JP5769850B1 - Moored balloon - Google Patents

Moored balloon Download PDF

Info

Publication number
JP5769850B1
JP5769850B1 JP2014126492A JP2014126492A JP5769850B1 JP 5769850 B1 JP5769850 B1 JP 5769850B1 JP 2014126492 A JP2014126492 A JP 2014126492A JP 2014126492 A JP2014126492 A JP 2014126492A JP 5769850 B1 JP5769850 B1 JP 5769850B1
Authority
JP
Japan
Prior art keywords
balloon
mooring
length
length adjusting
cable
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.)
Active
Application number
JP2014126492A
Other languages
Japanese (ja)
Other versions
JP2016002973A (en
Inventor
潤一 中島
潤一 中島
春弥 宮島
春弥 宮島
藤井 輝也
輝也 藤井
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.)
SoftBank Corp
Original Assignee
SoftBank Mobile Corp
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 SoftBank Mobile Corp filed Critical SoftBank Mobile Corp
Priority to JP2014126492A priority Critical patent/JP5769850B1/en
Application granted granted Critical
Publication of JP5769850B1 publication Critical patent/JP5769850B1/en
Publication of JP2016002973A publication Critical patent/JP2016002973A/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Toys (AREA)

Abstract

【課題】気球が気流を受けたときでも気球の傾きが増大するおそれが低い係留気球を提供する。【解決手段】本発明に係る係留気球1は、気球10と、それぞれの一端が気球10の表面に接続された複数の係留索30〜33と、索長調整部50とを有する。索長調整部50は、気球10が受ける気流の風速に応じて複数の係留索30〜33の何れかの長さを調整する。本発明に係る係留気球10は、気球10の表面に接合されると共に、索長調整部50が長さを調整する係留索に接続される膜状のスクープ20を更に有してもよい。【選択図】図1To provide a moored balloon that is less likely to increase the inclination of the balloon even when the balloon receives an air flow. A mooring balloon 1 according to the present invention includes a balloon 10, a plurality of mooring lines 30 to 33 each having one end connected to the surface of the balloon 10, and a line length adjusting unit 50. The cable length adjusting unit 50 adjusts the length of any of the plurality of mooring cables 30 to 33 according to the wind speed of the airflow received by the balloon 10. The mooring balloon 10 according to the present invention may further include a film-like scoop 20 that is joined to the surface of the balloon 10 and connected to the mooring line whose length is adjusted by the rope length adjusting unit 50. [Selection] Figure 1

Description

本発明は、係留気球に関する。   The present invention relates to a mooring balloon.

災害等で基地局の動作が停止した場合、動作を停止した基地局がカバーしていたエリアでは、携帯電話等の携帯端末の通信ができなくなる通信障害が発生する。通信障害が発生した場合に、動作を停止した基地局を早急に回復して通信障害を解消することが求められる。しかしながら、基地局が倒壊した場合等、基地局の機能を早急に復旧することが困難な場合がある。   When the operation of the base station is stopped due to a disaster or the like, a communication failure that prevents communication of a mobile terminal such as a mobile phone occurs in an area covered by the base station that has stopped the operation. When a communication failure occurs, it is required to quickly recover the base station that has stopped operating to eliminate the communication failure. However, there are cases where it is difficult to quickly restore the functions of the base station, such as when the base station collapses.

一方、気球と、気球を係留するために気球に接続された係留索とを有す係留気球が知られている。係留気球は、風力発電装置等の大型構造物を建設するときの上空の風速調査、風速及び気温等の鉛直分布の調査、及び災害時の被害状況の確認のための映像撮影等に使用されることが知られている。しかしながら、係留気球は、強風を受けると適切な位置を維持できないおそれがある。   On the other hand, a mooring balloon having a balloon and a mooring line connected to the balloon for mooring the balloon is known. Moored balloons are used for surveying the wind speed in the sky when constructing large structures such as wind power generators, surveying the vertical distribution of wind speed and temperature, etc., and taking pictures to check the damage situation at the time of disaster It is known. However, the mooring balloon may not be able to maintain an appropriate position when subjected to strong winds.

特許文献1には、強風を受けた場合でも適切な位置することができる係留気球が記載されている。特許文献1に記載される係留気球は、気球、及び気球に接続された係留索に加えて、気球が強風を受けた場合でも気球が適切な位置を保つように機能するスクープを有する。スクープは、気球が適切な位置を保つのに適切な空気抵抗を気球に付与するように多孔性材料で形成される。   Patent Document 1 describes a mooring balloon that can be positioned appropriately even when subjected to strong winds. The mooring balloon described in Patent Document 1 includes a balloon and a mooring line connected to the balloon, and also has a scoop that functions to keep the balloon in an appropriate position even when the balloon receives a strong wind. The scoop is formed of a porous material so as to provide the balloon with the appropriate air resistance to keep the balloon in place.

米国特許第5065163号明細書US Pat. No. 5,065,163

本願発明者は、災害等で動作を停止した基地局を早急に復旧することが困難な場合に、基地局の機能を代替する中継局を気球に搭載して、動作を停止した基地局がカバーしていたエリアの通信障害を早急に回復することを見出した。中継局を搭載した気球を約100[m]の高度まで上昇させて係留することにより、半径3[km]以上のエリアをカバーする中継局を実現することができる。   The inventor of the present application covers a base station that has stopped operating by installing a relay station that replaces the function of the base station in a balloon when it is difficult to quickly recover the base station that has stopped operating due to a disaster or the like. I found that I could quickly recover from the communication failure in my area. By raising the balloon carrying the relay station to an altitude of about 100 [m] and mooring it, a relay station covering an area with a radius of 3 [km] or more can be realized.

しかしながら、中継局を搭載した気球として扁平形状の気球を使用した場合、気球が気流を受けると、気球が傾くおそれがある。扁平形状の気球は、気球が受ける気流の方向から見た投影面積が所定の面積になることが好ましいが、気流を受けることにより気球の傾きが増大し、気流の方向から見た投影面積が増大する。   However, when a flat balloon is used as a balloon on which a relay station is mounted, the balloon may be tilted when the balloon receives an air current. Flat-shaped balloons preferably have a projected area as seen from the direction of the airflow received by the balloon, but the inclination of the balloon increases by receiving the airflow, and the projected area as seen from the direction of the airflow increases. To do.

本発明は、気球が気流を受けたときでも気球の傾きが増大するおそれが低い係留気球を提供することを目的とする。   An object of the present invention is to provide a moored balloon that is less likely to increase the inclination of the balloon even when the balloon receives airflow.

上記目的を実現するため、本発明に係る係留気球は、内部に気体が充填されたときに扁平形状になる気球と、それぞれの一端が気球の表面に接続された複数の係留索と、気球が受ける気流の風速に応じて、複数の係留索の何れかの長さを調整する索長調整部と、を有することを特徴とする。   In order to achieve the above object, a mooring balloon according to the present invention includes a balloon that becomes flat when gas is filled therein, a plurality of mooring lines each having one end connected to the surface of the balloon, and the balloon A cable length adjusting unit that adjusts the length of any of the plurality of mooring lines according to the wind speed of the received airflow.

本発明に係る係留気球では、索長調整部は、複数の係留索の何れか1つの長さを調整する弾性部材を有することが好ましい。   In the mooring balloon according to the present invention, it is preferable that the rope length adjusting unit includes an elastic member that adjusts the length of any one of the plurality of mooring lines.

本発明に係る係留気球では、弾性部材は、複数の係留索の何れか1つの所定の部分に、弾性部材に張力が印加されていないときの長さが所定の部分の長さよりも短くなるように並列接続されることが好ましい。   In the mooring balloon according to the present invention, the length of the elastic member when any tension is not applied to the elastic member is shorter than the length of the predetermined portion of any one of the plurality of mooring lines. Are preferably connected in parallel.

