WO2019098478A1 - 인명 구조용 자동 전개 튜브 및 이를 운반하는 드론 - Google Patents
인명 구조용 자동 전개 튜브 및 이를 운반하는 드론 Download PDFInfo
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- WO2019098478A1 WO2019098478A1 PCT/KR2018/006753 KR2018006753W WO2019098478A1 WO 2019098478 A1 WO2019098478 A1 WO 2019098478A1 KR 2018006753 W KR2018006753 W KR 2018006753W WO 2019098478 A1 WO2019098478 A1 WO 2019098478A1
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- WIPO (PCT)
- Prior art keywords
- tube
- arm
- gas
- automatic
- drone body
- Prior art date
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- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 1
- 229920002554 vinyl polymer Polymers 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63C—LAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
- B63C9/00—Life-saving in water
- B63C9/01—Air-sea rescue devices, i.e. equipment carried by, and capable of being dropped from, an aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63C—LAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
- B63C9/00—Life-saving in water
- B63C9/08—Life-buoys, e.g. rings; Life-belts, jackets, suits, or the like
- B63C9/18—Inflatable equipment characterised by the gas-generating or inflation device
-
- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
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- 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
-
- B63B2728/00—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63C—LAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
- B63C9/00—Life-saving in water
- B63C2009/0023—Particular features common to inflatable life-saving equipment
- B63C2009/0029—Inflation devices comprising automatic activation means, e.g. for puncturing gas-generating cartridges
-
- 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
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Definitions
- the present invention relates to an automatic extension tube for lifesaving and a dron for carrying the same.
- the rescuer when rescuing a person who has fallen into the water from a river or sea, the rescuer swims directly to hold the person in the water and swim to the dry land to rescue it or to throw it at the end of an object such as a rope, When you grab it, the rescuer pulls the rope or the like to rescue it.
- the size of the tubes is so large that the drones' gas, various components such as batteries and chargers must also be enormous, and a specially designed drones are required. Also, since the volume of the tube is large, there is a limitation on the number of tubes that can carry the air resistance, and it is difficult to fly for a long time due to the gas giantization.
- the present invention can be applied to general hunting drones and utilized for lifesaving structure, and it is possible to carry out automatic lifting tube transportation and dropping part to existing lifesaving drones, An automatic expansion tube for lifesaving and a dron for carrying the same.
- An object of the present invention is to provide an automatic expansion tube which is transported through a dron and is automatically deployed by injecting gas through a gravitational acceleration at the time of drop from the dron, and a dron for transporting the automatic expansion tube.
- a drones for lifting an automatic lifting tube for lifesaving comprising: a drone body; A flywheel flying unit operable to generate a lift by a rotational force of the propeller provided in the drone body to fly in air; And an automatic expanding tube transporting and discharging unit provided on a lower surface of the drone body for separating the automatic expanding tube from the lower surface of the drone body at a predetermined height and discharging the automatic expanding tube, And the gas is injected into the interior through the lever position conversion according to the position of the lever.
- the automatic deployment tube includes a tube bag that is detachably attached to the automatic deployment tube transportation and discharge unit; A tube provided in the tube bag; And a gas supply unit having a release valve whose position is changed due to the gravitational acceleration, wherein the gas supply unit opens the gas stopper due to a change in the position of the release valve and injects the gas stored therein into the expansion tube .
- the automatic expanding tube transporting and discharging unit includes a body coupled to a lower surface of the drone body; And a hanger part provided in the body part and detachable from the tube bag and the release valve through a sliding operation.
- the hanger portion includes: a first arm slidably moved in a first direction to disengage the tube bag from the drone body; A second arm slidably moved in a second direction to separate the release valve from the drone body; A gear motor connected between the first arm and the second arm; A first binding unit coupled to the first arm; And a second engaging portion engaged with the second arm, wherein the first arm and the second arm are slidably operated through the gear motor so as to have a time difference.
- the tube bag further includes a first hook member detachable from the first binding portion via the first arm.
- the gas supply portion further includes a second hook member detachable from the second binding portion via the second arm.
- the automatic expanding tube transporting and discharging unit includes a distance measuring sensor for measuring a drop height between a water surface and the drone body; And a control unit for driving the gear motor when the drop height reaches the predetermined height.
- the automatic expanding tube transporting and delivering unit includes a camera unit for photographing a position image of a rescuer; An ultrasonic sensor for detecting the position of the rescuer through ultrasonic waves; And a heat-sensitive portion that detects the position of the rescuer through the thermal sensation.
