JP2016037246A - Aerial imaging apparatus - Google Patents

Aerial imaging apparatus Download PDF

Info

Publication number
JP2016037246A
JP2016037246A JP2014163053A JP2014163053A JP2016037246A JP 2016037246 A JP2016037246 A JP 2016037246A JP 2014163053 A JP2014163053 A JP 2014163053A JP 2014163053 A JP2014163053 A JP 2014163053A JP 2016037246 A JP2016037246 A JP 2016037246A
Authority
JP
Japan
Prior art keywords
balloon
radio control
axis direction
aerial
radio
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2014163053A
Other languages
Japanese (ja)
Inventor
和之 高橋
Kazuyuki Takahashi
和之 高橋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Eyetec Co Ltd
Original Assignee
Eyetec Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eyetec Co Ltd filed Critical Eyetec Co Ltd
Priority to JP2014163053A priority Critical patent/JP2016037246A/en
Publication of JP2016037246A publication Critical patent/JP2016037246A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • G—PHYSICS
    • G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
    • G03B15/00—Special procedures for taking photographs; Apparatus therefor
    • G03B15/006—Apparatus mounted on flying objects

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Toys (AREA)
  • Stereoscopic And Panoramic Photography (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide an aerial imaging apparatus capable of improving wind resistance and capable of being easily moved to a target place.SOLUTION: An aerial imaging apparatus 10 includes a balloon 11, a radio-controlled helicopter 12 that is attached to the balloon 11, and imaging equipment 13 for being operated by radio control. The balloon 11 is formed in a spheroidal shape, and its inside is filled with helium gas. The ratio L2/L1 of the minor-axis-direction length L2 of the balloon 11 to the major-axis-direction length L1 thereof is set to be in the range of 0.55 or larger and 0.65 or smaller.SELECTED DRAWING: Figure 1

Description

本発明は、気球を利用して上空から目的の場所を撮影することのできる空中撮影装置に関する。   The present invention relates to an aerial photographing apparatus capable of photographing a target place from above using a balloon.

従来、空撮写真は、例えば、セスナ機に依存してきたが、コストが高いために、すぐに欲しい画像を入手することは難しかった。また、ラジコンヘリコプターによる空撮も利用されているが、操縦に熟練が必要で、墜落の危険性がある。これに対して、ヘリウムガスを用いた気球による空撮は、撮影の自由度が高く、低コストでリアルタイムに画像を入手することができ、万一落下しても事故の可能性が低いことから、一般に利用されている。この気球を利用した空中撮影装置は、気球にカメラを取り付けて、空中に浮上させ、目的の場所を撮影することができるようにしたものであり、気球の形状としては、例えば、球形状や一方向に伸長させた形状が用いられている（例えば、特許文献１参照）。   Conventionally, aerial photography has been dependent on, for example, a Cessna machine, but due to the high cost, it was difficult to obtain the desired image immediately. In addition, aerial photography with a radio control helicopter is also used, but skill is required for maneuvering and there is a risk of crash. On the other hand, aerial photography using a balloon using helium gas has a high degree of freedom of photography, and can obtain images in real time at low cost, and even if it falls, the possibility of an accident is low Is generally used. This aerial photography device using a balloon is a device in which a camera is attached to a balloon and floats in the air so that a target location can be photographed. The shape extended in the direction is used (for example, refer to Patent Document 1).

特開２００３−４３５６９号公報JP 2003-43569 A

しかしながら、上空は風が吹いていることが多いので、気球を球形状とした場合には、風に流されやすく、少し強い風が吹いていると撮影ができないという問題があった。また、気球を一方向に伸長させた形状とした場合には、伸長方向の風には強いが、横方向に風には弱いので、少し強い風が吹いていると、目的の場所に移動させることが難しくなり、目的の撮影ができないという問題があった。   However, since the wind is often blowing in the sky, there is a problem that when the balloon is made into a spherical shape, it is easy to be blown by the wind, and shooting is not possible if a little strong wind is blowing. Also, when the balloon is extended in one direction, it is strong against the wind in the extension direction but weak against the wind in the lateral direction, so if the wind is blowing a little, move it to the target location. There was a problem that it was difficult to achieve the desired shooting.

本発明は、このような問題に基づきなされたものであり、耐風性を向上させることができ、目的の場所に容易に移動させることができる空中撮影装置を提供することを目的とする。   The present invention has been made based on such problems, and an object of the present invention is to provide an aerial photographing apparatus that can improve wind resistance and can be easily moved to a target location.

