110 allows tilting the lift axis to move to the desired aerial position.
  • the position of the inertial navigation sensor is stored without using the control means, and the position of the inertial navigation sensor is stored by the inertial navigation sensor. It can be operated to move.
  • a battery (not shown) for supplying driving power required to drive the aerial photographing apparatus 100 is built in the body 110, and the battery itself is used as the weight 176 or the weight 176.
  • the weight required to implement the weight function can be replaced with the weight of the battery, thereby miniaturizing the device.
  • the battery is not used for forcibly rotating the blade like the conventional drone, but used for providing a driving power source for communication and control, driving of the automatic opening means 150 and the direction control unit 170. Therefore, a small battery that can be mounted in the body 110 is used.
  • the aerial shooting is carried out by free-falling by being released into the air by means of launching means such as rubber bands or springs, Since drones do not require motors, batteries, or complex control systems to forcibly rotate the blades, they simplify the equipment's accessories, greatly reducing the manufacturing cost of the device, and simplifying preparation for shooting.
  • launching means such as rubber bands or springs
  • the blade 130 mounted on the upper portion of the body 110 after being launched into the air to fly by the lift generated by the rotation and free fall, it can take a stable aerial image while maintaining a balanced state to the user It is not necessary to maneuver in the air by the public, so it can be used easily by the general public without any professional maneuvering training.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Accessories Of Cameras (AREA)

Abstract

According to the present invention, disclosed is an aerial photographing device comprising: a body part (110) having a streamlined appearance and having a rotation shaft (111) arranged upright on an upper part thereof; a head part (120) axially coupled to the rotation shaft (111) so as to be rotatably provided independently of the body part (110); blades (130) foldably mounted to be spaced from each other at predetermined intervals along the circumference of the head part (120), and generating lift while rotating together with the head part (120); and a camera (140) arranged at a lower part of the body part (110) and driven to photograph while being directed downward or sideways.

Description

헬리콥터의 자유회전을 이용한 자유낙하 방식의 공중촬영장치Free-falling aerial photographing device using free rotation of helicopter
본 발명은 공중촬영장치에 관한 것으로, 보다 상세하게는 헬리콥터의 자유회전 방식과 같이 공중에서 하강하며 하부에서 유입되는 공기흐름에 의해 회전하는 블레이드의 양력으로 공중에서 저속으로 자유낙하하면서 지상의 물체, 시설 및 지형 등을 촬영하기 위한 헬리콥터의 자유회전을 이용한 자유낙하 방식의 공중촬영장치에 관한 것이다.The present invention relates to an aerial photographing apparatus, and more particularly, such as a helicopter's free-rotating method, descending from the air and lifting freely in the air at low speed in the air with the lifting force of a blade rotating by air flowing from the bottom, the ground object, The present invention relates to a free-fall aerial photographing apparatus using free rotation of a helicopter for photographing facilities and terrain.
최근 군사용도로 개발된 드론(멀티콥터)에 카메라를 탑재하여 공중촬영하는 방식이 레저용이나 방송용으로 대중화되어 널리 이용되고 있다.Recently, a drone (multi-copter) that was developed for military use with a camera mounted in the air shooting method is widely used for leisure and broadcasting.
그러나, 드론을 이용한 공중촬영은 고가의 비행체와 조종장비, 통신장비 및 다량의 배터리 등의 부속품 일체를 구비하여야 하며, 자유롭게 드론을 조종하기 위해서는 전문적인 조종훈련이 필요하며 숙달까지 상당기간 훈련시간이 필요하기 때문에, 촬영을 위한 준비단계가 매우 번거로워 일반인이 쉽게 이용하기가 제한되었다.However, aerial photography using drones should be equipped with all kinds of accessories such as expensive aircraft, control equipment, communication equipment, and a large amount of batteries. Because of the necessity, the preparation for the shooting was very cumbersome and the general public was not easily used.
또한, 드론을 고고도로 상승시키거나 드론을 멀리 직선 이동시키면서 광역범위를 촬영하지 않을 경우에는 굳이 기동성이 구비된 고가의 장비를 이용할 필요가 없다. 이에 장비의 부속품이 간소하면서도 저고도에서 한정된 범위를 공중촬영할 수 있는 저가의 촬영장치의 개발이 대두되고 있는 실정이다.In addition, it is not necessary to use expensive equipment equipped with maneuverability when not raising the drone at high altitude or moving the drone linearly while not photographing a wide range. Therefore, the development of low-cost imaging device capable of taking a limited range of aerial photography at a low altitude while simplifying the accessories of the equipment is on the rise.
(선행기술 문헌)(Prior art literature)
(특허문헌)(Patent literature)
일본공개특허공보 제2015-10911호(2015.1.19), 공중촬영 측량 방법 및 장치Japanese Laid-Open Patent Publication No. 2015-10911 (2015.1.19), aerial photography surveying method and apparatus
본 발명은 상술한 문제점을 해결하기 위하여 창출된 것으로, 본 발명의 목적은 장비의 부속품이 간소하고 별도의 조종훈련없이도 쉽게 촬영할 수 있으며 저고도에서 한정된 범위를 공중촬영하기 위한 용도로 이용할 수 있는 헬리콥터의 자유회전을 이용한 자유낙하 방식의 공중촬영장치를 제공하는 것에 있다.The present invention was created in order to solve the above problems, the object of the present invention is to simplify the accessories of the equipment can be easily taken without a separate training training and helicopters that can be used for the purpose of aerial photography in a limited range at low altitude An object of the present invention is to provide a free fall aerial photographing apparatus using free rotation.
상기의 목적을 달성하기 위한 본 발명에 따른 헬리콥터의 자유회전을 이용한 자유낙하 방식의 공중촬영장치는, 유선형의 외형을 가지며 상부에는 회전축(111)이 직립배치된 바디부(110); 상기 회전축(111)에 축결합되어 상기 바디부(110)에 대하여 독립적으로 회전가능하게 장착되는 헤드부(120); 상기 헤드부(120)의 둘레를 따라 일정간격 이격되어 접철가능하게 장착되고 헤드부(120)와 함께 회전하며 양력을 생성하는 블레이드(130); 및 상기 바디부(110)의 하부에 배치되어 하부방향 또는 측부방향을 지향하여 촬영구동하는 카메라(140);를 포함한다.A free-fall aerial photographing apparatus using a free rotation of the helicopter according to the present invention for achieving the above object, has a streamlined appearance and the upper portion of the rotating shaft 111 is arranged upright body 110; A head portion 120 coupled to the rotation shaft 111 and rotatably mounted independently of the body portion 110; Blades 130 that are spaced apart at regular intervals along the circumference of the head portion 120 is mounted foldable and rotates with the head portion 120 to generate a lift; And a camera 140 disposed under the body part 110 to drive the camera 140 in a downward direction or a lateral direction.
여기서, 상기 바디부(110)의 둘레에는 상부에서 하부를 향해 연장형성된 블레이드홈(112)이 형성되고, 상기 블레이드(130)는 힌지부(133)를 통해 헤드부(120)에 접철되게 장착되면서 상기 블레이드홈(112)에 삽입되어 바디부(110)에 밀착되거나 수평하게 펼쳐져 개방되도록 동작할 수 있다.Here, the blade groove 112 extending from the upper portion to the lower portion is formed around the body portion 110, and the blade 130 is foldably mounted to the head portion 120 through the hinge portion 133. The blade groove 112 may be inserted into the blade groove 112 to be in close contact with the body 110 or open to be horizontally opened.
또한, 상기 블레이드홈(112)은 하강에 따른 공기흐름으로 상기 바디부(110)가 상기 블레이드(130)의 회전방향과 반대방향으로 회전하도록 상기 바디부(110)의 둘레를 따라 트위스트된 형태로 형성될 수 있다.In addition, the blade groove 112 is in a twisted form along the circumference of the body portion 110 so that the body portion 110 rotates in a direction opposite to the rotational direction of the blade 130 in the air flow according to the descending. Can be formed.
