JP2017196949A5 - - Google Patents

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Publication number
JP2017196949A5
JP2017196949A5 JP2016087685A JP2016087685A JP2017196949A5 JP 2017196949 A5 JP2017196949 A5 JP 2017196949A5 JP 2016087685 A JP2016087685 A JP 2016087685A JP 2016087685 A JP2016087685 A JP 2016087685A JP 2017196949 A5 JP2017196949 A5 JP 2017196949A5
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Japan
Prior art keywords
fixed
shaft
bottom plate
main body
link pieces
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JP2016087685A
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Japanese (ja)
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JP6536996B2 (en
JP2017196949A (en
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Priority to JP2016087685A priority Critical patent/JP6536996B2/en
Priority claimed from JP2016087685A external-priority patent/JP6536996B2/en
Priority to PCT/JP2017/015434 priority patent/WO2017188041A1/en
Publication of JP2017196949A publication Critical patent/JP2017196949A/en
Publication of JP2017196949A5 publication Critical patent/JP2017196949A5/ja
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Claims (8)

複数の回転翼を備える小型無人飛行機と、
投下物を収容および投下可能な搬送容器と、
前記搬送容器を操作するアクチュエータと、を備える鉛直投下装置であって、
前記搬送容器は前記小型無人飛行機の下部に相対移動不能に固定されており、
前記搬送容器の底部はその幅方向に並べて配置された二枚の底板部により構成され、
前記各底板部において、それぞれ他方となる前記底板部側の端部を先端、その反対側の端部を後端としたときに、
前記各底板部の上面は、前記後端から前記先端に向かって同じ傾斜角度で下方へ傾斜しており、
前記二枚の底板部は、同時に、かつ対称的な軌跡で展開可能であり、
前記搬送容器は、前記底部の閉時において筒形状の外形を有する本体部と、該本体部の両端の開口を塞ぐ二枚の蓋体と、を有し、
前記二枚の蓋体のうち少なくともいずれか一方は、軸体である固定軸に、該固定軸を中心としてその周方向に回転可能に支持された回転蓋であることを特徴とする鉛直投下装置。
A small unmanned airplane with multiple rotors,
A transport container capable of containing and dropping products;
And an actuator for operating the transport container.
The transfer container is fixed to the lower part of the small unmanned airplane relative to the lower part of the small unmanned airplane,
The bottom portion of the transfer container is constituted by two bottom plate portions arranged side by side in the width direction,
In each of the bottom plate portions, when the other end on the side of the bottom plate which is the other is a front end and the end on the opposite side is a rear end,
The upper surface of each bottom plate portion is inclined downward at the same inclination angle from the rear end toward the front end,
Wherein two of the bottom plate portion simultaneously, and Ri deployable der in a symmetrical trajectory,
The transport container has a main body having a cylindrical outer shape when the bottom is closed, and two lids closing the openings at both ends of the main body,
A vertical drop apparatus characterized in that at least one of the two lids is a rotary lid rotatably supported in a circumferential direction about the stationary shaft on a stationary shaft which is a shaft. .
前記本体部は、いずれかの前記開口から見て左右に分割された二つの半筒体を有し、
前記二つの半筒体の下側の半体は前記底部を構成し、
前記各半筒体の上端部は、該上端部と平行に配置された共通の軸体である前記固定軸に、該固定軸の周方向に沿って回動可能に支持されており、
前記二つの半筒体は、同時に、かつ対称的な軌跡で展開可能であることを特徴とする請求項1に記載の鉛直投下装置。
The main body portion has two half cylinders divided into right and left as viewed from any one of the openings;
The lower half of the two halves form the bottom,
The upper end of the respective half-cylindrical body, said fixed shaft is a common shaft which is parallel with the upper end portion, and is rotatably supported along the circumferential direction of the fixed shaft,
The vertical throwing apparatus according to claim 1, wherein the two semi-cylindrical bodies can be deployed simultaneously and in symmetrical trajectories.
前記本体部は前記底部の閉時において角筒形状の外形を有し、
前記各半筒体は、いずれかの前記開口から見た断面がL字形に形成されており、
前記二つの底板部の先端には、その長手方向に沿って互い違いに設けられた凸状の歯部が形成されており、
前記底部の閉時には前記二つの底板部の歯部が噛合されることを特徴とする請求項2に記載の鉛直投下装置。
The main body portion has a rectangular cylindrical outer shape when the bottom portion is closed,
Each of the half cylinders has an L-shaped cross section as viewed from any one of the openings;
The tips of the two bottom plates are formed with convex tooth portions provided alternately along the longitudinal direction,
The vertical drop apparatus according to claim 2, wherein the teeth of the two bottom plates are engaged when the bottom is closed.
複数の回転翼を備える小型無人飛行機と、
投下物を収容および投下可能な搬送容器と、
前記搬送容器を操作するアクチュエータと、を備える鉛直投下装置であって、
前記搬送容器は前記小型無人飛行機の下部に相対移動不能に固定されており、
前記搬送容器の底部はその幅方向に並べて配置された二枚の底板部により構成され、
前記各底板部において、それぞれ他方となる前記底板部側の端部を先端、その反対側の端部を後端としたときに、
前記各底板部の上面は、前記後端から前記先端に向かって同じ傾斜角度で下方へ傾斜しており、
前記搬送容器は、前記底部の閉時において筒形状の外形を有する本体部と、該本体部の両端の開口を塞ぐ二枚の蓋体と、を有し、