- an automatic deployment tube that is transported through a dron according to an embodiment of the present invention includes a tube bag including an automatic rejection tube transporting and dropping portion of the drone and a detachable first hook member.
- a tube provided in the tube bag;
- the gas supply unit stores gas (CO 2) therein, Gas cylinders; A release valve whose position is varied to open the gas plug due to the gravitational acceleration; And a second hook member connecting the release valve and the row rejection.
- lifesaving structure can be effectively improved according to an embodiment of the present invention.
- the automatic opening tube of the cover dog can be attached to the drone and utilized for a plurality of the victims.
- FIG. 1 is a view showing an automatic expansion tube for lifesaving structure for drones according to an embodiment of the present invention and a dron for carrying the same.
- FIGS. 2A to 2C are views illustrating an example of the automatic expanding tube transporting and dropping unit shown in FIG. 1.
- FIG. 1
- FIGS. 3A to 3C are views illustrating another example of the automatic expanding tube transporting and dropping unit shown in FIG. 1.
- FIG. 3A to 3C are views illustrating another example of the automatic expanding tube transporting and dropping unit shown in FIG. 1.
- FIGS. 4A to 4D are views illustrating the operation of the automatic expanding tube transporting and delivering unit shown in FIG. 2 sequentially.
- FIG 5 is an exemplary view for explaining the process of injecting gas in the automatic expansion tube.
- FIG. 6 is an exemplary view showing a state in which the automatic expansion tube has been developed.
- FIG. 7 is a diagram illustrating an exemplary computing environment in which one or more embodiments disclosed herein may be implemented.
- a or B “at least one of A and / or B,” or “one or more of A and / or B,” may include all possible combinations of the listed items .
- “A or B,” “at least one of A and B,” or “at least one of A or B” includes (1) at least one A, (2) Or (3) at least one A and at least one B all together.
- first As used herein, the terms “first,” “second,” “first,” or “second,” and the like may denote various components, But is used to distinguish it from other components and does not limit the components.
- first user equipment and the second user equipment may represent different user equipment, regardless of order or importance.
- the first component can be named a second component, and similarly the second component can also be named a first component.
- any such element may be directly connected to the other element or may be connected through another element (e.g., a third element).
- a component e.g., a first component
- another component e.g., a second component
- there is no other component e.g., a third component
- a processor configured (or configured) to perform the phrases " A, B, and C " may be implemented by executing one or more software programs stored in a memory device or a dedicated processor (e.g., an embedded processor) , And a generic-purpose processor (e.g., a CPU or an application processor) capable of performing the corresponding operations.
- FIG. 1 is a view showing an automatic expansion tube for lifesaving structure for drones according to an embodiment of the present invention and a dron for transporting the same.
- FIGS. 2a to 2c show an example of the automatic expanding tube transportation and drop-
- FIGS. 3A to 3C are views showing another example of the automatic expanding tube transporting and dropping unit shown in FIG. 1, and FIGS. 4A to 4D sequentially show the operation of the automatic expanding tube transporting and dropping unit shown in FIG.
- FIG. 5 is an exemplary view for explaining a process of injecting gas in the automatic expanding tube
- FIG. 6 is an exemplary view showing a state in which the automatic expanding tube is completely deployed.
- the drones 200 for lifting the lifesaving structure automatic extension tube includes a drone body 210, a rotor blade flying unit 220, an automatic deployment tube transportation and dropping (230). ≪ / RTI >
- the automatic expanding tube transporting and dropping unit 230 is used for loading and unloading the automatic expanding tube 100 to be described later. A more detailed description of the structure of the automatic expansion tube 100 will be given later.
- the drone body 210 may be a circular, elliptical or polygonal structure.
- a wireless communication unit (not shown) for communicating with the remote control device 10 is provided on the inner side of the drone body 210.
- the wireless communication unit (not shown) includes RF communication, a VHF modem, (WiFi), and a satellite communication modem.
- the flywheel flying unit 220 is provided on the dragon body 210 to generate a lift by a rotational force to operate the flywheel 210 to fly.
- the rotor blade flying unit 220 may include a propeller motor and a propeller.
- the propeller motors are respectively provided at both side ends of the horizontal frame to generate rotational force, and the propeller is coupled to the end of the propeller motor and receives the rotational force of the propeller motor to generate a lift force.
- the automatic expanding tube transporting and discharging unit 230 is provided on the lower surface of the drone body 210 to separate the automatic opening tube 100 from the lower surface of the drone body 210 at a predetermined height And performs a dropping function.