本発明の空中撮影装置は、回転楕円体形に形成され、長軸方向の長さに対する短軸方向の長さの比が０．５５以上０．６５以下の範囲内である気球と、この気球に取り付けられたラジコンヘリコプターと、このラジコンヘリコプターに取り付けられ、ラジコンにより操作される撮像機器と、気球を地上に繋留する繋留索とを備えたものである。   An aerial photographing apparatus of the present invention is formed in a spheroid shape, and a ratio of a length in a minor axis direction to a length in a minor axis direction is in a range of 0.55 or more and 0.65 or less, and the balloon A radio control helicopter attached, an imaging device attached to the radio control helicopter and operated by the radio control, and a tether for tethering the balloon to the ground are provided.

本発明の空中撮影装置によれば、気球を回転楕円体形とし、長軸方向の長さに対する短軸方向の長さの比を０．５５以上０．６５以下とするようにしたので、全ての方向における耐風性を向上させることができる。また、気球にラジコンヘリコプターを取り付けているので、空撮時に容易に希望の場所に移動させることができる。更に、気球とラジコンヘリコプターとを用いるようにしたので、ラジコンヘリコプターの電池が切れても、気球により緩やかに下降させることができる。   According to the aerial photographing apparatus of the present invention, since the balloon has a spheroid shape, the ratio of the length in the minor axis direction to the length in the major axis direction is set to 0.55 or more and 0.65 or less. Wind resistance in the direction can be improved. Also, since a radio control helicopter is attached to the balloon, it can be easily moved to the desired location during aerial photography. Further, since the balloon and the radio control helicopter are used, even if the battery of the radio control helicopter runs out, the balloon can be lowered slowly.

本発明の一実施の形態に係る空中撮影装置の構成を表す図である。It is a figure showing the structure of the aerial imaging device which concerns on one embodiment of this invention.

以下、本発明の実施の形態について、図面を参照して詳細に説明する。   Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings.

図１は、本発明の一実施の形態に係る空中撮像装置１０の構成を表わすものである。この空中撮像装置１０は、例えば、気球１１と、この気球１１に取り付けられたラジコンヘリコプター１２と、撮像機器１３とを備えている。   FIG. 1 shows a configuration of an aerial imaging apparatus 10 according to an embodiment of the present invention. The aerial imaging device 10 includes, for example, a balloon 11, a radio control helicopter 12 attached to the balloon 11, and an imaging device 13.

気球１１は、回転楕円体形に形成されており、内部にはヘリウムガスが充填されている。気球１１の長軸方向の長さＬ１に対する短軸方向の長さＬ２の比Ｌ２／Ｌ１は、０．５５以上０．６５以下の範囲内とされており、０．５８以上０．６２以下の範囲内であればより好ましい。長軸方向の長さＬ１に対する短軸方向の長さＬ２の比Ｌ２／Ｌ１が０．６５よりも大きいと、球体に近くなるので風が上下に分かれ難くなり、風の抵抗を受けやすく、耐風性が低下してしまうからである。また、長軸方向の長さＬ１に対する短軸方向の長さＬ２の比Ｌ２／Ｌ１が０．５５よりも小さいと、厚みが薄くなり、浮力が低下してしまうからである。このような構成により、従来の気球では、風速２ｍ程度までしか空撮ができなかったのに対して、風速４ｍ程度まで空撮可能となっている。   The balloon 11 is formed in a spheroid shape and is filled with helium gas. The ratio L2 / L1 of the length L2 in the minor axis direction to the length L1 in the major axis direction of the balloon 11 is in the range of 0.55 or more and 0.65 or less, and is 0.58 or more and 0.62 or less. It is more preferable if it is within the range. If the ratio L2 / L1 of the length L2 in the short axis direction to the length L1 in the long axis direction is larger than 0.65, the wind becomes difficult to separate because it is close to a sphere, and it is susceptible to wind resistance. This is because the performance is lowered. Further, if the ratio L2 / L1 of the length L2 in the minor axis direction to the length L1 in the major axis direction is smaller than 0.55, the thickness is reduced and the buoyancy is reduced. With such a configuration, the conventional balloon can only take aerial photography up to a wind speed of about 2 m, whereas it can take aerial photography up to a wind speed of about 4 m.