또한, 복수의 카메라(140)는 각 블레이드홈(112) 내에 배치되어 상기 블레이드(130)가 개방된 상태에서 촬영이미지를 획득할 수 있다.In addition, the plurality of cameras 140 may be disposed in each blade groove 112 to acquire a photographed image in a state in which the blade 130 is opened.
또한, 상기 헤드부(120)의 상단에는 탄성을 이용한 발사수단의 일부를 걸 수 있도록 절곡형성된 형상의 발사용고리(121)가 장착되며, 상기 바디부(110)의 외부면에는 바디부(110)를 파지한 사용자의 피부간에 마찰력을 증대시키기 위한 마찰돌기(113)가 돌출형성될 수 있다.In addition, the top of the head portion 120 is equipped with a firing ring 121 is bent to form a portion of the firing means using the elastic, the body portion 110 on the outer surface of the body portion 110 Friction protrusion 113 may be formed to increase the friction between the skin of the user gripping the).
또한, 상기 블레이드(130)는 힌지스프링 형태의 힌지부(133)를 통해 헤드부(120)의 둘레에 접철되게 장착되고, 상기 블레이드(130)의 단부에는 링형상의 고정링(131)이 마련되며, 상기 바디부(110)의 하부에 인출가능하게 장착되며 하단이 바디부(110)의 인출공(115)을 통해 하향 노출되게 직립배치되어 상기 고정링(131)이 삽입되면서 각 블레이드(130)를 고정시키는 인출로드(151)와, 상기 인출로드(151)가 인출동작하는데 필요한 구동력을 제공하는 액추에이터(152)와, 공중으로 발사된 바디부(110)의 하강을 감지하는 센서부(153) 및, 상기 센서부(153)를 통해 하강이 감지되면 상기 액추에이터(152)를 구동제어하여 상기 인출로드(151)의 노출된 하단을 바디부(110)의 내부로 인입시키면서 각 블레이드(130)를 자동개방시키는 제어부(154)를 포함하는 자동개방수단(150);을 더 포함할 수 있다.In addition, the blade 130 is foldably mounted around the head portion 120 through a hinge spring 133 of the hinge spring form, a ring-shaped fixing ring 131 is provided at the end of the blade 130 And, it is mounted to be pulled out of the lower portion of the body portion 110 and the lower end is placed upright to be exposed downward through the withdrawal hole 115 of the body portion 110, the fixing ring 131 is inserted into each blade 130 Take-out rod 151 for fixing a), an actuator 152 for providing a driving force necessary for the take-out rod 151 to take out, and a sensor unit 153 for detecting a fall of the body unit 110 launched into the air. And, if the falling through the sensor unit 153 is detected by driving the actuator 152 to drive the exposed lower end of the withdrawal rod 151 into the body portion 110, each blade 130 Automatic opening means 150 including a control unit 154 for automatically opening the; Can.
또한, 상기 블레이드(130)는 힌지스프링 형태의 힌지부(133)를 통해 헤드부(120)에 접철되게 장착되고, 상기 블레이드(130)의 내측에는 상기 바디부(110)의 내부에 관통삽입되는 걸림부(132)가 돌출형성되며, 상기 바디부(110) 내에서 승강가능하게 장착되며 각 걸림부(132)에 지지되어 상기 블레이드(130)의 접철된 상태를 고정시키는 지지플레이트(161)와, 상기 지지플레이트(161)가 승강동작하는데 필요한 구동력을 제공하는 액추에이터(162)와, 공중으로 발사된 바디부(110)의 하강을 감지하는 센서부(163) 및, 상기 센서부(163)를 통해 하강이 감지되면 상기 액추에이터(162)를 구동제어하여 각 걸림부(132)의 지지된 상태를 해제시키면서 각 블레이드(130)를 자동개방시키는 제어부(164)를 포함하는 자동개방수단(160);을 더 포함할 수 있다.In addition, the blade 130 is foldably mounted to the head portion 120 through the hinge portion 133 of the hinge spring form, and is inserted through the inside of the body portion 110 inside the blade 130. The engaging portion 132 is protruding, the support plate 161 is mounted so as to be liftable in the body portion 110 and supported by each engaging portion 132 to fix the folded state of the blade 130 and The actuator 162 provides driving force necessary for the support plate 161 to move up and down, a sensor unit 163 for detecting a fall of the body unit 110 launched into the air, and the sensor unit 163. An automatic opening means 160 including a control unit 164 for automatically opening each blade 130 while releasing the supported state of each locking unit 132 by controlling the driving of the actuator 162 when the falling is sensed; It may further include.
또한, 상기 바디부(110)의 내부에는 공간부(116)가 마련되고, 상기 공간부(116) 내에 배치되며 제어신호에 따라 웨이트(176)의 위치를 조절하여 바디부(110)의 낙하방향을 제어하는 방향조절부(170);를 더 포함할 수 있다.In addition, a space portion 116 is provided inside the body portion 110, and disposed in the space portion 116 and adjusting the position of the weight 176 according to a control signal in a falling direction of the body portion 110. Direction control unit 170 for controlling the; may further include.
한편, 상기 방향조절부(170)는, 상기 공간부(116)의 내측에 지지되어 x축을 중심으로 롤링 가능하게 수평배치된 수평고리(171)와, y축 방향으로 연장되어 상기 수평고리(171)의 중앙을 가로 질러 수평배치되며 y축을 중심으로 롤링 가능하게 양단이 상기 수평고리(171)에 힌지결합되는 수평바(172)와, z축 방향으로 연장되어 상기 수평바(172)의 중앙에 직립배치되며 하단에는 웨이트(176)가 장착된 수직바(173)와, 상기 수직바(173)의 상부를 x축 방향으로 밀거나 잡아당기는 제1구동부(174) 및, 상기 수평바(172) 또는 수평고리(171)의 일측을 z축 방향으로 일거나 잡아당기는 제2구동부(175)를 포함할 수 있다.On the other hand, the direction control unit 170, the horizontal ring 171 is supported on the inside of the space portion 116 is arranged horizontally rollable around the x-axis, and extends in the y-axis direction the horizontal ring 171 A horizontal bar 172 horizontally disposed across the center of the horizontal axis and rolled about the y axis so that both ends are hinged to the horizontal ring 171, and extend in a z-axis direction to a center of the horizontal bar 172. A vertical bar 173 having an upright position and having a weight 176 mounted thereon, a first driving part 174 that pushes or pulls an upper portion of the vertical bar 173 in the x-axis direction, and the horizontal bar 172. Or it may include a second driving unit 175 to lift or pull one side of the horizontal ring 171 in the z-axis direction.
본 발명에 따른 헬리콥터의 자유회전을 이용한 자유낙하 방식의 공중촬영장치에 의하면,According to the free-falling aerial photography apparatus using the free rotation of the helicopter according to the present invention,
첫째, 고무줄이나 용수철 등의 발사수단에 의해 공중으로 발사되어 자유낙하하면서 공중촬영이 이루어지면서 종래의 드론과 같이 블레이드를 강제회전시키기 위한 모터, 배터리, 복잡한 조종시스템 등이 불필요하므로 장비의 부속품을 간소화하여 장치의 제조비용을 대폭 절감할 수 있으며 촬영을 위한 준비단계를 간소화할 수 있다.First, it is launched into the air by a launch means such as a rubber band or a spring, and the aerial photography is performed while free-falling. This significantly reduces the manufacturing cost of the device and simplifies the preparation for shooting.