また、本発明に係る係留気球では、弾性部材は、中空部が内部に形成され、弾性部材に張力が印加されていないときに、並列接続された係留索の所定の部分が中空部に配置されることが好ましい。   In the mooring balloon according to the present invention, the elastic member has a hollow portion formed therein, and when tension is not applied to the elastic member, a predetermined portion of the mooring lines connected in parallel is arranged in the hollow portion. It is preferable.

また、本発明に係る係留気球では、索長調整部は、所定の方向に対する気球の傾斜角を検出する傾斜検出部と、傾斜検出部が検出した傾斜角に応じて、係留索の長さを決定する索長決定部と、索長決定部が決定した長さになるように、係留索の長さを変更する索長変更部と、を有することが好ましい。   Further, in the moored balloon according to the present invention, the rope length adjusting unit detects the inclination angle of the balloon with respect to a predetermined direction, and the length of the mooring line is determined according to the inclination angle detected by the inclination detection unit. It is preferable to have a cable length determining unit to determine and a cable length changing unit to change the length of the mooring cable so as to have the length determined by the cable length determining unit.

また、本発明に係る係留気球は、気球の表面に接合されると共に、索長調整部により長さを調整される係留索に接続される膜状のスクープを更に有することが好ましい。   Moreover, it is preferable that the mooring balloon according to the present invention further includes a film-like scoop that is joined to the surface of the balloon and connected to the mooring line whose length is adjusted by the rope length adjusting unit.

本発明によれば、気球が気流を受けたときでも気球の傾きが増大するおそれが低い係留気球が提供される。   According to the present invention, there is provided a moored balloon that is less likely to increase the inclination of the balloon even when the balloon receives an airflow.

空中に位置する第1実施形態に係る係留気球の斜視図である。It is a perspective view of the mooring balloon which concerns on 1st Embodiment located in the air. (a)は図1に示す気球の部分断面側面図であり、(b)は(a)に示す気球の底面図である。(A) is a partial cross-sectional side view of the balloon shown in FIG. 1, and (b) is a bottom view of the balloon shown in (a). 図1に示すスクープの平面図である。It is a top view of the scoop shown in FIG. 第1実施形態に係る索長調整部材と、索長調整部材が接続された係留索との接続関係を示す図であり、(a)は係留索に張力が印加されていない状態を示す図であり、(b)は係留索に張力が印加されている状態を示す図である。It is a figure which shows the connection relation of the cable length adjustment member which concerns on 1st Embodiment, and the mooring line to which the cable length adjustment member was connected, (a) is a figure which shows the state by which the tension | tensile_strength is not applied to the mooring line. (B) is a figure which shows the state in which the tension | tensile_strength is applied to the mooring cable. 従来の係留気球と、実施形態に係る係留気球との比較を示す図であり、(a)は従来の気球が水平方向から気流をほとんど受けない場合を示し、(b)は(a)のときの気流方向から見た気球の投影面を示し、(c)は従来の気球が水平方向から風速が大きい気流を受けた場合を示し、(d)は(c)のときの気流方向から見た気球の投影面を示し、(e)は気球が水平方向から気流をほとんど受けない場合を示し、(f)は(e)のときの気流方向から見た気球の投影面を示し、(f)は気球が水平方向から風速が大きい気流を受けた場合を示し、(g)は(f)のときの気流方向から見た気球の投影面を示す。It is a figure which shows the comparison with the conventional mooring balloon and the mooring balloon which concerns on embodiment, (a) shows the case where the conventional balloon receives little airflow from a horizontal direction, (b) is the case of (a) 2 shows a projection plane of a balloon viewed from the airflow direction of FIG. 1. (c) shows a case where a conventional balloon receives an airflow with a high wind speed from the horizontal direction, and (d) shows from the airflow direction at (c). The balloon projection plane is shown, (e) shows the case where the balloon receives little airflow from the horizontal direction, (f) shows the balloon projection plane seen from the airflow direction at (e), (f) Indicates a case where the balloon receives an air flow with a high wind speed from the horizontal direction, and (g) indicates a projection plane of the balloon viewed from the air flow direction at (f). 第2実施形態に係る索長調整部材と、索長調整部材が接続された係留索との接続関係を示す図であり、(a)は係留索に張力が印加されていない状態を示す図であり(b)は係留索に張力が印加されている状態を示す図である。It is a figure which shows the connection relation of the cable length adjustment member which concerns on 2nd Embodiment, and the mooring line to which the cable length adjustment member was connected, (a) is a figure which shows the state by which the tension | tensile_strength is not applied to the mooring line. Yes (b) is a diagram showing a state in which tension is applied to the mooring line. 第3実施形態に係る索長調整装置と、索長調整装置が接続された係留索との接続関係を示す図であり、(a)は係留索に張力が印加されていない状態を示す図であり、(b)は係留索に張力が印加されている状態を示す図である。It is a figure which shows the connection relation of the rope length adjustment apparatus which concerns on 3rd Embodiment, and the mooring line to which the rope length adjustment apparatus was connected, (a) is a figure which shows the state in which the tension | tensile_strength is not applied to the mooring line. (B) is a figure which shows the state in which the tension | tensile_strength is applied to the mooring cable. 第4実施形態に係る索長調整システムの機能ブロック図である。It is a functional block diagram of the cable length adjustment system which concerns on 4th Embodiment.

以下の図面を参照して、本発明に係る係留気球について説明する。但し、本発明の技術的範囲はそれらの実施の形態に限定されず、特許請求の範囲に記載された発明との均等物に及ぶ点に留意されたい。   A mooring balloon according to the present invention will be described with reference to the following drawings. However, it should be noted that the technical scope of the present invention is not limited to these embodiments, and extends to equivalents to the invention described in the claims.

実施形態に係る係留気球は、扁平形状の気球が受ける気流の風速にかかわらず、気球の傾斜を一定に保つように、気流の風速に応じて係留索の何れかの長さを調整する索長調整部を有する。索長調整部の一例は複数の係留索の何れか1つの長さを調整する弾性部材であり、索長調整部の他の例は所定の方向に対する気球の傾斜角に応じて係留索の長さを変更する索長調整システムである。実施形態に係る係留気球では、索長調整部が気流の風速に応じて係留索の長さを調整することにより、気球の傾きを一定に保つことができる。   The mooring balloon according to the embodiment adjusts the length of one of the mooring lines according to the wind speed of the airflow so as to keep the inclination of the balloon constant regardless of the wind speed of the airflow received by the flat balloon. It has an adjustment part. One example of the cord length adjusting unit is an elastic member that adjusts the length of any one of a plurality of mooring cords, and another example of the cord length adjusting unit is the length of the mooring cord according to the inclination angle of the balloon with respect to a predetermined direction. It is a cable length adjustment system that changes the height. In the mooring balloon according to the embodiment, the rope length adjusting unit adjusts the length of the mooring line according to the wind speed of the airflow, so that the inclination of the balloon can be kept constant.

図1は、空中に位置する第1実施形態に係る係留気球の斜視図である。   FIG. 1 is a perspective view of a mooring balloon according to a first embodiment located in the air.

係留気球1は、気球10と、スクープ20と、第1〜第3係留索30〜32と、主係留索33と、中継局40と、索長調整部材50とを有する。   The mooring balloon 1 includes a balloon 10, a scoop 20, first to third mooring lines 30 to 32, a main mooring line 33, a relay station 40, and a rope length adjusting member 50.

図2(a)は内部に気体が充填された気球10の部分断面側面図であり、図2(b)は内部に気体が充填された気球10の底面図である。   FIG. 2A is a partial cross-sectional side view of the balloon 10 filled with gas inside, and FIG. 2B is a bottom view of the balloon 10 filled with gas inside.