気球１１には、長軸方向を水平、短軸方向を垂直とした下側に、例えば、１又は複数のリング状の係止具１４が配設されている。この係止具１４には、例えば、吊索１５の一端が取り付けられ、吊索１５の他端は、ラジコンヘリコプター１２に取り付けられている。これにより、気球１１とラジコンヘリコプター１２とは吊索１５により連結され、気球１１は、長軸方向を水平、短軸方向を垂直として空中に浮上するようになっている。吊索１５は、例えば、ワイヤーをチューブで覆った構成とすることが好ましく、チューブはビニール製のものが好ましい。揺れに強くなり、ジャイロ的な役目を果たすことができるからである。   In the balloon 11, for example, one or a plurality of ring-shaped locking tools 14 are disposed on the lower side with the major axis direction being horizontal and the minor axis direction being vertical. For example, one end of a suspension rope 15 is attached to the locking tool 14, and the other end of the suspension rope 15 is attached to the radio control helicopter 12. Thereby, the balloon 11 and the radio control helicopter 12 are connected by the suspension rope 15, and the balloon 11 floats in the air with the major axis direction being horizontal and the minor axis direction being vertical. For example, the suspension cord 15 is preferably configured by covering a wire with a tube, and the tube is preferably made of vinyl. This is because it can withstand shaking and play a gyroscopic role.

ラジコンヘリコプター１２は、空撮時に自由に気球１１及び撮像機器１３を希望の場所に移動させるためのものである。ラジコンヘリコプター１２は、例えば、電池を内蔵し、電池により駆動するように構成されている。また、ラジコンヘリコプター１２は、無線により操縦できるように構成されている。   The radio control helicopter 12 is for freely moving the balloon 11 and the imaging device 13 to a desired location during aerial photography. The radio control helicopter 12 includes, for example, a battery and is configured to be driven by the battery. In addition, the radio control helicopter 12 is configured to be operated by radio.

撮像機器１３は、ラジコンヘリコプター１２に取り付けられており、ラジコンにより、すなわち無線により操作できるように構成されている。撮像機器１３としては、例えば、カメラやビデオが挙げられ、ラジコンヘリコプター１２に内蔵された電池から電力が供給されて駆動するように構成されている。このようにラジコンヘリコプター１２と撮像機器１３との電源を共通とすることにより、軽量化が図られている。   The imaging device 13 is attached to the radio control helicopter 12 and configured to be operated by radio control, that is, by radio. Examples of the imaging device 13 include a camera and a video, which are configured to be driven by power supplied from a battery built in the radio-controlled helicopter 12. Thus, weight reduction is achieved by making the power supply of the radio controlled helicopter 12 and the imaging device 13 common.

また、この空中撮像装置１０は、気球１１を地上に繋留する繋留索１６を備えている。繋留索１６の一端は、例えば、ラジコンヘリコプター１２又は撮像機器１３に取り付けられており、繋留索１６の他端は、リールなどよりなる巻き取りドラム１７に巻き取られている。これにより、繋留索１６を巻き戻せば気球１１は上昇し、逆に、繋留索１６を巻き取れば気球１１は下降するようになっている。また、ラジコンヘリコプター１２に繋留索１６を取り付けているので、ラジコンヘリコプター１２を移動させることにより、繋留索１６を撮像機器１３の撮像範囲外に流し、繋留索１６が映像に映り込まないようにすることができるようになっている。   The aerial imaging apparatus 10 includes a tether 16 for tethering the balloon 11 to the ground. One end of the tether 16 is attached to, for example, the radio control helicopter 12 or the imaging device 13, and the other end of the tether 16 is wound around a winding drum 17 made of a reel or the like. Thereby, if the tether 16 is rewound, the balloon 11 will rise, and conversely, if the tether 16 is wound up, the balloon 11 will descend. Further, since the mooring line 16 is attached to the radio controlled helicopter 12, the mooring line 16 is moved outside the imaging range of the imaging device 13 by moving the radio controlled helicopter 12, so that the mooring line 16 is not reflected in the image. Be able to.