둘째, 공중으로 발사된 후 바디부(110)의 상부에 장착된 블레이드(130)가 회전하면서 생성된 양력에 의해 비행하며 자유낙하하기 때문에 균형을 유지한 상태로 안정적인 공중영상을 촬영할 수 있으며 사용자에 의한 공중에서의 조종이 불필요하므로 전문적인 조종훈련없이도 일반인이 쉽게 이용할 수 있다.Second, since the blade 130 mounted on the upper portion of the body 110 after being launched into the air to fly by the lift generated by the rotation and free fall, it is possible to shoot a stable aerial image in a balanced state and to the user It is not necessary to maneuver in the air by the public, so it can be used easily by the general public without any professional maneuvering training.
셋째, 상기 바디부(110)의 둘레에는 상부에서 하부로 연장된 블레이드홈(112)이 형성되고, 상기 블레이드(130)는 힌지부(133)를 통해 바디부(110)에 밀착되도록 접거나 수평하게 펼쳐져 개방시킬 수 있으므로, 발사수단에 의한 공중 발사시에는 블레이드(130)를 접어 공기저항을 최소화함으로써 동일한 발사동력으로 보다 높은 위치까지 발사시킬 수 있으며, 하강하면서 자유낙하시에는 접어진 블레이드(130)를 개방시켜 균형을 위한 양력을 생성시킬 수 있다.Third, the blade groove 112 extending from the top to the bottom is formed around the body portion 110, the blade 130 is folded or horizontally in close contact with the body portion 110 through the hinge portion 133 Since the air can be expanded and opened, the blade 130 can be fired up to a higher position with the same firing power by minimizing air resistance when the air is launched by the launch means, and the blade 130 is folded during free fall while descending. ) To generate lift for balance.
넷째, 상기 블레이드홈(112)은 하강에 따른 공기흐름으로 바디부(110)가 블레이드(130)의 회전방향과 반대방향으로 회전하도록 바디부(110)의 둘레를 따라 트위스트된 형태로 형성되므로, 상기 블레이드(130)의 회전력에 의해 함께 회전하려는 바디부(110)의 회전력을 최소화하여 정지된 공중영상을 촬영할 수 있다.Fourth, the blade groove 112 is formed in a twisted form along the circumference of the body portion 110 so that the body portion 110 rotates in the opposite direction to the rotation direction of the blade 130 in the air flow according to the falling, By the rotational force of the blade 130 to minimize the rotational force of the body portion 110 to be rotated together can take a still aerial image.
다섯째, 상기 바디부(110)의 하부에 배치되어 하부방향 또는 측부방향을 지향하면서 촬영구동하는 카메라(140)는 각 블레이드홈(112) 내에 배치되어 블레이드(130)가 개방된 상태에서 촬영이미지를 획득하므로 착지시 카메라(140)의 파손을 최소화하고 휴대나 보관시 카메라(140)의 렌즈에 먼지나 수분 등의 이물질이 유입되는 것을 효과적으로 방지할 수 있다. 또한, 복수의 카메라(140)를 각 블레이드홈(112)별로 배치함으로써 각 카메라(140)의 촬영영역을 분할하여 보다 넓은 영역의 공중영상을 획득할 수 있다.Fifth, the camera 140 disposed under the body part 110 and driving in a downward direction or a lateral direction is disposed in each blade groove 112 to capture a captured image in a state where the blade 130 is opened. Therefore, it is possible to minimize damage of the camera 140 when landing and effectively prevent foreign substances such as dust or moisture from entering the lens of the camera 140 when carrying or storing. In addition, by arranging the plurality of cameras 140 for each blade groove 112, an aerial image of a wider area may be obtained by dividing a photographing area of each camera 140.
여섯째, 상기 바디부(110)의 상부에 축결합된 헤드부(120)의 상단에는 절곡형성된 형상의 발사용고리(121)가 장착되어, 이 발사용고리(121)에 고무줄이나 용수철 등과 같이 탄성을 이용한 발사수단의 일부를 걸어 공중으로 발사시킬 수 있으므로 저가의 비용으로 발사수단을 마련할 수 있다. 또한, 상기 바디부(110)의 외부면에는 마찰돌기(113)가 돌출형성되어 바디부(110)를 파지한 사용자 피부와의 마찰력을 증대시킬 수 있으므로, 땀이나 건조한 피부 상태로 인해 미끄러지면서 조준방향이 어긋나거나 오발되는 것을 미연에 방지할 수 있어 보다 정확한 발사작업이 이루어질 수 있다.Sixth, the upper end of the head portion 120 is axially coupled to the upper portion of the body portion 110 is equipped with a firing ring 121 of the bent shape, the elastic ring, such as a rubber band or spring to the firing ring 121 It is possible to provide a launch means at low cost because it can be launched into the air by walking a part of the launch means using. In addition, since the friction protrusion 113 protrudes from the outer surface of the body part 110 to increase the frictional force with the user's skin holding the body part 110, it is aimed while sliding due to sweat or dry skin condition. Misalignment or misfire can be prevented beforehand, resulting in more accurate firing.
일곱째, 상기 블레이드(130)의 단부에 형성된 고정링(131)을 바디부(110)의 하부에 인출가능하게 직립배치된 인출로드(151)에 삽입하거나 블레이드(130)의 내측에 돌출형성된 걸림부(132)를 바디부(110)의 내부에 승강가능하게 배치된 지지플레이트(161)에 지지시켜, 각 블레이드(130)가 바디부(110)에 밀착되게 고정된 상태로 발사시킬 수 있으며, 자동개방수단(150,160)은 공중으로 발사된 공중촬영장치(100)의 하강이 감지되면 상기 인출로드(151)를 바디부(110)의 내부로 인입시키거나 지지플레이트(161)에 의한 각 걸림부(132)의 지지된 상태를 해제하도록 동작되면서, 각 블레이드(130)가 힌지스프링 형태를 갖는 힌지부(133)의 탄성력으로 자동개방되도록 제어할 수 있으므로 공중에서 블레이드(130)가 개방되지 않아 그대로 추락하면서 장치가 파손되는 현상을 효과적으로 방지할 수 있다.Seventh, the locking portion 131 formed at the end of the blade 130 is inserted into the pull-out rod 151, which is arranged to be pulled upright in the lower portion of the body portion 110, or the engaging portion protruding in the blade 130 132 is supported on the support plate 161 which is placed up and down inside the body portion 110, so that each blade 130 can be launched in a fixed state in close contact with the body portion 110, and automatically Opening means (150, 160) when the falling of the aerial shooting device 100 is launched into the air is pulled in the withdrawal rod 151 into the interior of the body portion 110 or each engaging portion by the support plate 161 ( While operating to release the supported state of the 132, each blade 130 can be controlled to be automatically opened by the elastic force of the hinge portion 133 having a hinge spring form, so that the blade 130 does not open in the air and fall as it is. Effectively break the device It can be prevented.
여덟째, 상기 바디부(110)의 공간부 내에는 방향조절부(170)가 배치되어 제어신호에 따라 웨이트(176)의 위치를 조절하여 바디부(110)의 낙하방향을 제어할 수 있으므로 공중에 발사된 공중촬영장치를 지정된 낙하지점으로 유도하거나 공중에서의 위치를 용이하게 조절할 수 있다.Eighth, the direction control unit 170 is disposed in the space portion of the body 110 to adjust the position of the weight 176 according to the control signal to control the falling direction of the body 110 in the air Launched aerial cameras can be directed to designated drop points or can be easily positioned in the air.