- the automatic expanding tube transporting and delivering unit 230 may include a body part 231 and a row rejecting part 232.
- the body portion 231 may be coupled to the lower surface of the drone body 210 through a fastening member.
- the row rejection 232 is provided in the body portion 231 and mechanically connected to the tube back of the automatic expansion tube 100 and the release valve through a sliding operation.
- the automatic deployment tube 100 may include a tube bag 110, a development tube 120, and a gas supply unit 130.
- the tube bag 110 is detachable from the drone 200 and may be made of a cloth, vinyl or rubber material having a belt tape. Further, the tube bag 110 includes a first hook member composed of a reel and a wire.
- the tube 120 is provided in the tube bag 110 and expanded (expanded) when humidified.
- the gas supply unit 130 functions to inject gas (CO 2) into the expansion type tube by opening the gas pores due to the acceleration of gravity during dropping in the drones 200.
- the gas supply unit 130 may include a gas cylinder 131, a release valve 132, and a second hook member 134.
- the gas cylinder 131 may store a gas (CO 2) therein and may be a gas tank sealed with a gas stopper.
- the release valve 132 may be a unit for opening a gas ejection port (not shown) of the gas cylinder by opening a gas stopper of the gas cylinder 131.
- the second hook member 133 is composed of a reel 133-2 and a wire 133-1. One end of the wire 133-1 is connected to the release valve 132, 2).
- the reel 133-2 of the second hook member 134 is inserted into the second coupling portion 232-5 of the row rejection 232 of the automatic deployment tube transfer and dropping unit 230 described above.
- the row rejection 232 of the automatic expanding tube transporting and dropping unit 230 includes a first arm 232-1, a second arm 232-2, a gear motor 232-3, a first binding portion 232-4, and a second binding portion 232-5.
- the first arm 232-1 is slid in a first direction (for example, a leftward direction) through the operation of the gear motor 232-3 with a "?" And a reel connected to the tube bag 110 of the automatic expansion tube 100 connected to the body 210 is detached from the drone body 210.
- a first direction for example, a leftward direction
- the second arm 232-2 is slid in a second direction (for example, the right direction) through the operation of the gear motor 232-3, which is a " And the second hook member 134 of the automatic expansion tube 100 connected to the body 210 is detached from the drone body 210.
- the gear motor 232-3 is connected between the first arm 232-1 and the second arm 232-2 to rotate the first arm 232-1 in the first direction and the second arm 232-2, And drives the arm 232-2 to slide in the second direction.
- the gear motor 232-3 is connected to a rack gear provided at one end of the first arm 232-1 and connected to a rack gear provided at one end of the second arm 232-2 .
- the first binding portion 232-4 is a structure having a space in which the first arm 232-1 and the reels of the first hook member 111 are bound together and the second binding portion 232-5 Is a structure having a space (groove) in which the reels of the second arm 232-2 and the second hook member 133 are engaged.
- the length of the first arm 232-1 (the portion drawn into the first binding portion) and the length of the second arm 232-2 (the portion drawn into the second binding portion) have. More specifically, the length of the first arm 232-1 may be longer than that of the second arm 232-2. This means that the first arm 232-1 and the second arm 232-2 are slidably operated with a time difference.
- the automatic opening tube 100 transported through the above-described operation of the automatic expanding tube transporting and dropping unit 230 can be removed from the dron 200 (see FIGS. 4A to 4D).
- the automatic expanding tube transporting and unloading unit 230 may be configured such that the sliding operation of the first arm 232-1 and the sliding operation of the second arm 232-2 are performed And may include a first pinion gear and a second pinion gear having different numbers of teeth and sizes of teeth to have a time difference.
- the first pinion gear meshes with the gear motor 232-3 and the gear of the first arm 232-1 and the second pinion gear meshes with the gear motor 232-3 and the second arm 232-2. And is disposed so as to engage with the < Desc / Clms Page number 2 >
- first arm 232-1 and the second arm 232-2 of the automatic expanding tube transporting and dropping unit 230 are arranged such that the number of teeth and the size of the first and second pinion gears As shown in Fig.
- the automatic expanding tube transporting and delivering unit 230 may include a distance measuring sensor 233 and a driving control unit 234.
- the distance measuring sensor 233 measures the falling height between the water surface and the drone body 210.