気球10は、外袋11と、ヘリウム収納袋12と、空気収納袋13と、ペイロード用ドーム14と、3つの係留索取付け部15とを有する。気球10は、ヘリウム収納袋12及び空気収納袋13と外袋11との二重構造となっているので、外袋11は、ガスバリア性を有する材料で形成される必要はない。外袋11は、合成繊維等の堅固、軽量且つ風を通さない材料で形成される。ヘリウム収納袋12は、ヘリウムを充填する袋であり、外袋11と比較して強度及び耐久性が低く且つ軽量な材料により形成される。例えば、ヘリウム収納袋12は、プラスチックフィルムを溶着することにより形成される。空気収納袋13は、外袋11と比較して強度及び耐久性が低く且つ軽量な材料により形成される。空気収納袋13は、ヘリウム収納袋12と同様に、プラスチックフィルムを溶着することにより形成される。ペイロード用ドーム14は、有底の円筒状の部材であり、底部が空気収納袋13に接するように配置される。ペイロード用ドーム14は、発泡スチロール等の堅固且つ軽量な素材により形成される。ペイロード用ドーム14の凹部には、中継局40が配置される。   The balloon 10 includes an outer bag 11, a helium storage bag 12, an air storage bag 13, a payload dome 14, and three mooring line attachment portions 15. Since the balloon 10 has a double structure of the helium storage bag 12 and the air storage bag 13 and the outer bag 11, the outer bag 11 does not need to be formed of a material having gas barrier properties. The outer bag 11 is formed of a rigid, lightweight and air-tight material such as synthetic fiber. The helium storage bag 12 is a bag filled with helium, and is formed of a material that is lower in strength and durability than the outer bag 11 and is light in weight. For example, the helium storage bag 12 is formed by welding a plastic film. The air storage bag 13 is made of a lightweight material that has lower strength and durability than the outer bag 11. Similar to the helium storage bag 12, the air storage bag 13 is formed by welding a plastic film. The payload dome 14 is a cylindrical member with a bottom, and is arranged so that the bottom is in contact with the air storage bag 13. The payload dome 14 is made of a rigid and lightweight material such as polystyrene foam. A relay station 40 is disposed in the concave portion of the payload dome 14.

気球10は、ヘリウム収納袋12にヘリウムが充填され且つ空気収納袋13に空気が充填されているとき、高さ方向に短軸を有する回転楕円体状の形状を有する。すなわち、内部に気体が充填されているとき、気球10は、円形状の平面形状を有し且つ楕円状の正面形状を有する扁平形状となる。一例では、気球10は、直径4.6[m]の円状の平面形状を有し且つ、長径4.6[m]、短径2.66[m]の楕円状の正面形状を有する。   The balloon 10 has a spheroid shape having a minor axis in the height direction when the helium storage bag 12 is filled with helium and the air storage bag 13 is filled with air. That is, when the inside is filled with gas, the balloon 10 has a flat shape having a circular plane shape and an elliptical front shape. In one example, the balloon 10 has a circular planar shape with a diameter of 4.6 [m], and an elliptical front shape with a major axis of 4.6 [m] and a minor axis of 2.66 [m].

3つの係留索取付け部15は、正面から見たときに長径に沿うように気球10の表面に配置される。3つの係留索取付け部15のそれぞれは、第1〜第3係留索30〜32の何れか1つの一端に接続される。スクープ20が接合される部分に近接する位置に配置される係留索取付け部15には第1係留索30の一端が接続され、他の2つの係留索取付け部15には、第2係留索31及び第3係留索32の一端がそれぞれ接続される。   The three mooring line attachment portions 15 are arranged on the surface of the balloon 10 so as to follow the long diameter when viewed from the front. Each of the three mooring line attachment portions 15 is connected to one end of any one of the first to third mooring lines 30 to 32. One end of the first mooring line 30 is connected to the mooring line attachment part 15 arranged at a position close to the part to which the scoop 20 is joined, and the second mooring line 31 is connected to the other two mooring line attachment parts 15. And one end of the 3rd mooring line 32 is connected, respectively.

図3は、スクープ20の平面図である。   FIG. 3 is a plan view of the scoop 20.

スクープ20は、一方の面から他方の面に空気を透過するように編み込まれたポリエステルにより形成される可とう性の面21を有する膜材である。スクープ20は、姿勢安定膜とも称される。スクープ20は、底辺23と、底辺23の反対に位置する頂角28で一端が接続された第1等辺24及び第2等辺25と、底辺23の両端から第1等辺24及び第2等辺25の他端にそれぞれ伸びる第1切欠辺26及び第2切欠辺27とにより囲まれた形状を有する。第1等辺24及び第2等辺25は互いに長さが等しく、第1切欠辺26及び第2切欠辺27は互いに長さが等しい。すなわち、スクープ20は、底角部分が切欠された二等辺三角形状に形成される。スクープ20の底辺23、第1切欠辺26及び第2切欠辺27のそれぞれの近傍で、気球10に接合される。スクープ20の頂角28には、スクープ20と第1係留索30とを接続する接続索29が接続される。スクープ20の頂角28と第1係留索30とが接続索29を介して接続されることにより、係留気球1が空中に上げられたときに、ヨットの帆のようにスクープ20が風を受けて、係留気球1は、スクープ20が風下となるように風見安定する。   The scoop 20 is a film material having a flexible surface 21 formed of polyester woven so as to transmit air from one surface to the other surface. The scoop 20 is also referred to as a posture stabilizing film. The scoop 20 includes a base 23, a first equilateral side 24 and a second equilateral side 25 connected at one end at an apex angle 28 positioned opposite to the base 23, and a first equilateral side 24 and a second equilateral side 25 from both ends of the base 23. It has a shape surrounded by a first cutout side 26 and a second cutout side 27 that extend to the other end. The first equal side 24 and the second equal side 25 are equal in length to each other, and the first cut-out side 26 and the second cut-out side 27 are equal in length to each other. That is, the scoop 20 is formed in an isosceles triangle shape with a base corner portion notched. The scoop 20 is joined to the balloon 10 in the vicinity of the base 23, the first cut-out side 26, and the second cut-out side 27. A connection line 29 that connects the scoop 20 and the first mooring line 30 is connected to the apex angle 28 of the scoop 20. By connecting the apex angle 28 of the scoop 20 and the first mooring line 30 via the connection line 29, when the mooring balloon 1 is raised in the air, the scoop 20 receives wind like a sail of a yacht. Thus, the mooring balloon 1 is stabilized in the wind so that the scoop 20 becomes leeward.

第1〜第3係留索30〜32のそれぞれは、係留気球1が空中にあるときに受ける気流による張力で切断されない材料で形成される。第1係留索30の一端はスクープ20が接合される部分に近接する位置に配置される係留索取付け部15に接続され、第2係留索31及び第3係留索32のそれぞれの一端は他の2つの係留索取付け部15に接続される。第1〜第3係留索30〜32のそれぞれの他端は、結節点34において、主係留索33の一端と接続される。一例では、結節点34における第1〜第3係留索30〜32のそれぞれの他端と主係留索33の一端とは、接続金具を介して接続される。第1係留索30は、スクープ20の頂角と接続索29を介して接続される。一例では、第1係留索30と接続索29とは、接続金具を介して接続される。   Each of the first to third mooring lines 30 to 32 is formed of a material that is not cut by the tension caused by the airflow received when the mooring balloon 1 is in the air. One end of the first mooring line 30 is connected to the mooring line attaching part 15 disposed at a position close to the portion where the scoop 20 is joined, and one end of each of the second mooring line 31 and the third mooring line 32 is the other. Connected to the two mooring line attachment portions 15. The other ends of the first to third mooring lines 30 to 32 are connected to one end of the main mooring line 33 at the node 34. In one example, the other end of each of the first to third mooring lines 30 to 32 at the node 34 and one end of the main mooring line 33 are connected via a connection fitting. The first mooring line 30 is connected to the apex angle of the scoop 20 via the connection line 29. In one example, the first mooring line 30 and the connection line 29 are connected via a connection fitting.

第1係留索30の長さは、第2係留索31及び第3係留索32の長さよりも長く、第2係留索31及び第3係留索32の長さは互いに等しい。   The length of the first mooring line 30 is longer than the lengths of the second mooring line 31 and the third mooring line 32, and the lengths of the second mooring line 31 and the third mooring line 32 are equal to each other.