도 1은 본 발명의 바람직한 실시예에 따른 공중촬영장치의 외부 구성을 나타낸 사시도 및 저면도,1 is a perspective view and a bottom view showing the external configuration of the aerial shooting apparatus according to a preferred embodiment of the present invention,
도 2는 본 발명의 바람직한 실시예에 따른 블레이드가 개방되면서 공중촬영장치가 비행하면서 자유낙하는 동작원리를 나타낸 사시도 및 저면도,Figure 2 is a perspective view and a bottom view showing the principle of operation of free-falling while the aerial shooting device is flying while the blade is opened in accordance with a preferred embodiment of the present invention,
도 3은 본 발명의 바람직한 실시예에 따른 고정링과 인출로드를 이용한 자동개방수단의 구성을 나타낸 부분단면 측면도 및 저면도,Figure 3 is a partial cross-sectional side view and bottom view showing the configuration of the automatic opening means using the fixing ring and the pull-out rod according to an embodiment of the present invention,
도 4는 본 발명의 바람직한 실시예에 따른 걸림부와 지지플레이트를 이용한 자동개방수단의 구성을 나타낸 측단면도,Figure 4 is a side cross-sectional view showing the configuration of the automatic opening means using the engaging portion and the support plate according to a preferred embodiment of the present invention,
도 5는 본 발명의 바람직한 실시예에 따른 방향조절부의 구성을 나타낸 개략도 및 사시도이다.5 is a schematic view and a perspective view showing the configuration of the direction control unit according to a preferred embodiment of the present invention.
이하 첨부된 도면을 참조하면서 본 발명에 따른 바람직한 실시예를 상세히 설명하기로 한다. 이에 앞서, 본 명세서 및 청구범위에 사용된 용어나 단어는 통상적이거나 사전적인 의미로 한정해서 해석되어서는 아니 되며, 발명자는 그 자신의 발명을 가장 최선의 방법으로 설명하기 위해 용어의 개념을 적절하게 정의할 수 있다는 원칙에 입각하여, 본 발명의 기술적 사상에 부합하는 의미와 개념으로 해석되어야만 한다.Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings. Prior to this, terms or words used in the present specification and claims should not be construed as being limited to the common or dictionary meanings, and the inventors should properly explain the concept of terms in order to best explain their own invention. Based on the principle that it can be defined, it should be interpreted as meaning and concept corresponding to the technical idea of the present invention.
따라서, 본 명세서에 기재된 실시예와 도면에 도시된 구성은 본 발명의 가장 바람직한 일 실시예에 불과할 뿐이고 본 발명의 기술적 사상을 모두 대변하는 것은 아니므로, 본 출원시점에 있어서 이들을 대체할 수 있는 다양한 균등물과 변형예들이 있을 수 있음을 이해하여야 한다.Therefore, the embodiments described in the specification and the drawings shown in the drawings are only the most preferred embodiment of the present invention and do not represent all of the technical idea of the present invention, various modifications that can be replaced at the time of the present application It should be understood that there may be equivalents and variations.
본 발명의 바람직한 실시예에 따른 헬리콥터의 자유회전을 이용한 자유낙하 방식의 공중촬영장치(100)는, 발사수단에 의해 공중으로 발사되어 자유낙하하며 지상의 물체, 시설 및 지형 등을 촬영하는 촬영장치로서, 도 1 및 도 2에 도시된 바와 같이, 바디부(110), 헤드부(120), 블레이드(130) 및 카메라(140)를 포함하여 구비된다.The free-falling aerial photographing apparatus 100 using the free rotation of the helicopter according to the preferred embodiment of the present invention is a shooting device that is launched into the air by the firing means free-falling and photographing objects, facilities and terrain of the ground, etc. As shown in FIG. 1 and FIG. 2, the body part 110, the head part 120, the blade 130, and the camera 140 are provided.
먼저, 상기 바디부(110)는 공중촬영장치(100)의 본체를 형성하여 자유낙하중에 공중촬영장치(100)가 직립될 수 있도록 웨이트로 작용하는 부재로서, 알(Egg) 형상과 같은 유선형의 외형을 가지며 내부에는 각종 부품들이 실장되기 위한 공간부(116)가 마련되고 상부에는 헤드부(120)의 장착을 위한 회전축(111)이 직립배치된다.First, the body 110 is a member that forms a main body of the aerial photographing apparatus 100 and acts as a weight to allow the aerial photographing apparatus 100 to stand upright during free fall, and has a streamlined shape such as an egg shape. It has an external shape and is provided with a space portion 116 for mounting various components therein, and the rotary shaft 111 for mounting the head portion 120 is placed upright.
여기서, 상기 바디부(110)는 유선형의 외형을 가짐에 따라 발사시 공기저항을 최소화하여 동일한 발사동력으로 보다 높은 위치까지 발사시킬 수 있다.Here, the body portion 110 has a streamlined appearance to minimize the air resistance when firing can be launched to a higher position with the same firing power.
상기 헤드부(120)는 블레이드(130)를 회전시키기 위한 부재로서, 상기 회전축(111)에 축결합되어 바디부(110)에 대하여 독립적으로 회전가능하게 장착된다.The head part 120 is a member for rotating the blade 130 and is axially coupled to the rotation shaft 111 so as to be independently rotatable with respect to the body part 110.
여기서, 상기 회전축(111)에는 볼베어링과 같이 바디부(110)와 헤드부(120) 간의 상대회전 운동에 따른 마찰력을 감소시키기 위한 회전지지부재가 마련되어, 상기 마찰력에 의해 헤드부(120)의 회전력의 일부가 바디부(110)로 전달면서 바디부(110)가 함께 회전하려는 힘을 감소시킬 수 있도록 구비되는 것이 바람직하다.Here, the rotation shaft 111 is provided with a rotation support member for reducing the frictional force due to the relative rotational movement between the body 110 and the head 120, such as a ball bearing, the rotational force of the head portion 120 by the frictional force A portion of the body portion 110 is preferably provided to be able to reduce the force to be rotated together while the body portion 110.
또한, 상기 헤드부(120)의 상부면은 도면에서와 같이 라운드진 유선형으로 형성되어 발사시 또는 회전시 공기와의 마찰을 최소화하는 것이 바람직하다.In addition, the upper surface of the head portion 120 is preferably formed in a rounded streamline as shown in the figure to minimize the friction with air during launch or rotation.
상기 블레이드(130)는 공중촬영장치(100)가 균형을 유지할 수 있도록 양력을 제공하는 부재로서, 상기 헤드부(120)의 둘레를 따라 일정간격 이격되어 장착되면서 하강함에 따라 하부에서 유입되는 공기흐름에 의해 헤드부(120)와 함께 회전하며 양력을 생성한다.The blade 130 is a member that provides lifting force so that the aerial shooting apparatus 100 maintains a balance, and the air flows from the lower portion as it descends while being mounted at a predetermined interval along the circumference of the head part 120. By rotating with the head portion 120 to generate a lift.
여기서, 생성된 양력은 공중촬영장치(100)가 공중에 체류하는 시간을 증대시키며 바디부(110)가 직립한 상태로 균형을 유지하는데 이용되고, 양력축의 기울임으로 인해 공중촬영장치(100)를 조종하는데 이용된다.Here, the generated lift is used to increase the time that the aerial photographing apparatus 100 stays in the air and maintain the balance in the upright state of the body part 110, and the aerial photographing apparatus 100 is moved due to the tilt of the lifting axis. Used to steer.
상기 카메라(140)는 공중영상을 획득하는 촬영수단으로서, 상기 바디부(110)의 하부에 배치되어 하부방향 및 측부방향을 지향하여 촬영구동한다. 여기서, 촬영된 영상은 별도의 메모리에 저장되거나 무선통신으로 지상에 전송된다.The camera 140 is a photographing means for acquiring an aerial image. The camera 140 is disposed under the body 110 and drives the camera 140 in a lower direction and a side direction. Here, the captured image is stored in a separate memory or transmitted to the ground by wireless communication.