この空中撮像装置１０は、例えば、次のようにして用いることができる。まず、例えば、気球１１内部にヘリウムガスを充填し、気球１１を空中に浮上させる。次いで、繋留索１６を巻き戻し、気球１１を上昇させ、ラジコンヘリコプター１２を無線により操縦して、目的とする希望の場所に気球１１及び撮像機器１３を移動させる。このように、この空中撮像装置１０では、ラジコンヘリコプター１２を用いているので、希望の場所に容易に移動させることができる。また、この空中撮像装置１０では、気球１１の形状を回転楕円体形とし、かつ、長軸方向の長さＬ１に対する短軸方向の長さＬ２の比Ｌ２／Ｌ１を所定の範囲内としているので、風速４ｍ程度の風が吹いていても、気球１１を浮上させて移動させることができる。   This aerial imaging apparatus 10 can be used as follows, for example. First, for example, the balloon 11 is filled with helium gas, and the balloon 11 is floated in the air. Next, the tether 16 is rewound, the balloon 11 is raised, the radio control helicopter 12 is operated by radio, and the balloon 11 and the imaging device 13 are moved to a desired desired location. Thus, in this aerial imaging device 10, since the radio control helicopter 12 is used, it can be easily moved to a desired place. Further, in this aerial imaging device 10, since the shape of the balloon 11 is a spheroid, and the ratio L2 / L1 of the length L2 in the minor axis direction to the length L1 in the major axis direction is within a predetermined range, Even when a wind with a wind speed of about 4 m is blowing, the balloon 11 can be lifted and moved.

続いて、ラジコンにより撮像機器１３を操作して撮像する。その際、ラジコンヘリコプター１２を操縦して、繋留索１６が撮像機器１３の撮像範囲内に入らない位置となるように調整することが好ましい。撮像が終了したら、ラジコンヘリコプター１２を無線により操縦して、操縦者の近くまで戻す。そののち、繋留索１６を巻き取り、気球１１を下降させる。なお、この空中撮像装置１０では、気球１１とラジコンヘリコプター１２とを用いているので、ラジコンヘリコプター１２の電池が切れたり、操縦を誤っても、気球１１により緩やかに下降させることができる。   Subsequently, an image is picked up by operating the imaging device 13 with a radio control. At that time, it is preferable that the radio controlled helicopter 12 is operated so that the tether 16 is adjusted to a position that does not fall within the imaging range of the imaging device 13. When imaging is completed, the radio controlled helicopter 12 is operated by radio and returned to the vicinity of the operator. After that, the tether 16 is wound up and the balloon 11 is lowered. In this aerial imaging apparatus 10, since the balloon 11 and the radio control helicopter 12 are used, even if the battery of the radio control helicopter 12 is exhausted or misoperated, the balloon 11 can be lowered slowly.

このように本実施の形態によれば、気球１１を回転楕円体形とし、長軸方向の長さＬ１に対する短軸方向の長さＬ２の比Ｌ２／Ｌ１を０．５５以上０．６５以下とするようにしたので、全ての方向における耐風性を向上させることができる。また、気球１１にラジコンヘリコプター１２を取り付けているので、空撮時に容易に希望の場所に移動させることができる。更に、気球１１とラジコンヘリコプター１２とを用いるようにしたので、ラジコンヘリコプター１２の電池が切れても、気球１１により緩やかに下降させることができる。   Thus, according to the present embodiment, the balloon 11 has a spheroid shape, and the ratio L2 / L1 of the length L2 in the minor axis direction to the length L1 in the major axis direction is set to 0.55 or more and 0.65 or less. Since it did in this way, the wind resistance in all the directions can be improved. Moreover, since the radio control helicopter 12 is attached to the balloon 11, it can be easily moved to a desired place during aerial photography. Furthermore, since the balloon 11 and the radio control helicopter 12 are used, even if the battery of the radio control helicopter 12 runs out, the balloon 11 can be gently lowered.

以上、実施の形態を挙げて本発明を説明したが、本発明は上記実施の形態に限定されるものではなく、種々変形可能である。例えば、上記実施の形態では、各構成要素について具体的に説明したが、全ての構成要素を備えていなくてもよく、また、他の構成要素を備えていてもよい。また、各構成要素は、他の構成を備えていてもよい。   The present invention has been described with reference to the embodiment. However, the present invention is not limited to the above embodiment, and various modifications can be made. For example, in the above embodiment, each component has been specifically described. However, not all the components may be provided, and other components may be provided. Each component may have other configurations.

空撮に用いることができる。   Can be used for aerial photography.