主係留索33は、第1〜第3係留索30〜32と同様に、係留気球1が空中にあるときに受ける気流による張力で切断されない材料で形成される。主係留索33の他端は、不図示のウインチに接続される。主係留索33の他端に接続されるウインチから主係留索33が巻き出されるとき、係留気球1は巻出量に応じて空中に上昇し、ウインチから主係留索33が巻き取られるとき、係留気球1は巻取量に応じて空中から下降する。   Similar to the first to third mooring lines 30 to 32, the main mooring line 33 is formed of a material that is not cut by the tension caused by the airflow received when the mooring balloon 1 is in the air. The other end of the main mooring line 33 is connected to a winch (not shown). When the main mooring line 33 is unwound from the winch connected to the other end of the main mooring line 33, the mooring balloon 1 rises in the air according to the unwinding amount, and when the main mooring line 33 is wound from the winch, The mooring balloon 1 descends from the air according to the winding amount.

中継局40は、不図示の中継用アンテナ及び対移動局用アンテナを有し、移動体通信網に接続される基地局と、基地局がカバーしていたエリア内に位置する携帯端末との間の通信網を形成する。   The relay station 40 has a relay antenna and a mobile station antenna (not shown), and is between a base station connected to the mobile communication network and a mobile terminal located in an area covered by the base station. A communication network.

索長調整部材50は、第1係留索30の結節点34の近接する位置に第1係留索30の一部と並列するように接続される弾性部材である。一例では、索長調整部材50は、平ゴム又はコールゴムとも称される平板状のゴムひもから形成されてよく、またバネから形成されてもよい。   The cord length adjusting member 50 is an elastic member that is connected to a position near the node 34 of the first mooring line 30 so as to be parallel to a part of the first mooring line 30. In one example, the cord length adjusting member 50 may be formed of a flat rubber string also called flat rubber or coal rubber, or may be formed of a spring.

図4は、第1係留索30と、索長調整部材50との接続関係を示す図である。図4(a)は第1係留索30に張力が印加されていない状態を示す図であり、図4(b)は第1係留索30に張力が印加されている状態を示す図である。   FIG. 4 is a diagram showing a connection relationship between the first mooring line 30 and the line length adjusting member 50. FIG. 4A is a diagram showing a state in which no tension is applied to the first mooring line 30, and FIG. 4B is a diagram showing a state in which a tension is applied to the first mooring line 30.

索長調整部材50は、第1接続部51及び第2接続部52において第1係留索30と並列接続される。索長調整部材50は、第1係留索30と並列接続されるので、第1係留索30に張力が印加されると、索長調整部材50にも張力が印加される。張力が印加されていないときの索長調整部材50の第1接続部51と第2接続部52との間の長さはLaである。また、第1係留索30の第1接続部51及び第2接続部52の間の長さは、索長調整部材50の第1接続部51及び第2接続部52の間の長さLaよりも長いLbである。張力が印加されていないときの索長調整部材50の接続部間の長さLaは、第1係留索30の接続部間の長さLbよりも短いので、張力が印加されていないとき、第1係留索30の接続部間の部分は弛んでいる。   The cable length adjusting member 50 is connected in parallel to the first mooring cable 30 at the first connection part 51 and the second connection part 52. Since the rope length adjusting member 50 is connected in parallel with the first mooring line 30, when a tension is applied to the first mooring line 30, the tension is also applied to the rope length adjusting member 50. The length between the 1st connection part 51 and the 2nd connection part 52 of the cable length adjustment member 50 when tension is not applied is La. Further, the length between the first connection portion 51 and the second connection portion 52 of the first mooring line 30 is longer than the length La between the first connection portion 51 and the second connection portion 52 of the rope length adjusting member 50. Is also a long Lb. Since the length La between the connecting portions of the cable length adjusting member 50 when no tension is applied is shorter than the length Lb between the connecting portions of the first mooring cable 30, when the tension is not applied, The part between the connection parts of the 1 mooring line 30 is slack.

索長調整部材50の接続部間の長さLaは、気球10が気流を受けていないときに、係留索取付け部15と第1接続部51との間の長さ及び結節点34と第2接続部52との間の長さとの和が第2係留索31及び第3係留索32の長さと等しくなるように規定される。第1係留索30の接続部間の長さLbは、所定の風速の気流を気球10が受けたときの索長調整部材50の伸びが所望の長さになるように、索長調整部材50を形成する材料のヤング率を勘案して規定される。一例では、第1係留索30の接続部間の長さLbは、気球10が風速5[m/s]の気流を水平方向から受けたときに、気球10の長径の方向が水平方向になるように規定される。本明細書において、気球が水平方向から気流を受けるというとき、気球が受ける気流が水平成分を有していることをいい、気球が水平方向から気球を受けないというとき、気球が受ける気流が水平成分を有していないことをいう。また、気球が風速X[m/s]の気流を水平方向から受けるという場合、気流の方向にかかわらず、気球が受ける気流の水平成分がX[m/s]であることをいう。   The length La between the connecting portions of the rope length adjusting member 50 is the length between the mooring rope attaching portion 15 and the first connecting portion 51 and the second connecting point 34 and the second when the balloon 10 is not receiving airflow. The sum of the length between the connecting portion 52 and the connecting portion 52 is defined to be equal to the length of the second mooring line 31 and the third mooring line 32. The length Lb between the connecting portions of the first mooring line 30 is set so that the length of the line length adjusting member 50 becomes a desired length when the balloon 10 receives an air flow at a predetermined wind speed. It is defined in consideration of the Young's modulus of the material forming the film. In one example, the length Lb between the connecting portions of the first mooring line 30 is such that when the balloon 10 receives an air flow with a wind speed of 5 [m / s] from the horizontal direction, the major axis direction of the balloon 10 becomes the horizontal direction. It is prescribed as follows. In this specification, when the balloon receives airflow from the horizontal direction, it means that the airflow received by the balloon has a horizontal component, and when the balloon does not receive the balloon from the horizontal direction, the airflow received by the balloon is horizontal. It means having no ingredients. In addition, when the balloon receives an airflow of wind speed X [m / s] from the horizontal direction, it means that the horizontal component of the airflow received by the balloon is X [m / s] regardless of the direction of the airflow.

気球10が受ける気流により印加される張力が増加するとき、索長調整部材50は、印加される張力に応じて長さを長くする。そして、索長調整部材50の長さが、第1係留索30の第1接続部51と第2接続部52との間の長さLbに等しくなると、印加される張力が増加しても、索長調整部材50の長さは増加しない。また、気球10が受ける気流により印加される張力が減少するとき、索長調整部材50は、印加される張力に応じて長さをLbから短くする。そして、印加される張力が0になると、索長調整部材50の長さはLaに戻る。   When the tension applied by the airflow received by the balloon 10 increases, the cord length adjusting member 50 increases the length according to the applied tension. And if the length of the cord length adjusting member 50 becomes equal to the length Lb between the first connecting portion 51 and the second connecting portion 52 of the first mooring cord 30, even if the applied tension increases, The length of the cord length adjusting member 50 does not increase. Further, when the tension applied by the air flow received by the balloon 10 decreases, the cord length adjusting member 50 shortens the length from Lb according to the applied tension. When the applied tension becomes zero, the length of the cord length adjusting member 50 returns to La.