한편, 상기 헤드부(120)의 상단에는 탄성을 이용한 발사수단의 일부를 걸 수 있도록 절곡형성된 형상의 발사용고리(121)가 장착되어, 이 발사용고리(121)에 고무줄이나 용수철 등과 같이 탄성을 이용한 발사수단의 일부를 걸어 공중으로 발사시킬 수 있으므로 저가의 비용으로 발사수단을 마련할 수 있다.On the other hand, the upper end of the head portion 120 is equipped with a firing ring 121 of a shape bent to hang a portion of the firing means using the elastic, the firing ring 121 is elastic, such as a rubber band or a spring It is possible to provide a launch means at low cost because it can be launched into the air by walking a part of the launch means using.
또한, 상기 바디부(110)의 외부면에는 마찰돌기(113)가 돌출형성되어 바디부(110)를 파지한 사용자 피부와의 마찰력을 증대시킬 수 있으므로, 땀이나 건조한 피부 상태로 인해 미끄러지면서 조준방향이 어긋나거나 오발되는 것을 미연에 방지할 수 있어 보다 정확한 발사작업이 이루어질 수 있다.In addition, since the friction protrusion 113 protrudes from the outer surface of the body part 110 to increase the frictional force with the user's skin holding the body part 110, it is aimed while sliding due to sweat or dry skin condition. Misalignment or misfire can be prevented beforehand, resulting in more accurate firing.
상기 발사수단으로는 고무줄이나 압축스프링 등과 같은 탄성부재의 탄성을 이용하며 새총과 같이 탄성부재의 일측을 사용자가 파지한 별도의 지지대에 고정시키거나 탄성부재의 타측에 상기 발사용고리(121)를 지지하여 탄성부재가 신장되도록 잡아당긴 상태에서 원하는 조준방향으로 지향시킨 후 잡아당기는 힘을 제거함으로써 탄성부재의 탄성복원력의 힘을 이용하여 공중촬영장치(100)를 원하는 공중 위치로 발사시킬 수 있다.The firing means uses elasticity of an elastic member such as a rubber band or a compression spring, and fixes one side of the elastic member, such as a slingshot, to a separate support gripped by the user or the firing ring 121 on the other side of the elastic member. By supporting and pulling the elastic member so as to be directed in a desired aiming direction, the aerial photographing apparatus 100 may be launched to a desired aerial position by using the force of the elastic restoring force of the elastic member by removing the pulling force.
상기 탄성부재를 이용하는 방식 이외에 군사용으로 사용하는 신호탄용 발사장치와 같이 권총형상의 총구에 공중촬영장치(100)를 삽입하고 방아쇠를 당겨 화약의 연소력을 이용하여 공중 위치로 발사시킬 수도 있으며, 비행중인 항공기에서 공중촬영장치(100)를 원하는 지점에 낙하시키는 방식으로도 가능하다.In addition to the method using the elastic member, such as a signal firing device used for military purposes, such as a pistol-shaped muzzle is inserted into the air shooting device 100 and by pulling the trigger can be fired to the aerial position using the combustion power of gunpowder, flight It is also possible to drop the aerial shooting device 100 to the desired point in the aircraft in flight.
한편, 도 2에 도시된 바와 같이 상기 바디부(110)의 둘레에는 상부에서 하부를 향해 연장형성된 블레이드홈(112)이 형성되고, 상기 블레이드(130)는 힌지부(133)를 통해 헤드부(120)에 접철되게 장착되면서 상기 블레이드홈(112)에 삽입되어 바디부(110)에 밀착되거나 수평하게 펼쳐져 개방되도록 동작될 수 있다.Meanwhile, as shown in FIG. 2, a blade groove 112 extending from the upper portion to the lower portion is formed around the body portion 110, and the blade 130 has a head portion through a hinge portion 133. 120 may be inserted into the blade groove 112 while being foldably attached to the blade groove 112 to be in close contact with the body portion 110 or to be horizontally opened.
이에 따라 발사수단에 의한 공중 발사시에는 블레이드(130)를 접어 공기저항을 최소화함으로써 동일한 발사동력으로 보다 높은 위치까지 발사시킬 수 있으며, 하강하면서 자유낙하시에는 접어진 블레이드(130)를 개방시켜 균형을 위한 양력을 생성시킬 수 있다.Accordingly, when the air is launched by the launch means, the blade 130 can be folded to minimize the air resistance, so that it can be shot to a higher position with the same firing power, and when the free fall falls, the folded blade 130 is opened to balance. It can generate lift for.
이때, 상기 블레이드홈(112)은 공중촬영장치(100)의 하강에 따른 공기흐름으로 바디부(110)가 블레이드(130)의 회전방향과 반대방향으로 회전하도록 바디부(110)의 둘레를 따라 트위스트된 형태로 형성되는 것이 바람직하다.At this time, the blade groove 112 is along the circumference of the body portion 110 so that the body portion 110 rotates in a direction opposite to the rotation direction of the blade 130 in the air flow according to the aerial shooting device 100 descends. It is preferably formed in a twisted form.
예를 들어, 도면에서와 같이 블레이드(130)가 시계방향으로 회전하는 경우 상기 블레이드홈(112)은 도면기준 하부로 갈수록 반시계방향으로 회전하는 트위스트 형태로 형성됨으로써 하강하면서 발생되는 공기흐름에 의해 바디부(110)가 반시계방향으로 회전하도록 하는 것이다.For example, when the blade 130 rotates in a clockwise direction as shown in the drawing, the blade groove 112 is formed in a twisted shape that rotates counterclockwise as it goes downward to the drawing reference, and is caused by the air flow generated while falling. The body 110 is to rotate in a counterclockwise direction.
이와 같이, 상기 블레이드홈(112)은 하강에 따른 공기흐름으로 바디부(110)가 블레이드(130)의 회전방향과 반대방향으로 회전하도록 바디부(110)의 둘레를 따라 트위스트된 형태로 형성되므로, 상기 블레이드(130)의 회전력에 의해 함께 회전하려는 바디부(110)의 회전력을 최소화하여 정지된 공중영상을 촬영할 수 있다.As such, the blade groove 112 is formed in a twisted form along the circumference of the body portion 110 so that the body portion 110 rotates in a direction opposite to the rotational direction of the blade 130 in the air flow according to the falling By minimizing the rotational force of the body 110 to rotate together by the rotational force of the blade 130, it is possible to take a still aerial image.
또한, 상기 카메라(140)는 바디부(110)의 하부에 배치되되 복수 개가 각 블레이드홈(112) 내에 배치되어 상기 블레이드(130)가 개방된 상태에서 촬영이미지를 획득할 수 있도록 구비되는 것이 바람직하다. 따라서, 착지시 카메라(140)의 파손을 최소화하고 휴대나 보관시 카메라(140)의 렌즈에 먼지나 수분 등의 이물질이 유입되는 것을 효과적으로 방지할 수 있다. 또한, 복수의 카메라(140)를 각 블레이드홈(112)별로 배치함으로써 각 카메라(140)의 촬영영역을 분할하여 보다 넓은 영역의 공중영상을 획득할 수 있다.In addition, the camera 140 is disposed below the body portion 110, a plurality of are disposed in each blade groove 112 is preferably provided so as to obtain a photographed image in the open state of the blade 130. Do. Therefore, it is possible to minimize the damage of the camera 140 when landing and effectively prevent the inflow of foreign matter such as dust or moisture into the lens of the camera 140 when carrying or storing. In addition, by arranging the plurality of cameras 140 for each blade groove 112, an aerial image of a wider area may be obtained by dividing a photographing area of each camera 140.
한편, 본 발명의 바람직한 실시예에 따른 블레이드(130)는 힌지부(133)를 통해 헤드부(120)에 접철 가능하게 장착되되, 도 3 및 도 4에 도시된 자동개방수단(150,160)에 의해 발사시에는 접어져 바디부(110)에 밀착되고 공중에서 최고정점에서 하강하는 순간에 자동적으로 개방되도록 구비될 수 있다.On the other hand, the blade 130 according to the preferred embodiment of the invention is mounted to the head portion 120 foldable through the hinge portion 133, by the automatic opening means 150, 160 shown in Figures 3 and 4 When firing, it may be provided to be in close contact with the body 110 and open automatically at the moment of descending from the highest point in the air.