前記本体部は、いずれかの前記開口から見て左右に分割された二つの半筒体を有し、
前記二つの半筒体の下側の半体は前記底部を構成し、
前記各半筒体の上端部は、該上端部と平行に配置された共通の軸体である固定軸に、該固定軸の周方向に沿って回動可能に支持されており、
前記二つの半筒体は、同時に、かつ対称的な軌跡で展開可能であり、
前記搬送容器はさらに、前記二つの半筒体の開閉動作を同期させる同期機構を有し、
前記同期機構は、長穴が形成されたリンク片である固定リンク片および二つの可動リンク片と、これらすべてのリンク片の長穴に挿通された共通の軸体である可動軸とを有し、
前記固定リンク片は前記固定軸に、前記二つの可動リンク片は前記各半筒体の外周面における上端近傍部にそれぞれ固定されており、
前記固定リンク片はその長穴が上下方向に延びる角度で配置されており、
前記各可動リンク片は、それらの長穴のうち前記可動軸が挿通された部分のみが前記固定リンク片の長穴と重なるように、該固定リンク片に対して対称的な角度で配置されていることを特徴とする鉛直投下装置
A small unmanned airplane with multiple rotors,
A transport container capable of containing and dropping products;
And an actuator for operating the transport container.
The transfer container is fixed to the lower part of the small unmanned airplane relative to the lower part of the small unmanned airplane,
The bottom portion of the transfer container is constituted by two bottom plate portions arranged side by side in the width direction,
In each of the bottom plate portions, when the other end on the side of the bottom plate which is the other is a front end and the end on the opposite side is a rear end,
The upper surface of each bottom plate portion is inclined downward at the same inclination angle from the rear end toward the front end,
The transport container has a main body having a cylindrical outer shape when the bottom is closed, and two lids closing the openings at both ends of the main body,
The main body portion has two half cylinders divided into right and left as viewed from any one of the openings;
The lower half of the two halves form the bottom,
An upper end portion of each of the semi-cylindrical members is rotatably supported along a circumferential direction of the fixed shaft by a fixed shaft which is a common shaft disposed parallel to the upper end portion.
The two semi-cylindrical bodies can be deployed in simultaneous and symmetrical trajectories,
The transfer container further includes a synchronization mechanism that synchronizes the opening and closing operations of the two half cylinders,
The synchronization mechanism has a fixed link piece and two movable link pieces that are link pieces in which an elongated hole is formed, and a movable shaft that is a common shaft inserted into the elongated holes of all these link pieces. ,
The fixed link piece is fixed to the fixed shaft, and the two movable link pieces are fixed to the upper end vicinity portion of the outer peripheral surface of each half cylinder, respectively.
The fixed link pieces are disposed at an angle at which the elongated holes extend in the vertical direction,
Each of the movable link pieces is disposed at a symmetrical angle with respect to the fixed link piece such that only a portion of the elongated hole through which the movable shaft is inserted overlaps the long hole of the fixed link piece Vertical dropping device characterized by
前記固定リンク片は前記固定軸の軸方向に沿って所定の間隔を空けて二つ配置されており、
前記各可動リンク片は、前記軸方向において前記二つの固定リンク片の間に配置されていることを特徴とする請求項4に記載の鉛直投下装置。
The two fixed link pieces are arranged at predetermined intervals along the axial direction of the fixed shaft,
The vertical drop apparatus according to claim 4, wherein each of the movable link pieces is disposed between the two fixed link pieces in the axial direction.
前記アクチュエータは、前記二つの半筒体のうちいずれか一方にのみ連結されていることを特徴とする請求項4に記載の鉛直投下装置。 5. The vertical drop apparatus according to claim 4 , wherein the actuator is connected to only one of the two half cylinders. 前記回転蓋は、弾性部材により前記本体部側へ常時付勢されており、
前記回転蓋は、前記開口を塞ぐ位置ではその回転が規制され、
前記回転蓋は、前記弾性部材の付勢力に抗して前記搬送容器から引き離されることにより回転可能となることを特徴とする請求項1に記載の鉛直投下装置。
The rotating lid is always urged toward the main body by an elastic member,
The rotation of the rotary lid is restricted at the position where the opening is closed,
The vertical drop apparatus according to claim 1 , wherein the rotary lid is rotatable by being pulled away from the transport container against the biasing force of the elastic member.
前記底部には、前記底部の閉時において鉛直下方を向くカメラが配置されていることを特徴とする請求項1に記載の鉛直投下装置。 The vertical drop apparatus according to claim 1 , wherein a camera facing vertically downward when the bottom is closed is disposed at the bottom.
JP2016087685A 2016-04-26 2016-04-26 Vertical dropping device Active JP6536996B2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP2016087685A JP6536996B2 (en) 2016-04-26 2016-04-26 Vertical dropping device
PCT/JP2017/015434 WO2017188041A1 (en) 2016-04-26 2017-04-17 Drop-release device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2016087685A JP6536996B2 (en) 2016-04-26 2016-04-26 Vertical dropping device

