JP2019006361A - Buoyancy adjuster and drone with gas-closed vessel - Google Patents

Buoyancy adjuster and drone with gas-closed vessel Download PDF

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JP2019006361A
JP2019006361A JP2017139466A JP2017139466A JP2019006361A JP 2019006361 A JP2019006361 A JP 2019006361A JP 2017139466 A JP2017139466 A JP 2017139466A JP 2017139466 A JP2017139466 A JP 2017139466A JP 2019006361 A JP2019006361 A JP 2019006361A
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buoyancy
drone
gas
weight
specific gravity
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嘉幸 小林
Yoshiyuki Kobayashi
嘉幸 小林
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Abstract

To provide a drone that can fly and hover in the air while loading a heavy object or weighing heavy.SOLUTION: A drone includes: a gas-closed vessel 1 in which gas with a specific gravity that is lighter than earth atmosphere is hermetically closed; and a buoyancy adjustor 5 capable of adjusting buoyancy using a substance with a specific gravity that is heavier than the earth atmosphere, as a weight, thereby acquiring buoyancy and adjusting the buoyancy. Thus, the drone readily flies or hovers in the air while avoiding a possibility of out of control.SELECTED DRAWING: Figure 1

Description

本発明は、重量物を搭載しながら、あるいはドローン自身の重量が重い状態で飛行および空中浮揚するための浮力調節器および気体密閉器付きドローンに関するものである。  The present invention relates to a drone with a buoyancy regulator and a gas sealer for flying and floating in the air while carrying a heavy object or with a heavy weight of the drone itself.

解決しようとする問題点は、重量物を搭載しながら、あるいはドローン自身の重量が重い状態で飛行および空中浮揚する際にドローンが備える推進器によって得られる浮力だけでは浮力が足りず、飛行および空中浮揚が不可能な場合の問題を解決する点にある。  The problem to be solved is that the buoyancy obtained by the propulsion unit provided by the drone when flying and levitating while carrying a heavy object or with the heavy weight of the drone itself is not sufficient for buoyancy. It is to solve the problem when levitation is impossible.

本発明は、重量物を搭載しながら、あるいはドローン自身の重量が重い状態で飛行および空中浮揚する際にドローンが備える推進器によって得られる浮力が不足している場合においても飛行および空中浮揚を可能とするため、ドローンに地球大気より比重の軽い気体を密閉した気体密閉器と、地球大気より比重が重い物質を用いて錘とし浮力を調節可能とするための浮力調節器と、を備え、浮力を得るとともに浮力の調節を可能とすることを最も主要な特徴とする。  The present invention enables flying and floating in the air even when the buoyancy obtained by the propulsion device provided by the drone is insufficient when a heavy object is loaded or the drone itself is heavy and flying and floating in the air. Therefore, the drone is equipped with a gas seal that seals a gas whose specific gravity is lighter than the earth's atmosphere in a drone, and a buoyancy regulator that makes it possible to adjust the buoyancy as a weight using a substance whose specific gravity is heavier than the earth's atmosphere. The most important feature is that the buoyancy can be adjusted.

本発明の浮力調節器および気体密閉器付きドローンは、ドローンが備える推進器によって得られる浮力だけでなく、気体密閉器自体によっても浮力を得られるため、ドローンが備える推進器の浮力のみだけでは飛行および空中浮揚が不可能な場合においてもそれらが可能になり、かつ浮力を調節することが可能になるという利点がある。  Since the buoyancy regulator and the drone with the gas sealer of the present invention can obtain buoyancy not only by the buoyancy provided by the drone but also by the gas sealer itself, only the buoyancy of the propulsion device provided by the drone can fly. And, even when levitation is impossible, there is an advantage that they are possible and the buoyancy can be adjusted.

上部に気体密閉器を備え、かつ下部に浮力調節器を備え、中央部のドローンに連結した、浮力調節器および気体密閉器付きドローンの側面図。(実施例1)The side view of a drone with a buoyancy regulator and a gas sealer, which has a gas sealer at the top and a buoyancy regulator at the bottom and is connected to a drone in the center. (Example 1)

地球大気より比重が軽い気体を用いて浮力を得、地球大気より比重が重い物質を用いて浮力を調節するという目的を、最小の部品点数で、ドローンが備える機能を損なわずに実現した。  The objective of obtaining buoyancy using a gas with a specific gravity lower than that of the Earth's atmosphere and adjusting the buoyancy using a substance with a specific gravity higher than that of the Earth's atmosphere was achieved with the minimum number of parts and without compromising the functions of the drone.