먼저, 도 3을 참고하면, 상기 블레이드(130)는 힌지스프링 형태의 힌지부(133)를 통해 헤드부(120)의 둘레에 접철되게 장착되고, 상기 블레이드(130)의 단부에는 링형상의 고정링(131)이 마련된다. 이때 상기 힌지부(133)는 블레이드(130)가 개방되도록 외측으로 작용하는 탄성력을 갖고 있다.First, referring to FIG. 3, the blade 130 is foldably mounted around the head portion 120 through a hinge portion 133 having a hinge spring shape, and a ring shape is fixed to an end portion of the blade 130. Ring 131 is provided. At this time, the hinge portion 133 has an elastic force acting outward so that the blade 130 is opened.
또한, 상기 자동개방수단(150)은, 상기 바디부(110)의 하부에 인출가능하게 장착되며 하단이 바디부(110)의 인출공(115)을 통해 하향 노출되게 직립배치되어 상기 고정링(131)이 삽입되면서 각 블레이드(130)를 고정시키는 인출로드와, 상기 인출로드(151)가 인출동작하는데 필요한 구동력을 제공하는 액추에이터(152)와, 공중으로 발사된 바디부(110)의 하강을 감지하는 센서부(153) 및, 상기 센서부(153)를 통해 하강이 감지되면 상기 액추에이터(152)를 구동제어하여 상기 인출로드(151)의 노출된 하단을 바디부(110)의 내부로 인입시키면서 각 블레이드(130)를 자동개방시키는 제어부(154)를 포함하여 구비될 수 있다.In addition, the automatic opening means 150 is mounted to be pulled out to the lower portion of the body portion 110 and the lower end is disposed upright so as to be exposed downward through the withdrawal hole 115 of the body portion 110 and the fixing ring ( 131 is inserted into the take-out rod for fixing each blade 130, the actuator 152 for providing the driving force required for the take-out rod 151 withdrawal operation, and the lowering of the body portion 110 launched into the air When the sensor unit 153 detects the fall through the sensor unit 153 and drives the actuator 152, the exposed lower end of the lead-out rod 151 is drawn into the body 110. It may be provided including a control unit 154 to automatically open each blade 130 while.
더불어, 도 4를 참고하면, 상기 블레이드(130)의 내측에는 상기 공간부의 내부에 관통삽입되는 걸림부(132)가 돌출형성된다.In addition, referring to Figure 4, the inside of the blade 130, the engaging portion 132 is inserted through the interior of the space is formed protruding.
또한, 상기 자동개방수단(160)은, 상기 바디부(110) 내에서 승강가능하게 장착되며 각 걸림부(132)에 지지되어 상기 블레이드(130)의 접철된 상태를 고정시키는 지지플레이트(161)와, 상기 지지플레이트(161)가 승강동작하는데 필요한 구동력을 제공하는 액추에이터(162)와, 공중으로 발사된 바디부(110)의 하강을 감지하는 센서부(163) 및, 상기 센서부(163)를 통해 하강이 감지되면 상기 액추에이터(162)를 구동제어하여 각 걸림부(132)의 지지된 상태를 해제시키면서 각 블레이드(130)를 자동개방시키는 제어부(164)를 포함하여 구비될 수 있다.In addition, the automatic opening means 160, the support plate 161 is mounted so as to be elevated in the body portion 110 and supported by each engaging portion 132 to fix the folded state of the blade 130. And an actuator 162 providing driving force necessary for the support plate 161 to move up and down, a sensor unit 163 for detecting a fall of the body unit 110 launched into the air, and the sensor unit 163. When the fall is detected through the control unit 162 may be provided with a control unit 164 for automatically opening each blade 130 while releasing the supported state of each engaging portion 132 by driving control.
이와 같이, 상기 블레이드(130)의 단부에 형성된 고정링(131)을 바디부(110)의 하부에 인출가능하게 직립배치된 인출로드(151)에 삽입하거나 블레이드(130)의 내측에 돌출형성된 걸림부(132)를 바디부(110)의 내부에 승강가능하게 배치된 지지플레이트(161)에 지지시켜, 각 블레이드(130)가 바디부(110)에 밀착되게 고정된 상태로 발사시킬 수 있으며, 자동개방수단(150,160)은 공중으로 발사된 공중촬영장치(100)의 하강이 감지되면 상기 인출로드(151)를 바디부(110)의 내부로 인입시키거나 지지플레이트(161)에 의한 각 걸림부(132)의 지지된 상태를 해제하도록 동작되면서, 각 블레이드(130)가 힌지스프링 형태를 갖는 힌지부(133)의 탄성력에 의해 자동개방되도록 제어할 수 있으므로 공중에서 블레이드(130)가 개방되지 않아 그대로 추락하여 장치가 파손되는 현상을 효과적으로 방지할 수 있다.As such, the locking ring 131 formed at the end of the blade 130 is inserted into the pull-out rod 151 arranged to be pulled upright in the lower portion of the body 110 or the protrusion formed to protrude inside the blade 130. By supporting the portion 132 to the support plate 161 which is arranged to be elevated in the body portion 110, each blade 130 can be launched in a fixed state in close contact with the body portion 110, The automatic opening means (150, 160) is to detect the falling of the aerial shooting device 100 launched into the air to pull the withdrawal rod 151 into the interior of the body portion 110 or each engaging portion by the support plate 161 While operating to release the supported state of 132, each blade 130 can be controlled to be automatically opened by the elastic force of the hinge portion 133 having a hinge spring form, so that the blade 130 is not opened in the air. Falling as it is, effectively destroying the device Can be prevented.
한편, 본 발명의 바람직한 실시예에 따른 공중촬영장치(100)는 자유낙하는 중에 낙하위치를 조절할 수 있도록 구비될 수 있다.On the other hand, the aerial shooting device 100 according to a preferred embodiment of the present invention may be provided to adjust the drop position during free fall.
이를 위해, 도 5의 (a)에 도시된 바와 같이 상기 바디부(110)의 내부에는 공간부(116)가 마련되고,상기 공간부(116) 내에 배치되며 제어신호에 따라 웨이트(176)의 위치를 조절하여 바디부(110)의 낙하방향을 제어하는 방향조절부(170)를 더 포함하여 구비될 수 있다.To this end, as shown in (a) of FIG. 5, a space portion 116 is provided inside the body portion 110, and disposed in the space portion 116 and the weight of the weight 176 according to a control signal. It may further include a direction control unit 170 for adjusting the position to control the falling direction of the body portion 110.
보다 구체적으로 설명하면, 도 5의 (b)에 도시된 바와 같이 상기 방향조절부(170)는 상기 공간부(116)의 내측에 지지되어 x축을 중심으로 롤링 가능하게 수평배치된 수평고리(171)와, y축 방향으로 연장되어 상기 수평고리(171)의 중앙을 가로 질러 수평배치되며 y축을 중심으로 롤링 가능하게 양단이 상기 수평고리(171)에 힌지결합되는 수평바(172)와, z축 방향으로 연장되어 상기 수평바(172)의 중앙에 직립배치되며 하단에는 웨이트(176)가 장착된 수직바(173)와, 상기 수직바(173)의 상부를 x축 방향으로 밀거나 잡아당기는 제1구동부(174) 및, 상기 수평바(172) 또는 수평고리(171)의 일측을 z축 방향으로 일거나 잡아당기는 제2구동부(175)를 포함하여 구비된다.More specifically, as illustrated in FIG. 5B, the direction adjusting part 170 is supported on the inner side of the space part 116 so that the horizontal ring 171 is horizontally arranged to be rolled around the x-axis. A horizontal bar 172 extending in the y-axis direction and horizontally disposed across the center of the horizontal ring 171 and having both ends hinged to the horizontal ring 171 so as to roll about the y axis; A vertical bar 173 extending in an axial direction and disposed upright in the center of the horizontal bar 172 and having a weight 176 mounted thereon, and pushing or pulling an upper portion of the vertical bar 173 in the x-axis direction. The first driving unit 174 and the horizontal bar 172 or the horizontal ring 171 includes a second driving unit 175 that lifts or pulls one side in the z-axis direction.