１０…空中撮像装置、１１…気球、１２…ラジコンヘリコプター、１３…撮像装置、１４…係止具、１５…吊索、１６…繋留索、１７…巻き取りドラム   DESCRIPTION OF SYMBOLS 10 ... Aerial imaging device, 11 ... Balloon, 12 ... Radio control helicopter, 13 ... Imaging device, 14 ... Locking tool, 15 ... Suspension rope, 16 ... Mooring rope, 17 ... Winding drum

Claims (1)

回転楕円体形に形成され、長軸方向の長さに対する短軸方向の長さの比が０．５５以上０．６５以下の範囲内である気球と、
この気球に取り付けられたラジコンヘリコプターと、
このラジコンヘリコプターに取り付けられ、ラジコンにより操作される撮像機器と、
前記気球を地上に繋留する繋留索と
を備えたことを特徴とする空中撮影装置。 A balloon having a spheroid shape and a ratio of a length in a minor axis direction to a length in a major axis direction within a range of 0.55 or more and 0.65 or less;
Radio control helicopter attached to this balloon,
An imaging device attached to this radio control helicopter and operated by the radio control,
An aerial imaging apparatus comprising: a tether for tethering the balloon to the ground.
JP2014163053A 2014-08-08 2014-08-08 Aerial imaging apparatus Pending JP2016037246A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2014163053A JP2016037246A (en) 2014-08-08 2014-08-08 Aerial imaging apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014163053A JP2016037246A (en) 2014-08-08 2014-08-08 Aerial imaging apparatus

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2016000825U Continuation JP3204086U (en) 2016-02-24 2016-02-24 Aerial photography device

Publications (1)

Publication Number Publication Date
JP2016037246A true JP2016037246A (en) 2016-03-22

Family

ID=55528702

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014163053A Pending JP2016037246A (en) 2014-08-08 2014-08-08 Aerial imaging apparatus

Country Status (1)

Country Link
JP (1) JP2016037246A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107444629A (en) * 2017-08-11 2017-12-08 广州光使者科技应用有限公司 A kind of unmanned plane electric power system and unmanned plane
JP2018050784A (en) * 2016-09-27 2018-04-05 正 星野 Flight toy
TWI641532B (en) * 2017-09-05 2018-11-21 朝陽科技大學 UAV and its flying method and driving device
WO2019012614A1 (en) * 2017-07-12 2019-01-17 株式会社エアロネクスト High-place observation device
JP2020034934A (en) * 2017-07-12 2020-03-05 株式会社エアロネクスト High-place observation device

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5212826A (en) * 1975-07-22 1977-01-31 Technical Eng Res:Kk Aerial photographic device
JPS55101937A (en) * 1979-01-31 1980-08-04 Fujita Corp Method and apparatus for aerial photography
JPS5897595A (en) * 1981-12-02 1983-06-10 株式会社東京タツノ Wireless controlled balloon
JPH03109199A (en) * 1989-09-20 1991-05-09 Hitachi Cable Ltd Sky monitoring device
JP2000326899A (en) * 1999-05-18 2000-11-28 Asahi:Kk Aerial photography device
JP2005271831A (en) * 2004-03-26 2005-10-06 Chugoku Electric Power Co Inc:The Unmanned flying object using floating gas
JP2006086140A (en) * 2004-08-05 2006-03-30 Soichiro Ono Method and device for solar light power generation using balloon object
JP3127683U (en) * 2006-04-13 2006-12-14 隆雄 本間 A flying object that freely moves in the air by a combination of the vertical thrust generated by a rotor blade driven by an electric motor or the like and the buoyancy of a balloon.
JP2007001458A (en) * 2005-06-24 2007-01-11 Tokyo Institute Of Technology Mooring type balloon
JP2012071645A (en) * 2010-09-28 2012-04-12 Topcon Corp Automatic taking-off and landing system
JP2013005471A (en) * 2011-06-11 2013-01-07 Kinki Univ Laser energy transmission system for major reactor accident
JP2013079034A (en) * 2011-10-05 2013-05-02 Zero:Kk Rotorcraft for aerial photographing
JP2013532608A (en) * 2010-07-30 2013-08-19 デイビッドソン・テクノロジー・リミテッド High altitude platform