図1は本発明装置の1実施例の側面図であって、1は気体密閉器、2はドローンの推進器、3はドローンのモーター、4はドローンの筐体および制御部、5は浮力調節器である。  FIG. 1 is a side view of an embodiment of the apparatus of the present invention, where 1 is a gas seal, 2 is a drone propulsion device, 3 is a drone motor, 4 is a drone housing and control unit, and 5 is a buoyancy adjustment. It is a vessel.

1の気体密閉器は気体を密閉して格納する目的を満たすものであれば、その材質および形状は問わない。5の浮力調節器は錘としての目的を満たすものであれば、その材質および形状は問わない。また1の気体密閉器と2のドローンの推進器と3のドローンのモーターと4のドローンの筐体および制御部と5の浮力調節器の配置については、飛行および空中浮揚に支障がない限り自由である。1の気体密閉器と4のドローンの筐体および制御部は固定された場合またはワイヤー等によりゆるやかに連結された場合のどちらでも可とする。同じく4のドローンの筐体および制御部と5の浮力調節器は固定された場合またはワイヤー等によりゆるやかに連結された場合のどちらでも可とする。固定または連結の方法についても、飛行および空中浮揚に支障がない限り自由である。  The material and shape of the gas sealer 1 are not limited as long as they satisfy the purpose of sealing and storing gas. The material and shape of the buoyancy adjuster 5 are not limited as long as they satisfy the purpose of the weight. Arrangement of 1 gas sealer, 2 drone propulsion device, 3 drone motor, 4 drone housing and control unit and 5 buoyancy adjuster is free as long as there is no hindrance to flight and air levitation. It is. The case and the control unit of the gas sealer 1 and the drone 4 can be either fixed or loosely connected by a wire or the like. Similarly, the case and the control unit of the drone 4 and the buoyancy adjuster 5 can be either fixed or loosely connected by a wire or the like. The method of fixing or connecting is also free as long as it does not hinder flight and levitation.

一例として、地球大気より比重の軽い気体としてヘリウムガスを用い、浮力調節器の錘として比重1の水を用いた場合、浮力調節器および気体密閉器付きドローンで、気温15度の環境下で100Kgの重量物を持ちつつ、飛行および空中浮揚する場合に必要なヘリウムガスの体積を以下の計算で示し、なおかつその場合、浮力調節器でどの程度の浮力の調節を必要とするかを示す。  As an example, when helium gas is used as a gas having a specific gravity lighter than the Earth's atmosphere, and water with a specific gravity of 1 is used as the weight of the buoyancy regulator, a drone with a buoyancy regulator and a gas sealer is used and is 100 kg in an environment with a temperature of 15 degrees. The following calculation shows the volume of helium gas required when flying and levitating while holding a heavy object, and in that case, how much buoyancy adjustment is required by the buoyancy regulator.

気体密閉器を球体の風船と仮定し、浮力調節器をポリタンクと仮定する。この場合の気体密閉器と浮力調節器の重量を以下で計算する。  The gas seal is assumed to be a spherical balloon, and the buoyancy regulator is assumed to be a poly tank. In this case, the weight of the gas sealer and the buoyancy adjuster is calculated as follows.