이러한 방향조절부(170)를 이용하여 지상에 배치된 무선통신을 이용한 조종수단을 이용하여 제어부(154)를 통해 방향조절부(170)의 각 구동부를 구동제어하여 웨이트(176)를 위치이동시킴으로써 바디부(110) 내에서의 편중된 하중이 양력축을 기울여서 원하는 공중 위치로의 이동이 가능하다.By controlling the driving unit of the direction control unit 170 through the control unit 154 by using a control means using a wireless communication disposed on the ground using the direction control unit 170 by moving the weight 176 to position The unbiased load in body 110 allows tilting the lift axis to move to the desired aerial position.
또는, 상기 조종수단을 이용하지 않고 관성항법센서를 배치하여 관성항법센서에 의한 발사위치를 기억하여 발사된 후 기류나 발사각도에 의해 발사지점으로부터 이격되더라도 관성항법센서를 통해 상기 발사지점으로의 위치이동이 가능하도록 동작시킬 수 있다.Alternatively, the position of the inertial navigation sensor is stored without using the control means, and the position of the inertial navigation sensor is stored by the inertial navigation sensor. It can be operated to move.
더불어, 상기 바디부(110) 내부에는 공중촬영장치(100)를 구동시키는데 필요한 구동전원을 공급하기 위한 배터리(미도시)가 내장되는데, 이 배터리 자체를 상기 웨이트(176)로 이용하거나 웨이트(176)의 케이스 내부에 배터리를 내장함으로써 웨이트 기능을 구현하는데 필요한 중량을 배터리의 중량으로 대체하여 장치의 소형화를 도모할 수도 있다.In addition, a battery (not shown) for supplying driving power required to drive the aerial photographing apparatus 100 is built in the body 110, and the battery itself is used as the weight 176 or the weight 176. By incorporating a battery inside the casing, the weight required to implement the weight function can be replaced with the weight of the battery, thereby miniaturizing the device.
여기서, 상기 배터리는 종래의 드론과 같이 블레이드를 강제회전시키기 위한 용도가 아니며, 통신 및 제어, 자동개방수단(150) 및 방향조절부(170)의 구동을 위한 구동전원을 제공하기 위한 용도로 이용되므로 바디부(110)의 내부에 실장될 수 있는 소형의 배터리가 이용된다.Here, the battery is not used for forcibly rotating the blade like the conventional drone, but used for providing a driving power source for communication and control, driving of the automatic opening means 150 and the direction control unit 170. Therefore, a small battery that can be mounted in the body 110 is used.
상술한 바와 같은 본 발명의 바람직한 실시예에 따른 공중촬영장치(100)의 각 구성 및 기능에 의해, 고무줄이나 용수철 등의 발사수단에 의해 공중으로 발사되어 자유낙하하면서 공중촬영이 이루어지므로, 종래의 드론과 같이 블레이드를 강제회전시키기 위한 모터, 배터리, 복잡한 조종시스템 등이 불필요하므로 장비의 부속품을 간소화하여 장치의 제조비용을 대폭 절감할 수 있으며 촬영을 위한 준비단계를 간소화할 수 있다.By the respective configurations and functions of the aerial shooting apparatus 100 according to the preferred embodiment of the present invention as described above, the aerial shooting is carried out by free-falling by being released into the air by means of launching means such as rubber bands or springs, Since drones do not require motors, batteries, or complex control systems to forcibly rotate the blades, they simplify the equipment's accessories, greatly reducing the manufacturing cost of the device, and simplifying preparation for shooting.
또한, 공중으로 발사된 후 바디부(110)의 상부에 장착된 블레이드(130)가 회전하면서 생성된 양력에 의해 비행하며 자유낙하하기 때문에 균형을 유지한 상태로 안정적인 공중영상을 촬영할 수 있으며 사용자에 의한 공중에서의 조종이 불필요하므로 전문적인 조종훈련없이도 일반인이 쉽게 이용할 수 있다.In addition, since the blade 130 mounted on the upper portion of the body 110 after being launched into the air to fly by the lift generated by the rotation and free fall, it can take a stable aerial image while maintaining a balanced state to the user It is not necessary to maneuver in the air by the public, so it can be used easily by the general public without any professional maneuvering training.
이상과 같이, 본 발명은 비록 한정된 실시예와 도면에 의해 설명되었으나, 본 발명은 이것에 의해 한정되지 않으며 본 발명이 속하는 기술분야에서 통상의 지식을 가진 자에 의해 본 발명의 기술 사상과 아래에 기재될 청구범위의 균등 범위 내에서 다양한 수정 및 변형이 가능함은 물론이다.As described above, although the present invention has been described by way of limited embodiments and drawings, the present invention is not limited thereto and is intended by those skilled in the art to which the present invention pertains. Of course, various modifications and variations are possible within the scope of equivalents of the claims to be described.
(부호의 설명)(Explanation of the sign)
100...공중촬영장치 110...바디부100 ... aerial photography 110 ... body parts
111...헤드부 112...블레이드홈111 Head 112 Blade groove
120...헤드부 121...발사용고리120 head 121 foot hook
130...블레이드 140...카메라130 ... blade 140 ... camera
150,160...자동개방수단 170...방향조절부150,160 ... automatic opening means 170 ... direction adjuster

Claims (9)

  1. 유선형의 외형을 가지며 상부에는 회전축(111)이 직립배치된 바디부(110);Body portion 110 has a streamlined appearance and the rotary shaft 111 is disposed upright;
    상기 회전축(111)에 축결합되어 상기 바디부(110)에 대하여 독립적으로 회전가능하게 장착되는 헤드부(120);A head portion 120 coupled to the rotation shaft 111 and rotatably mounted independently of the body portion 110;
    상기 헤드부(120)의 둘레를 따라 일정간격 이격되어 접철가능하게 장착되고 헤드부(120)와 함께 회전하며 양력을 생성하는 블레이드(130); 및Blades 130 that are spaced apart at regular intervals along the circumference of the head portion 120 is mounted foldable and rotates with the head portion 120 to generate a lift; And
    상기 바디부(110)의 하부에 배치되어 하부방향 또는 측부방향을 지향하여 촬영구동하는 카메라(140);를 포함하는 공중촬영장치.And a camera (140) disposed under the body unit (110) to drive the camera in a downward direction or in a lateral direction.
  2. 제 1항에 있어서,The method of claim 1,
    상기 바디부(110)의 둘레에는 상부에서 하부를 향해 연장형성된 블레이드홈(112)이 형성되고,Around the body portion 110 is formed a blade groove 112 extending from the top to the bottom,
    상기 블레이드(130)는 힌지부(133)를 통해 헤드부(120)에 접철되게 장착되면서 상기 블레이드홈(112)에 삽입되어 바디부(110)에 밀착되거나 수평하게 펼쳐져 개방되도록 동작하는 것을 특징으로 하는 공중촬영장치.The blade 130 is inserted into the blade groove 112 while being foldably mounted to the head portion 120 through the hinge portion 133 is in close contact with the body portion 110 or horizontally unfolded to operate to open Aerial shooting device.