- the drive control unit 234 functions to drive the gear motor 232-3 on the basis of the detection signal of the distance measuring sensor 233 when the fall height reaches the preset height or to operate the gear motor 232-3 10 to activate or deactivate the drive of the gear motor 232-3.
- the automatic expanding tube transporting and delivering unit 230 may further include an additional function.
- it may further include at least one or more of a camera section for photographing a position image of the rescuer, an ultrasonic sensor section for detecting the position of the rescuer through ultrasonic waves, and a thermal sensor section for sensing the temperature of the rescuer to detect the position of the rescuer.
- a camera section for photographing a position image of the rescuer
- an ultrasonic sensor section for detecting the position of the rescuer through ultrasonic waves
- a thermal sensor section for sensing the temperature of the rescuer to detect the position of the rescuer.
- the automatic extension tube for lifesaving structure according to the embodiment of the present invention and the drone for transporting it, it is not necessary for the rescuer to directly access the victim with the tube, thereby preventing the accident caused by the lifesaving structure .
- the present invention can be applied to general hunting drones and utilized for lifesaving structure, and it is possible to carry out automatic lifting tube transportation and dropping part to existing lifesaving drones, This provides the advantage.
- FIG. 7 is an illustration of an exemplary computing environment in which one or more embodiments disclosed herein may be implemented, and is illustrative of a system 1000 including a computing device 1100 configured to implement one or more of the embodiments described above. / RTI >
- the computing device 1100 may be a personal computer, a server computer, a handheld or laptop device, a mobile device (mobile phone, PDA, media player, etc.), a multiprocessor system, a consumer electronics device, A distributed computing environment including any of the above-described systems or devices, and the like.
- the computing device 1100 may include at least one processing unit 1110 and memory 1120.
- the processing unit 1110 may include, for example, a central processing unit (CPU), a graphics processing unit (GPU), a microprocessor, an application specific integrated circuit (ASIC), a field programmable gate array And may have a plurality of cores.
- the memory 1120 can be a volatile memory (e.g., RAM, etc.), a non-volatile memory (e.g., ROM, flash memory, etc.) or a combination thereof.
- the computing device 1100 may include additional storage 1130.
- Storage 1130 includes, but is not limited to, magnetic storage, optical storage, and the like.
- the storage 1130 may store computer readable instructions for implementing one or more embodiments as disclosed herein, and other computer readable instructions for implementing an operating system, application programs, and the like.
- the computer readable instructions stored in storage 1130 may be loaded into memory 1120 for execution by processing unit 1110.
- computing device 1100 may include input device (s) 1140 and output device (s) 1150.
- input device (s) 1140 may include, for example, a keyboard, a mouse, a pen, a voice input device, a touch input device, an infrared camera, a video input device, or any other input device.
- output device (s) 1150 can include, for example, one or more displays, speakers, printers, or any other output device.
- computing device 1100 may use an input device or output device included in another computing device as input device (s) 1140 or output device (s) 1150.
- the computing device 1100 may also include communication connection (s) 1160 that allow the computing device 1100 to communicate with other devices (e.g., computing device 1300).
- S 1160 may include a modem, a network interface card (NIC), an integrated network interface, a radio frequency transmitter / receiver, an infrared port, a USB connection or other Interface. Also, the communication connection (s) 1160 may include a wired connection or a wireless connection.
- NIC network interface card
- the communication connection (s) 1160 may include a wired connection or a wireless connection.
- Each component of the computing device 1100 described above may be connected by various interconnects (e.g., peripheral component interconnect (PCI), USB, firmware (IEEE 1394), optical bus architecture, etc.) And may be interconnected by the network 1200.
- PCI peripheral component interconnect
- IEEE 1394 firmware
- optical bus architecture etc.
- the terms "component,” “system,” and the like generally refer to a computer-related entity, which is hardware, a combination of hardware and software, software, or software in execution.
- an element may be, but is not limited to being, a processor, an object, an executable, an executable thread, a program and / or a computer running on a processor.
- both the application running on the controller and the controller may be components.
- One or more components may reside within a process and / or thread of execution, and the components may be localized on one computer and distributed among two or more computers.
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Abstract
Description
Claims (9)
- 인명 구조용 자동 전개 튜브를 운반하는 드론에 있어서,드론 몸체;상기 드론 몸체에 구비된 프로펠러의 회전력에 의해 양력을 발생시켜 공중비행하도록 동작하는 회전익비행수단부;상기 드론 몸체의 하부면에 구비되어, 기 설정된 높이에서 상기 자동 전개 튜브를 드론 몸체의 하부면과 분리시켜 투하하는 자동 전개 튜브 운송 및 투하부;를 포함하고,상기 자동 전개 튜브는투하시 중력가속도에 따른 레버 위치 변환을 통해 내부에 기체가 주입되어 자동전개되는 것을 특징으로 하는 인명 구조용 자동 전개 튜브 운반용 드론.