Publications (3)

Publication Number Publication Date
JP2017196949A JP2017196949A (en) 2017-11-02
JP2017196949A5 true JP2017196949A5 (en) 2019-05-23
JP6536996B2 JP6536996B2 (en) 2019-07-03

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Family Applications (1)

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JP2016087685A Active JP6536996B2 (en) 2016-04-26 2016-04-26 Vertical dropping device

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JP (1) JP6536996B2 (en)
WO (1) WO2017188041A1 (en)

Families Citing this family (11)

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JP6763578B2 (en) * 2018-08-25 2020-09-30 株式会社DroneWorkSystem Transport drop unit for drones
CN109335008A (en) * 2018-10-12 2019-02-15 南通理工学院 A kind of unmanned plane obstacle avoidance system and barrier-avoiding method
JP7205823B2 (en) 2018-12-05 2023-01-17 株式会社ニックス Gripping mechanism and conveying device
US11554856B2 (en) 2018-12-27 2023-01-17 Rakuten Group, Inc. Unmanned aerial vehicle
CN111629964B (en) 2018-12-27 2023-09-29 乐天集团股份有限公司 Unmanned plane
CN110271669B (en) * 2019-06-18 2024-02-09 深圳高度创新技术有限公司 Fire control disaster relief unmanned aerial vehicle
CN110316378B (en) * 2019-07-23 2024-04-05 河南农业大学 Trichogramma ball throwing device based on unmanned aerial vehicle
JP2020183326A (en) * 2020-06-18 2020-11-12 D−Plan株式会社 Hook for unloading
WO2022034628A1 (en) * 2020-08-11 2022-02-17 株式会社エアロネクスト Moving body
CN112193416A (en) * 2020-09-29 2021-01-08 北京二郎神科技有限公司 Unmanned aerial vehicle and logistics distribution system
CN115779299B (en) * 2022-11-15 2024-05-03 亿航智能设备(广州)有限公司 Unmanned aerial vehicle automatic fire extinguishing system and method

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US6679454B2 (en) * 2002-04-15 2004-01-20 The Boeing Company Radial sonobuoy launcher
US20110084162A1 (en) * 2009-10-09 2011-04-14 Honeywell International Inc. Autonomous Payload Parsing Management System and Structure for an Unmanned Aerial Vehicle
CN204527648U (en) * 2015-04-21 2015-08-05 刘亚敏 For the grabbing device of multi-rotor aerocraft

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