図5は、従来の係留気球と、実施形態に係る係留気球1との比較を示す図である。図5(a)は従来の気球が水平方向から気流をほとんど受けない場合を示し、図5(b)は図5(a)のときの気流方向から見た気球の投影面を示す図である。図5(c)は従来の気球が水平方向から風速が大きい気流を受けた場合を示し、図5(d)は図5(c)のときの気流方向から見た気球の投影面を示す図である。図5(e)は気球10が水平方向から気流をほとんど受けない場合を示し、図5(f)は図5(e)のときの気流方向から見た気球10の投影面を示す図である。図5(f)は気球10が水平方向から風速が大きい気流を受けた場合を示し、図5(g)は図5(f)のときの気流方向から見た気球10の投影面を示す図である。図5(a)、5(c)、5(e)及び5(g)において、矢印は気球が受ける気流を示す。図5(d)において、実線は図5(c)のときの気流方向から見た気球の投影面を示し、破線は図5(b)に示す図5(a)のときの気流方向から見た気球の投影面を示す。図5(h)において、実線は図5(g)のときの気流方向から見た気球10の投影面を示し、破線は図5(f)に示す図5(e)のときの気流方向から見た気球の投影面を示す。   FIG. 5 is a diagram showing a comparison between the conventional mooring balloon and the mooring balloon 1 according to the embodiment. FIG. 5A shows a case where a conventional balloon receives almost no airflow from the horizontal direction, and FIG. 5B shows a projection plane of the balloon viewed from the airflow direction in FIG. 5A. . FIG. 5 (c) shows a case where a conventional balloon receives an air flow having a high wind speed from the horizontal direction, and FIG. 5 (d) shows a projection plane of the balloon viewed from the air flow direction in FIG. 5 (c). It is. FIG. 5E shows a case where the balloon 10 receives almost no airflow from the horizontal direction, and FIG. 5F shows a projection plane of the balloon 10 viewed from the airflow direction in FIG. . FIG. 5 (f) shows a case where the balloon 10 receives an air flow having a high wind speed from the horizontal direction, and FIG. 5 (g) shows a projection plane of the balloon 10 viewed from the air flow direction in FIG. 5 (f). It is. 5 (a), 5 (c), 5 (e), and 5 (g), the arrows indicate the airflow received by the balloon. In FIG. 5 (d), the solid line shows the projection plane of the balloon viewed from the airflow direction in FIG. 5 (c), and the broken line shows from the airflow direction in FIG. 5 (a) shown in FIG. 5 (b). Shows the projection plane of the balloon. In FIG. 5 (h), the solid line indicates the projection plane of the balloon 10 viewed from the airflow direction in FIG. 5 (g), and the broken line indicates the airflow direction in FIG. 5 (e) shown in FIG. 5 (f). Shows the projected plane of the balloon.

従来の係留気球101は、索長調整部材50を有しないことが係留気球1と相違する。また、従来の係留気球101は、第1〜第3係留索130〜132の長さは互いに等しいことが係留気球1と相違する。   The conventional mooring balloon 101 is different from the mooring balloon 1 in that it does not have the cord length adjusting member 50. The conventional mooring balloon 101 differs from the mooring balloon 1 in that the first to third mooring lines 130 to 132 are equal in length.

従来の係留気球101は、第1〜第3係留索130〜132の長さは互いに等しいので、水平方向から気流をほとんど受けないとき、気球110は長径が水平方向になるように位置する。水平方向から気流をほとんど受けないときは、長径が水平方向になるように気球110が位置するので、気流方向から見た気球10の投影面190は、気球10を正面から見たときの投影面と略一致する。しかしながら、従来の繋留気球101は、水平方向から受ける気流の風速が大きくなるに従ってスクープ20が受ける気流が大きくなるため傾斜していき、気流の風速の増加に従って気流方向から見た気球110の投影面191は大きくなる。   In the conventional mooring balloon 101, the lengths of the first to third mooring lines 130 to 132 are equal to each other, so that the balloon 110 is positioned so that the major axis is in the horizontal direction when receiving almost no airflow from the horizontal direction. When the airflow is hardly received from the horizontal direction, the balloon 110 is positioned so that the major axis is in the horizontal direction. Therefore, the projection plane 190 of the balloon 10 viewed from the airflow direction is a projection plane when the balloon 10 is viewed from the front. Is approximately the same. However, the conventional tethered balloon 101 is inclined because the airflow received by the scoop 20 increases as the wind speed of the airflow received from the horizontal direction increases, and the projection plane of the balloon 110 viewed from the airflow direction as the wind speed of the airflow increases. 191 becomes larger.

係留気球1では、水平方向から気流をほとんど受けないとき、従来の繋留気球101と同様に、気球110は長径が水平方向になるように位置し、気流方向から見た気球10の投影面90は、気球10を正面から見たときの投影面と略一致する。係留気球1では、水平方向から受ける気流の風速が大きくなるに従って、索長調整部材50が伸びることにより、気球10は、索長調整部材50の第1接続部51と第2接続部52との間の長さがLbになるまで気球110は長径が水平方向になる状態を維持する。係留気球1では、気球10は、気流の風速が大きくなっても長径が水平方向になる状態を維持するので気流方向から見た気球10の投影面91は、気流の風速が大きくなっても気球10を正面から見たときの投影面と略一致する。   When the mooring balloon 1 receives almost no airflow from the horizontal direction, the balloon 110 is positioned so that the major axis is in the horizontal direction, like the conventional tethered balloon 101, and the projection plane 90 of the balloon 10 viewed from the airflow direction is , Substantially coincides with the projection plane when the balloon 10 is viewed from the front. In the mooring balloon 1, the rope length adjustment member 50 extends as the wind speed of the airflow received from the horizontal direction increases, so that the balloon 10 is connected to the first connection portion 51 and the second connection portion 52 of the rope length adjustment member 50. The balloon 110 maintains the state where the major axis is in the horizontal direction until the length between them becomes Lb. In the mooring balloon 1, the balloon 10 maintains a state in which the major axis is in the horizontal direction even when the wind speed of the air current increases. Therefore, the projection surface 91 of the balloon 10 viewed from the air flow direction is the balloon even if the wind speed of the air current increases. 10 substantially coincides with the projection plane when viewed from the front.

係留気球1では、気球10が受ける気流の風速が大きくなるに従って伸びる索長調整部材50が、スクープ20に接続される第1係留索30の所定の部分に並列接続される。気流の風速が大きくなるに従って索長調整部材50が伸びることにより、気球10は、気球10が受ける気流の風速にかかわらず一定の傾斜を維持できる。   In the mooring balloon 1, the cord length adjusting member 50 that extends as the wind speed of the airflow received by the balloon 10 increases is connected in parallel to a predetermined portion of the first mooring line 30 connected to the scoop 20. The rope length adjustment member 50 extends as the wind speed of the air current increases, so that the balloon 10 can maintain a constant inclination regardless of the wind speed of the air current received by the balloon 10.

図6は、第2実施形態に係る索長調整部材と、索長調整部材が接続された第1係留索30との接続関係を示す図である。図6(a)は第1係留索30に張力が印加されていない状態を示す図であり、図6(b)は第1係留索30に張力が印加されている状態を示す図である。   FIG. 6 is a diagram illustrating a connection relationship between the cable length adjusting member according to the second embodiment and the first mooring cable 30 to which the cable length adjusting member is connected. FIG. 6A is a view showing a state in which no tension is applied to the first mooring line 30, and FIG. 6B is a view showing a state in which a tension is applied to the first mooring line 30.

第2実施形態では、索長調整部材50の代わりに、索長調整部材50とは形状が異なる索長調整部材60が第1係留索30に並列接続される。   In the second embodiment, instead of the cable length adjusting member 50, a cable length adjusting member 60 having a shape different from that of the cable length adjusting member 50 is connected in parallel to the first mooring cable 30.