- 제1항에 있어서,상기 자동 전개 튜브는상기 자동 전개 튜브 운송 및 투하부와 착탈되는 튜브 백;상기 튜브 백 내에 구비된 전개식 튜브;상기 중력가속도로 인하여 위치가 변환되는 릴리즈 밸브를 구비한 가스 공급부;를 포함하고,상기 가스 공급부는 상기 릴리즈 밸브의 위치변화로 인하여 가스마개가 개구되어 내부에 저장된 가스를 상기 전개식 튜브 내로 주입하는 것을 특징으로 하는 인명 구조용 자동 전개 튜브 운반용 드론.
- 제2항에 있어서,상기 자동 전개 튜브 운송 및 투하부는상기 드론 몸체의 하부면과 결속된 몸체부;상기 몸체부 내에 구비되고, 슬라이딩 동작을 통해 상기 튜브 백 및 상기 릴리즈 밸브와 탈착되는 행거부를 포함하는 것을 특징으로 하는 인명 구조용 자동 전개 튜브 운반용 드론.
- 제3항에 있어서,상기 행거부는제1 방향으로 슬라이딩 동작되어 상기 튜브 백을 상기 드론 몸체에서 이탈시키는 제1 암;제2 방향으로 슬라이딩 동작되어 상기 릴리즈 밸브를 상기 드론 몸체에서 이탈시키는 제2 암;상기 제1 암과 상기 제2 암 간에 연결된 기어모터;상기 제1 암과 결속되는 제1 결속부; 및상기 제2 암과 결속되는 제2 결속부를 포함하고,상기 제1 암과 상기 제2 암은 시간 차를 갖도록 상기 기어모터를 통해 슬라이딩 동작되는 것을 특징으로 하는 인명 구조용 자동 전개 튜브 운반용 드론.
- 제4항에 있어서,상기 튜브 백은상기 제1 암을 통해 상기 제1 결속부와 탈착가능한 제1 후크 부재를 더 포함하는 인명 구조용 자동 전개 튜브 운반용 드론.
- 제4항에 있어서,상기 가스 공급부는상기 제2 암을 통해 상기 제2 결속부와 탈착가능한 제2 후크 부재를 더 포함하는 인명 구조용 자동 전개 튜브 운반용 드론.
- 제4항에 있어서,상기 자동 전개 튜브 운송 및 투하부는수면과 상기 드론 몸체 간의 낙하높이를 측정하는 거리측정센서; 및상기 낙하높이가 상기 기설정된 높이에 도달하면, 상기 거리측정센서에서 검출된 검출신호에 기초하여 상기 기어모터를 구동시키는 제어부를 더 포함하는 것을 특징으로 하는 인명 구조용 자동 전개 튜브 운반용 드론.
- 제4항에 있어서,상기 자동 전개 튜브 운송 및 투하부는구조자의 위치영상을 촬영하는 카메라부;초음파를 통해 구조자의 위치를 검출하는 초음파 감지부; 및열감지를 통해 구조자의 위치를 검출하는 열감지부 중 적어도 하나 이상을 포함하는 것을 특징으로 하는 인명 구조용 자동 전개 튜브 운반용 드론.
- 제1항 내지 제8항 중 어느 하나의 항에 기재된 드론을 통해 운반되는 자동 전개 튜브에 있어서,상기 드론의 자동 전개 튜브 운송 및 투하부의 행거부와 탈착가능한 제1 후크부재를 포함하는 튜브 백;상기 튜브 백 내에 구비된 전개식 튜브;상기 드론에서 낙하시에 중력가속도로 인하여 가스 막개를 개구시켜 상기 전개식 튜브 내로 가스(CO2)를 주입하는 가스 공급부를 포함하고,상기 가스 공급부는내부에 가스(CO2)를 저장하고, 가스 마개로 밀폐된 가스 실린더;상기 중력가속도로 인하여 상기 가스 마개를 개구시키도록 위치가 가변되는 릴리즈밸브; 및상기 릴리즈밸브와 상기 행거부 간을 연결하는 제2 후크부재를 포함하는 자동 전개 튜브.
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