  3. 제 2항에 있어서,The method of claim 2,
    상기 블레이드홈(112)은 하강에 따른 공기흐름으로 상기 바디부(110)가 상기 블레이드(130)의 회전방향과 반대방향으로 회전하도록 상기 바디부(110)의 둘레를 따라 트위스트된 형태로 형성된 것을 특징으로 하는 공중촬영장치.The blade groove 112 is formed in a twisted form along the circumference of the body portion 110 so that the body portion 110 rotates in a direction opposite to the rotation direction of the blade 130 in the air flow according to the descending Aerial shooting device characterized in that.
  4. 제 3항에 있어서,The method of claim 3, wherein
    복수의 카메라(140)는 각 블레이드홈(112) 내에 배치되어 상기 블레이드(130)가 개방된 상태에서 촬영이미지를 획득하는 것을 특징으로 하는 공중촬영장치.The plurality of cameras 140 is disposed in each blade groove 112, the aerial shooting device, characterized in that to obtain a photographed image in the state that the blade 130 is open.
  5. 제 1항에 있어서,The method of claim 1,
    상기 헤드부(120)의 상단에는 탄성을 이용한 발사수단의 일부를 걸 수 있도록 절곡형성된 형상의 발사용고리(121)가 장착되며,The upper end of the head portion 120 is equipped with a firing ring 121 is bent to be formed to hang a portion of the firing means using the elastic,
    상기 바디부(110)의 외부면에는 바디부(110)를 파지한 사용자의 피부간에 마찰력을 증대시키기 위한 마찰돌기(113)가 돌출형성된 것을 특징으로 하는 공중촬영장치.Aerial photographing device, characterized in that the outer surface of the body portion 110 is formed with a protruding friction projection 113 to increase the friction between the skin of the user holding the body portion 110.
  6. 제 1항에 있어서,The method of claim 1,
    상기 블레이드(130)는 힌지스프링 형태의 힌지부(133)를 통해 헤드부(120)의 둘레에 접철되게 장착되고,The blade 130 is foldably mounted around the head portion 120 through a hinge portion 133 of the hinge spring form,
    상기 블레이드(130)의 단부에는 링형상의 고정링(131)이 마련되며,An end portion of the blade 130 is provided with a ring-shaped fixing ring 131,
    상기 바디부(110)의 하부에 인출가능하게 장착되며 하단이 바디부(110)의 인출공(115)을 통해 하향 노출되게 직립배치되어 상기 고정링(131)이 삽입되면서 각 블레이드(130)를 고정시키는 인출로드(151)와, 상기 인출로드(151)가 인출동작하는데 필요한 구동력을 제공하는 액추에이터(152)와, 공중으로 발사된 바디부(110)의 하강을 감지하는 센서부(153) 및, 상기 센서부(153)를 통해 하강이 감지되면 상기 액추에이터(152)를 구동제어하여 상기 인출로드(151)의 노출된 하단을 바디부(110)의 내부로 인입시키면서 각 블레이드(130)를 자동개방시키는 제어부(154)를 포함하는 자동개방수단(150);을 더 포함하는 공중촬영장치.The lower end of the body portion 110 is mounted to be pulled out and the lower end is placed upright to be exposed downward through the outlet hole 115 of the body portion 110 so that the fixing ring 131 is inserted into each blade 130 A pull-out rod 151 for fixing, an actuator 152 for providing a driving force necessary for the pull-out rod 151 to pull out, a sensor unit 153 for detecting a fall of the body 110 fired into the air; When the lowering is sensed through the sensor unit 153, the actuator 152 is driven to control the actuator 152 to automatically guide each blade 130 while introducing the exposed lower end of the drawing rod 151 into the body 110. Aerial shooting device further comprises; automatic opening means 150 including a control unit 154 to open.
  7. 제 1항에 있어서,The method of claim 1,
    상기 블레이드(130)는 힌지스프링 형태의 힌지부(133)를 통해 헤드부(120)에 접철되게 장착되고,The blade 130 is foldably mounted to the head portion 120 through the hinge portion 133 of the hinge spring form,
    상기 블레이드(130)의 내측에는 상기 바디부(110)의 내부에 관통삽입되는 걸림부(132)가 돌출형성되며,The inside of the blade 130, the engaging portion 132 is inserted through the interior of the body portion 110 is formed projecting,
    상기 바디부(110) 내에서 승강가능하게 장착되며 각 걸림부(132)에 지지되어 상기 블레이드(130)의 접철된 상태를 고정시키는 지지플레이트(161)와, 상기 지지플레이트(161)가 승강동작하는데 필요한 구동력을 제공하는 액추에이터(162)와, 공중으로 발사된 바디부(110)의 하강을 감지하는 센서부(163) 및, 상기 센서부(163)를 통해 하강이 감지되면 상기 액추에이터(162)를 구동제어하여 각 걸림부(132)의 지지된 상태를 해제시키면서 각 블레이드(130)를 자동개방시키는 제어부(164)를 포함하는 자동개방수단(160);을 더 포함하는 것을 특징으로 하는 공중촬영장치.The support plate 161 which is mounted to be liftable in the body part 110 and is supported by each locking part 132 to fix the folded state of the blade 130, and the support plate 161 is lifted and lowered. Actuator 162 for providing the driving force required to perform, the sensor unit 163 for detecting the falling of the body portion 110 launched into the air, and the actuator 162 when the fall is sensed through the sensor unit 163 The driving control to release the supported state of each engaging portion 132 and automatically opening means 160 including a control unit 164 for automatically opening each blade 130; aerial shooting further comprising Device.
  8. 제 1항에 있어서,The method of claim 1,
    상기 바디부(110)의 내부에는 공간부(116)가 마련되고, 상기 공간부(116) 내에 배치되며 제어신호에 따라 웨이트(176)의 위치를 조절하여 바디부(110)의 낙하방향을 제어하는 방향조절부(170);를 더 포함하는 것을 특징으로 하는 공중촬영장치.A space portion 116 is provided inside the body portion 110, and disposed in the space portion 116 and controlling the drop direction of the body portion 110 by adjusting the position of the weight 176 according to a control signal. Directional control unit 170; Aerial shooting device further comprising.
  9. 제 8항에 있어서,The method of claim 8,
    상기 방향조절부(170)는,The direction control unit 170,
    상기 공간부(116)의 내측에 지지되어 x축을 중심으로 롤링 가능하게 수평배치된 수평고리(171)와,A horizontal ring 171 supported inside the space part 116 and arranged horizontally so as to be rolled about an x-axis;
    y축 방향으로 연장되어 상기 수평고리(171)의 중앙을 가로 질러 수평배치되며 y축을 중심으로 롤링 가능하게 양단이 상기 수평고리(171)에 힌지결합되는 수평바(172)와,a horizontal bar 172 extending in the y-axis direction and horizontally disposed across the center of the horizontal ring 171, the both ends being hinged to the horizontal ring 171 so as to be rolled around the y-axis;
    z축 방향으로 연장되어 상기 수평바(172)의 중앙에 직립배치되며 하단에는 웨이트(176)가 장착된 수직바(173)와,a vertical bar 173 extending in the z-axis direction and disposed upright in the center of the horizontal bar 172 and having a weight 176 mounted thereon;
    상기 수직바(173)의 상부를 x축 방향으로 밀거나 잡아당기는 제1구동부(174) 및,A first driving part 174 that pushes or pulls the upper portion of the vertical bar 173 in the x-axis direction;
    상기 수평바(172) 또는 수평고리(171)의 일측을 z축 방향으로 일거나 잡아당기는 제2구동부(175)를 포함하는 공중촬영장치.Aerial photographing apparatus comprising a second driving unit (175) for pulling or pulling one side of the horizontal bar (172) or the horizontal ring (171) in the z-axis direction.
PCT/KR2015/012050 2015-10-19 2015-11-10 Free-fall type aerial photographing device using free rotation of helicopter WO2017069320A1 (en)

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