第2実施形態に係る索長調整部材60は、索長調整部材50と同様に弾性部材であるが、一方の面から他方の面に貫通する貫通孔61が形成されることが索長調整部材50と相違する。第1係留索30は、貫通孔61の一方の貫通面の近傍で索長調整部材60に接続されると共に、索長調整部材50の貫通孔61には、第1係留索30の索長調整部材60に並列接続される部分が貫通孔61の端部で索長調整部材60に接続されて配置される。張力が印加されていないときの索長調整部材60の長さはLaであり、第1係留索30の索長調整部材60に並列接続される部分の長さはLbである。索長調整部材50の長さLaは、索長調整部材50の接続部間の長さLaと同様に、気球10が気流を受けていないときの索長調整部材60を介する第1係留索30の長さが第2係留索31及び第3係留索32の長さと等しくなるように規定される。第1係留索30の索長調整部材60に並列接続される部分の長さLbは、第1係留索30の接続部間の長さLbと同様に、索長調整部材50を形成する材料のヤング率を勘案して規定される。   The cord length adjusting member 60 according to the second embodiment is an elastic member, like the cord length adjusting member 50, but the cord length adjusting member is formed with a through hole 61 penetrating from one surface to the other surface. 50. The first mooring line 30 is connected to the line length adjusting member 60 in the vicinity of one through surface of the through hole 61, and the line length adjustment of the first mooring line 30 is inserted into the through hole 61 of the line length adjusting member 50. A portion connected in parallel to the member 60 is connected to the cord length adjusting member 60 at the end of the through hole 61 and arranged. The length of the cord length adjusting member 60 when no tension is applied is La, and the length of the portion of the first mooring cord 30 connected in parallel to the cord length adjusting member 60 is Lb. The length La of the cord length adjusting member 50 is the same as the length La between the connecting portions of the cord length adjusting member 50, and the first mooring cord 30 via the cord length adjusting member 60 when the balloon 10 is not receiving airflow. Is defined to be equal to the lengths of the second mooring line 31 and the third mooring line 32. The length Lb of the portion connected in parallel to the cable length adjusting member 60 of the first mooring line 30 is the same as the length Lb between the connecting parts of the first mooring cable 30 and is made of the material forming the cable length adjusting member 50. It is defined in consideration of Young's modulus.

索長調整部材60では、第1係留索30の索長調整部材60に並列接続される部分が貫通孔61の内部に配置されるので、第1係留索30の索長調整部材60に並列接続される部分が他の索等に絡まるおそれがない。また、索長調整部材60では、不図示のウインチに巻き取されて気球10を空中から下降するときに、第1係留索30の索長調整部材60に並列接続される部分がウインチに巻き込まれるおそれはない。   In the rope length adjusting member 60, a portion connected in parallel to the rope length adjusting member 60 of the first mooring line 30 is disposed inside the through hole 61, so that it is connected in parallel to the rope length adjusting member 60 of the first mooring line 30. There is no fear that the part to be entangled with other cords. Further, in the rope length adjusting member 60, when the balloon 10 is wound down by a winch (not shown) and the balloon 10 is lowered from the air, a portion connected in parallel to the rope length adjusting member 60 of the first mooring line 30 is caught in the winch. There is no fear.

索長調整部材60では、一方の面から他方の面に貫通する貫通孔61が形成されるが、実施形態は、貫通孔61には限定されず、第1係留索30の索長調整部材60に並列接続される部分が配置される空間が索長調整部材60の内部に形成されていればよい。   In the rope length adjusting member 60, a through hole 61 penetrating from one surface to the other surface is formed, but the embodiment is not limited to the through hole 61, and the rope length adjusting member 60 of the first mooring line 30 is formed. It is only necessary that a space in which a portion connected in parallel is arranged in the cord length adjusting member 60.

図7は、第3実施形態に係る索長調整装置と、索長調整装置が接続された第1係留索30との接続関係を示す図である。図7(a)は第1係留索30に張力が印加されていない状態を示す図であり、図7(b)は第1係留索30に張力が印加されている状態を示す図である。   FIG. 7 is a diagram illustrating a connection relationship between the cable length adjusting device according to the third embodiment and the first mooring cable 30 to which the cable length adjusting device is connected. FIG. 7A is a view showing a state in which no tension is applied to the first mooring line 30, and FIG. 7B is a view showing a state in which a tension is applied to the first mooring line 30.

第3実施形態では、索長調整部材50の代わりに、索長調整装置70が第1係留索30に接続される。   In the third embodiment, a cable length adjusting device 70 is connected to the first mooring cable 30 instead of the cable length adjusting member 50.

索長調整装置70は、第1係留索30に接合される円形の回転部71を有する。回転部71は、第1係留索30の長さを調整するように機能するぜんまいばね72を有する。回転部71は、印加される張力が増加すると、外周に巻き回された第1係留索30を巻き出す。また、回転部71は、印加される張力が減少すると、外周に巻き回して第1係留索30を巻き取る。索長調整装置70は、張力が印加されていないとき、第1係留索30の長さが第2係留索31及び第3係留索32の長さと等しくなるように、第1係留索30を回転部71の外周に巻き回す。   The cable length adjusting device 70 has a circular rotating part 71 joined to the first mooring cable 30. The rotating portion 71 has a mainspring spring 72 that functions to adjust the length of the first mooring line 30. When the applied tension increases, the rotating unit 71 unwinds the first mooring line 30 wound around the outer periphery. Moreover, when the tension | tensile_strength applied reduces, the rotation part 71 winds around the outer periphery and winds up the 1st mooring line 30. FIG. The rope length adjusting device 70 rotates the first mooring line 30 so that the length of the first mooring line 30 is equal to the length of the second mooring line 31 and the third mooring line 32 when no tension is applied. It is wound around the outer periphery of the part 71.

図8は、第4実施形態に係る索長調整システムの機能ブロック図である。   FIG. 8 is a functional block diagram of a cable length adjustment system according to the fourth embodiment.

第4実施形態では、索弾性部材である索長調整部材50の代わりに、気球10の傾斜角に応じて第1係留索30の長さを調整する索長調整システム80が配置される。   In the fourth embodiment, a cable length adjusting system 80 that adjusts the length of the first mooring cable 30 according to the inclination angle of the balloon 10 is arranged instead of the cable length adjusting member 50 that is a cable elastic member.

索長調整システム80は、中継局40に隣接して気球10のペイロード用ドーム14の凹部に配置される索長制御部81と、第1係留索30を巻き出すと共に巻き取ることにより、第1係留索30の長さを変更する索長変更部82とを有する。索長制御部81は、傾斜検出部811と、記憶部812と、索長決定部813と、索長送信部814と、バス815とを有する。索長変更部82は索長受信部821と、モータ駆動部822と、モータ823とを有する。一例では、索長変更部82は、モータ823により第1係留索30を巻き出すと共に巻き取るウインチである。   The cable length adjusting system 80 unwinds and winds the cable length control unit 81 disposed in the concave portion of the payload dome 14 of the balloon 10 adjacent to the relay station 40 and the first mooring cable 30. A cable length changing unit 82 for changing the length of the mooring cable 30; The cable length control unit 81 includes an inclination detection unit 811, a storage unit 812, a cable length determination unit 813, a cable length transmission unit 814, and a bus 815. The cable length changing unit 82 includes a cable length receiving unit 821, a motor driving unit 822, and a motor 823. In one example, the cable length changing unit 82 is a winch that unwinds and winds the first mooring cable 30 by the motor 823.

傾斜検出部811は、気球10の水平方向に対する傾斜角を検出し、検出した傾斜角を示す傾斜角信号を記憶部812に出力する。記憶部812は、傾斜検出部811から入力される傾斜角信号に対応する傾斜角を記憶すると共に、索長決定部813が処理を実行するためのコンピュータプログラム(本明細書では、プログラムとも称する)を記憶する。索長決定部813は、記憶部812に記憶されるプログラム及び気球の傾斜角に基づいて、気球10の長径の方向が水平方向になるように第1係留索30を巻き出す又は巻き取る長さを決定し、決定した長さを示す索長信号を生成して、索長送信部814に出力する。索長送信部814は、索長決定部813から入力された索長信号を無線信号に変調して、索長変更部82の索長受信部821に送信する。バス815は、傾斜検出部811、記憶部812、索長決定部813及び索長送信部814を互いに接続し、傾斜検出部811、記憶部812、索長決定部813及び索長送信部814の間の信号を伝送する。   The tilt detection unit 811 detects the tilt angle of the balloon 10 with respect to the horizontal direction, and outputs a tilt angle signal indicating the detected tilt angle to the storage unit 812. The storage unit 812 stores a tilt angle corresponding to the tilt angle signal input from the tilt detection unit 811 and a computer program (also referred to as a program in this specification) for the rope length determination unit 813 to execute processing. Remember. The rope length determining unit 813 is a length for unwinding or winding the first mooring cable 30 so that the major axis direction of the balloon 10 is horizontal, based on the program stored in the storage unit 812 and the inclination angle of the balloon. Is determined, and a cable length signal indicating the determined length is generated and output to the cable length transmitter 814. The cable length transmitting unit 814 modulates the cable length signal input from the cable length determining unit 813 into a radio signal, and transmits the radio signal to the cable length receiving unit 821 of the cable length changing unit 82. The bus 815 connects the inclination detection unit 811, the storage unit 812, the cable length determination unit 813, and the cable length transmission unit 814 to each other, and the inclination detection unit 811, the storage unit 812, the cable length determination unit 813, and the cable length transmission unit 814. Transmit signals between.