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5212826A (en) * 1975-07-22 1977-01-31 Technical Eng Res:Kk Aerial photographic device
JPS55101937A (en) * 1979-01-31 1980-08-04 Fujita Corp Method and apparatus for aerial photography
JPS5897595A (en) * 1981-12-02 1983-06-10 株式会社東京タツノ Wireless controlled balloon
JPH03109199A (en) * 1989-09-20 1991-05-09 Hitachi Cable Ltd Sky monitoring device
JP2000326899A (en) * 1999-05-18 2000-11-28 Asahi:Kk Aerial photography device
JP2005271831A (en) * 2004-03-26 2005-10-06 Chugoku Electric Power Co Inc:The Unmanned flying object using floating gas
JP2006086140A (en) * 2004-08-05 2006-03-30 Soichiro Ono Method and device for solar light power generation using balloon object
JP2007001458A (en) * 2005-06-24 2007-01-11 Tokyo Institute Of Technology Mooring type balloon
JP3127683U (en) * 2006-04-13 2006-12-14 隆雄 本間 A flying object that freely moves in the air by a combination of the vertical thrust generated by a rotor blade driven by an electric motor or the like and the buoyancy of a balloon.
JP2013532608A (en) * 2010-07-30 2013-08-19 デイビッドソン・テクノロジー・リミテッド High altitude platform
JP2012071645A (en) * 2010-09-28 2012-04-12 Topcon Corp Automatic taking-off and landing system
JP2013005471A (en) * 2011-06-11 2013-01-07 Kinki Univ Laser energy transmission system for major reactor accident
JP2013079034A (en) * 2011-10-05 2013-05-02 Zero:Kk Rotorcraft for aerial photographing

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018050784A (en) * 2016-09-27 2018-04-05 正 星野 Flight toy
WO2019012614A1 (en) * 2017-07-12 2019-01-17 株式会社エアロネクスト High-place observation device
JPWO2019012614A1 (en) * 2017-07-12 2019-12-12 株式会社エアロネクスト Altitude observation device
JP2020034934A (en) * 2017-07-12 2020-03-05 株式会社エアロネクスト High-place observation device
CN110869846A (en) * 2017-07-12 2020-03-06 株式会社爱隆未来 High-altitude observation device
EP3654098A4 (en) * 2017-07-12 2021-03-10 Aeronext Inc. High-place observation device
CN110869846B (en) * 2017-07-12 2022-03-22 盐城辉空科技有限公司 High-altitude observation device
CN114397791A (en) * 2017-07-12 2022-04-26 盐城辉空科技有限公司 High-altitude observation device
US11487189B2 (en) 2017-07-12 2022-11-01 Aeronext Inc. High-place observation device including a gas balloon and a detachable rotorcraft
US11774832B2 (en) 2017-07-12 2023-10-03 Aeronext Inc. High-place observation device including an extendable rod-shaped body and a detachable rotorcraft
CN107444629A (en) * 2017-08-11 2017-12-08 广州光使者科技应用有限公司 A kind of unmanned plane electric power system and unmanned plane
TWI641532B (en) * 2017-09-05 2018-11-21 朝陽科技大學 UAV and its flying method and driving device

Similar Documents

Publication Publication Date Title
JP2016037246A (en) Aerial imaging apparatus
US10099782B2 (en) Tethered unmanned aerial vehicle system
US10494121B2 (en) Tethered unmanned aerial vehicle system
US11390369B2 (en) Aircraft
JP3217820U (en) Drone
US11173997B2 (en) Aircraft
JP3204086U (en) Aerial photography device
US10926856B2 (en) Aircraft
JP6213968B2 (en) Shooting unit
WO2019021414A1 (en) Rotary wing aircraft
JP6167273B1 (en) Mooring balloon system
JP6889565B2 (en) Unmanned flight systems, unmanned flight equipment, and landing methods
JP6936508B2 (en) Height observation device
JP6441776B2 (en) A drone with natural and artificial lifts and a line between the ground
KR102328305B1 (en) Apparatus for inspecting LNGC cargo tank using unmaned aerial vehicle
JP2018095371A (en) Crane
WO2016075864A1 (en) Underwater robot
WO2019186621A1 (en) Unmanned aerial vehicle for image capture equipped with suspension device
KR20160081328A (en) autonomous sail-type balloon
KR20190092677A (en) Apparatus for aerial photographing
JP6244271B2 (en) Radio controlled balloon balloon
KR102643026B1 (en) Apparatus and method for controlling aerostat
JP7232719B2 (en) Waterway tunnel inspection device and waterway tunnel inspection device control method
JP2022176425A (en) Unmanned flight vehicle recovery device
JP2023038559A (en) Recovery device of unmanned air vehicle

Legal Events

Date Code Title Description
A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20160107