索長受信部821は、索長送信部814から受信した無線信号を索長信号に復調してモータ駆動部822に出力する。モータ駆動部822は、索長送信部814から入力された索長信号に対応する長さの第1係留索30を巻き出す又は巻き取るように、モータ823を駆動する。モータ823は、気球10の長径の方向が水平方向になるようにモータ駆動部822により第1係留索30を巻き出す又は巻き取る。   The cable length receiving unit 821 demodulates the radio signal received from the cable length transmitting unit 814 into a cable length signal and outputs the signal to the motor driving unit 822. The motor drive unit 822 drives the motor 823 so as to unwind or wind up the first mooring line 30 having a length corresponding to the line length signal input from the line length transmission unit 814. The motor 823 unwinds or winds up the first mooring line 30 by the motor driving unit 822 so that the direction of the major axis of the balloon 10 is horizontal.

索長調整システム80では、索長決定部813は傾斜検出部811が検出した傾斜角に応じて第1係留索30の長さを決定し、索長変更部82は、第1係留索30の長さが、索長決定部813が決定した長さになるように係留索の長さを変更する。   In the cable length adjusting system 80, the cable length determining unit 813 determines the length of the first mooring line 30 according to the inclination angle detected by the inclination detecting unit 811, and the cable length changing unit 82 is used for the first mooring line 30. The length of the mooring line is changed so that the length becomes the length determined by the cable length determination unit 813.

索長調整システム80では、スクープ20に接続される第1係留索30の長さを変更するように形成されるが、索長調整システムは、第1係留索30ではなく、第2係留索31及び第3係留索32の長さを変更するように形成してもよい。また、索長調整システムは、第1係留索30、第2係留索31及び第3係留索32の3本の繋留索全ての長さを変更するように形成してもよい。   The cable length adjusting system 80 is formed so as to change the length of the first mooring line 30 connected to the scoop 20, but the cable length adjusting system is not the first mooring line 30 but the second mooring line 31. And you may form so that the length of the 3rd mooring line 32 may be changed. Moreover, you may form a rope length adjustment system so that the length of all the 3 mooring lines of the 1st mooring line 30, the 2nd mooring line 31, and the 3rd mooring line 32 may be changed.

実施形態に係る係留気球では、気球10が受ける気流の風速にかかわらず水平方向から受ける気流に対して一定の傾斜を維持できるので、気流に対する気球10の投影面積は略変化しない。実施形態に係る係留気球では、水平方向から受ける気流に対する気球10の投影面積は略変化しないので、気球10が受ける気流の風速にかかわらず、気球10の姿勢を最適な状態に維持できるので、突風が吹いたときの気球10の姿勢の変動を小さくできる。また、実施形態に係る係留気球では、気球10が受ける気流の風速にかかわらず、気球10の姿勢を最適な状態に維持できるので、気球10が空中にあるときの見た目の不安定感がなくなる。なお、実施形態に係る係留気球では、扁平形状の気球10は、気球10が水平方向から受ける気流の風速が5[m/s]を超えると20[m/s]まで水平方向から略一定の傾斜で風見安定することが確認されている。   In the moored balloon according to the embodiment, since a constant inclination can be maintained with respect to the airflow received from the horizontal direction regardless of the wind speed of the airflow received by the balloon 10, the projected area of the balloon 10 with respect to the airflow is not substantially changed. In the moored balloon according to the embodiment, since the projected area of the balloon 10 with respect to the airflow received from the horizontal direction does not substantially change, the attitude of the balloon 10 can be maintained in an optimum state regardless of the wind speed of the airflow received by the balloon 10. The change in the posture of the balloon 10 when the balloon blows can be reduced. Further, in the moored balloon according to the embodiment, the posture of the balloon 10 can be maintained in an optimum state regardless of the wind speed of the airflow received by the balloon 10, so that there is no apparent instability when the balloon 10 is in the air. In the moored balloon according to the embodiment, the flat-shaped balloon 10 is substantially constant from the horizontal direction up to 20 [m / s] when the wind speed of the airflow received by the balloon 10 from the horizontal direction exceeds 5 [m / s]. It has been confirmed that the weather is stable with inclination.

実施形態に係る係留気球では、索長調整部材50、60、索長調整装置70及び索長調整システム80は、気球10が気球10の長径の方向が水平方向になるように機能する。しかしながら、索長調整部材50、60、索長調整装置70及び索長調整システム80は、気球が気球10の長径の方向が水平方向に対して所定の傾斜を有するようにしてもよい。例えば、索長調整部材50の接続部間の長さLaを、気球10が気流を受けていないときの索長調整部材50を介する第1係留索30の長さが第2係留索31及び第3係留索32の長さより短くするように規定してもよい。索長調整部材50の接続部間の長さLaをこのように規定することにより、スクープ20が配置される風下端に対して気球10の風上端が上方に位置するヘッドアップした状態にすることができる。   In the mooring balloon according to the embodiment, the cord length adjusting members 50 and 60, the cord length adjusting device 70, and the cord length adjusting system 80 function so that the direction of the major axis of the balloon 10 becomes the horizontal direction. However, the cord length adjusting members 50 and 60, the cord length adjusting device 70, and the cord length adjusting system 80 may be configured such that the direction of the major axis of the balloon 10 has a predetermined inclination with respect to the horizontal direction. For example, the length La between the connecting portions of the cord length adjusting member 50 is set to be the length of the first mooring cord 30 through the cord length adjusting member 50 when the balloon 10 is not receiving the air current, You may prescribe | regulate so that it may be shorter than the length of 3 mooring lines 32. By defining the length La between the connecting portions of the rope length adjusting member 50 in this way, the head 10 is in a head-up state in which the wind upper end of the balloon 10 is located above the wind lower end where the scoop 20 is disposed. Can do.

実施形態に係る係留気球では、気球10は、内部に気体が充填されているときに高さ方向に短軸を有する回転楕円体状の形状を有し且つスクープ20が接合されているが、気球の実施形態は、このような実施形態に限定されない。例えば、気球の形状は、流線形でもよく、ドーナッツ状でもよく、風見安定するように垂直尾翼を有する形状、又は垂直尾翼及び水平尾翼を有する形状としてもよい。スクープ20、垂直尾翼及び水平尾翼のような風見安定するための構造を有する場合、索長調整部材50、60等の索長調整部材は、第1係留索30等の風下側に配置される係留索に並列接続してもよい。風見安定するための構造を有しない場合、長調整部材50、60等の索長調整部材は、第1〜第3係留索30〜32の全てに並列接続してもよい。   In the moored balloon according to the embodiment, the balloon 10 has a spheroid shape having a minor axis in the height direction when the gas is filled therein, and the scoop 20 is joined. The embodiment is not limited to such an embodiment. For example, the shape of the balloon may be streamlined or donut-shaped, and may have a shape having a vertical tail or a shape having a vertical tail and a horizontal tail so as to stabilize the weather. In the case of having a structure for stabilizing the weather such as the scoop 20, the vertical tail and the horizontal tail, the rope length adjusting members such as the rope length adjusting members 50 and 60 are moored arranged on the leeward side of the first mooring line 30 and the like. It may be connected in parallel to the cable. When the structure for stabilizing the weather is not provided, the length adjusting members such as the length adjusting members 50 and 60 may be connected in parallel to all the first to third mooring lines 30 to 32.

実施形態に係る係留気球では、第1〜第3係留索30〜32によって気球10が係留されるが、第1〜第3係留索30〜32の代わりに2本、又は4本以上の係留索を配置してもよい。この場合、索長調整部材50、60は、2本、又は4本以上の係留索の何れかに並列接続される。また、主係留索33を有さずに、第1〜第3係留索30〜32によって、気球10がウインチに係留されてもよい。   In the mooring balloon according to the embodiment, the balloon 10 is moored by the first to third mooring lines 30 to 32, but two or four or more mooring lines are used instead of the first to third mooring lines 30 to 32. May be arranged. In this case, the cable length adjusting members 50 and 60 are connected in parallel to either two or four or more mooring cables. The balloon 10 may be moored on the winch by the first to third mooring lines 30 to 32 without having the main mooring line 33.

1 係留気球
10 気球
20 スクープ
30〜34 係留索
50、60 索長調整部材
70 索長調整装置
80 索長調整システム
DESCRIPTION OF SYMBOLS 1 Mooring balloon 10 Balloon 20 Scoop 30-34 Mooring cable 50, 60 Cable length adjustment member 70 Cable length adjustment apparatus 80 Cable length adjustment system

Claims (2)

内部に気体が充填されたときに扁平形状になる気球と、
それぞれの一端が前記気球の表面に接続された複数の係留索と、
前記気球が受ける気流の風速に応じて、前記複数の係留索の何れかの長さを調整する索長調整部と、を有し、
前記索長調整部は、前記複数の係留索の何れか1つの長さを調整する弾性部材を有し、
前記弾性部材は、前記複数の係留索の何れか1つの所定の部分に、前記弾性部材に張力が印加されていないときの長さが前記所定の部分の長さよりも短くなるように並列接続され、
前記弾性部材は、中空部が内部に形成され、前記弾性部材に張力が印加されていないときに、前記所定の部分が前記中空部に配置される、ことを特徴とする係留気球。
A balloon that becomes flat when filled with gas,
A plurality of mooring lines, one end of which is connected to the surface of the balloon;
A cable length adjustment unit that adjusts the length of any of the plurality of mooring lines according to the wind speed of the airflow received by the balloon,
The cord length adjusting unit has an elastic member that adjusts the length of any one of the plurality of mooring cords,
The elastic member is connected in parallel to a predetermined portion of any one of the plurality of mooring lines so that the length when no tension is applied to the elastic member is shorter than the length of the predetermined portion. ,
A mooring balloon, wherein the elastic member has a hollow portion formed therein, and the predetermined portion is disposed in the hollow portion when no tension is applied to the elastic member.
前記気球の表面に接合されると共に、前記索長調整部により長さを調整される係留索に接続される膜状のスクープを更に有する、請求項に記載の係留気球。 Wherein while being bonded to the surface of the balloon, further comprising a film-like scoop connected to the mooring lines to be adjusted in length by the cord length adjusting unit, tethered balloon according to claim 1.
JP2014126492A 2014-06-19 2014-06-19 Moored balloon Active JP5769850B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2014126492A JP5769850B1 (en) 2014-06-19 2014-06-19 Moored balloon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014126492A JP5769850B1 (en) 2014-06-19 2014-06-19 Moored balloon

Publications (2)

Publication Number Publication Date
JP5769850B1 true JP5769850B1 (en) 2015-08-26
JP2016002973A JP2016002973A (en) 2016-01-12

Family

ID=54187145

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014126492A Active JP5769850B1 (en) 2014-06-19 2014-06-19 Moored balloon

Country Status (1)

Country Link
JP (1) JP5769850B1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109703730A (en) * 2019-01-29 2019-05-03 广东高空风能技术有限公司 A kind of high altitude kite balloon balloon and its control method
CN111186555A (en) * 2020-01-02 2020-05-22 上海交通大学 Method for designing and implementing overpressure balloon of sliding rope reinforced structure

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017154473A1 (en) * 2016-03-10 2017-09-14 パナソニックIpマネジメント株式会社 Flying object
JP6357494B2 (en) * 2016-03-10 2018-07-11 ソフトバンク株式会社 Moored balloon
JP6357499B2 (en) * 2016-05-25 2018-07-11 ソフトバンク株式会社 Moored balloon
JP6259866B2 (en) * 2016-05-25 2018-01-10 ソフトバンク株式会社 Moored balloon
CN106275363B (en) * 2016-10-08 2018-10-19 中国科学院光电研究院 A kind of microminiature captive balloon system
JP6176814B1 (en) * 2017-03-13 2017-08-09 義英 土橋 Cable-connected balloon-type rocket launcher.
JP6939532B2 (en) * 2017-12-26 2021-09-22 株式会社Ihi Underwater equipment
CN108557051B (en) * 2018-06-15 2023-10-24 湖南航天远望科技有限公司 Tethered balloon sphere, guaranteeing shelter and tethered balloon system thereof
JP6643417B2 (en) 2018-08-02 2020-02-12 Hapsモバイル株式会社 Systems, controllers and light aircraft
FR3111117B1 (en) * 2020-06-05 2022-07-22 Centre Nat Etd Spatiales Aerostat intended to carry out payload transport missions

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109703730A (en) * 2019-01-29 2019-05-03 广东高空风能技术有限公司 A kind of high altitude kite balloon balloon and its control method
CN109703730B (en) * 2019-01-29 2024-04-02 广东高空风能技术有限公司 High-altitude captive balloon and control method thereof
CN111186555A (en) * 2020-01-02 2020-05-22 上海交通大学 Method for designing and implementing overpressure balloon of sliding rope reinforced structure

Also Published As

Publication number Publication date
JP2016002973A (en) 2016-01-12

Similar Documents

Publication Publication Date Title
JP5769850B1 (en) Moored balloon
JP5697782B1 (en) Moored balloon
US9663214B2 (en) Balloon-borne platform stabilization
US8544788B1 (en) Aerostat assembly
US11772814B2 (en) System including a drone, a wire, and a docking station, enabling autonomous landings of the drones in degraded conditions
JP2928771B1 (en) Captive balloon
US20120181381A1 (en) Self-righting aerostat and relative takeoff and recovery system
US9938001B1 (en) Unmanned aerial vehicle (UAV) deployment of passive control stabilizers
US8368241B2 (en) Wind driven power generator
JP2013079034A (en) Rotorcraft for aerial photographing
US3227398A (en) Balloon tether cable
JP2017191963A (en) Ship communication method, ship, ship to ship communication system, and ship-land communication system
WO2000066424A1 (en) Balloon lifting system
JP6357494B2 (en) Moored balloon
US9902480B1 (en) Anti-tilt assembly for balloons
KR20200127634A (en) Mooring type flight apparatus
CN209600783U (en) A kind of captive balloon with kite empennage
JP2003227882A (en) Meteorological observation device
JP2019001309A (en) Flight vehicle unit
JP6282688B2 (en) Moored balloon
KR102643026B1 (en) Apparatus and method for controlling aerostat
KR102100111B1 (en) Apparatus for aerial photographing
KR20160081328A (en) autonomous sail-type balloon
JP2007001458A (en) Mooring type balloon
JP2017118308A (en) Vessel communication method, vessel, inter-vessel communication system, and vessel-to-land communication system

Legal Events

Date Code Title Description
TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20150526

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20150623

R150 Certificate of patent or registration of utility model

Ref document number: 5769850

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

S533 Written request for registration of change of name

Free format text: JAPANESE INTERMEDIATE CODE: R313533

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

S531 Written request for registration of change of domicile

Free format text: JAPANESE INTERMEDIATE CODE: R313531

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250