風船の直径を8mと仮定し、風船を完全な球体と仮定すると、風船の表面積Sbは
仮に風船の生地の1平方メートルあたりの重量を0.3Kg/m^2とすると、直径8mの風船自体の重量Mfは
ポリタンクを一辺1mの立方体のポリタンク(容量1000リットル)と仮定すると、このポリタンクの表面積Spは
仮にポリタンクの1平方メートルあたりの重量を0.5Kg/m^2とすると、一辺1mの立方体のポリタンク自体の重量Mpは
ドローン自体の重量を20Kgと仮定すれば、直径8mの風船および一辺1mの立方体のポリタンクの重量を合計すると、重量MnはMn=Mf+Mp+20Kgであるから
よって83.288Kgが上記の場合の浮力調節器および気体密閉器付きドローンの空重量となる。
Assuming that the balloon diameter is 8 m and the balloon is a perfect sphere, the surface area Sb of the balloon is
If the weight per square meter of the balloon fabric is 0.3 kg / m ^ 2, the weight Mf of the 8 m diameter balloon itself is
Assuming that the polytank is a cubic polytank with a side of 1 m (capacity 1000 liters), the surface area Sp of this polytank is
If the weight per square meter of the plastic tank is 0.5 kg / m ^ 2, the weight Mp of the cubic plastic tank itself with a side of 1 meter is
If the weight of the drone itself is assumed to be 20 kg, the weight Mn is Mn = Mf + Mp + 20 kg when the weight of a balloon with a diameter of 8 m and a cubic poly tank with a side of 1 m is added up.
Therefore, 83.288 kg is the empty weight of the drone with the buoyancy regulator and the gas sealer in the above case.

次に直径8mの風船に充填されたヘリウムガスの浮力を以下で計算する。気温0度で1気圧の場合、地球大気の密度は1.293kg/m^3、ヘリウムガスの密度は0.178Kg/m^3である。よって気温15度の場合の地球大気の密度Daとヘリウムガスの密度Dhは
したがって気温15度でのヘリウムガスにおける1m^3あたりの浮力Bhは
風船の体積はV=4/3πr3なので、直径8mの風船の体積Vaは
すなわちヘリウムガスを充填した直径8mの風船が持つ浮力Bh’は
浮力調節器および気体密閉器付きドローンの空重量Mnは83.288Kgであるので、気体密閉器として上記のヘリウムガスを充填した直径8mの風船を用いた場合、これに100Kgの重量物を搭載した際の重量Mgは
この場合のヘリウムガスの浮力はBh’=284.0235Kgなので、Bh’>Mnとなり浮力が強すぎる。これでは浮力調節器および気体密閉器付きドローンが勝手に上昇してしまい、制御不能となる恐れがある。よって浮力調節器で浮力を調節する。
Next, the buoyancy of helium gas filled in an 8 m diameter balloon is calculated as follows. When the temperature is 0 degree and 1 atmosphere, the density of the earth atmosphere is 1.293 kg / m ^ 3, and the density of helium gas is 0.178 Kg / m ^ 3. Therefore, the density Da of the earth atmosphere and the density Dh of helium gas when the temperature is 15 degrees are
Therefore, the buoyancy Bh per m ^ 3 in helium gas at a temperature of 15 degrees is
Since the volume of the balloon is V = 4 / 3πr3, the volume Va of the balloon with a diameter of 8 m is
In other words, the buoyancy Bh 'of the 8m diameter balloon filled with helium gas is
Since the empty weight Mn of the drone with the buoyancy regulator and the gas sealer is 83.288 kg, when a balloon with an diameter of 8 m filled with the above helium gas is used as the gas sealer, a heavy object of 100 kg is mounted on the balloon. The weight of Mg is
In this case, the buoyancy of the helium gas is Bh ′ = 284.0235 kg, so that Bh ′> Mn and the buoyancy is too strong. In this case, the buoyancy adjuster and the drone with the gas sealer may rise without permission and may become uncontrollable. Therefore, the buoyancy is adjusted with the buoyancy adjuster.

調節する必要がある浮力をBcとすると
つまり浮力調節器によって100.7355Kg以上の重量負荷をかけることで、浮力調節器および気体密閉器付きドローンが勝手に上昇してしまい制御不能となる恐れを回避できる。ここで、必要とされる重量負荷をMcとする。ここでは浮力調節器を一辺1mの立方体のポリタンク(容量1000リットル)を用いると仮定しており、浮力調節器の錘として比重1の水を用いると仮定している。よってポリタンク内にMc=101リットルの比重1の水を注入すれば、上記の場合における浮力調節器として機能する。
上記の場合の総重量Mg’は
ドローン自身が持ち上げる必要がある重量Mdは、Bh’=284.0235Kgであるから
つまり上記の場合、ドローン自身が備える推進器によって持ち上げる必要がある重量はわずか0.2645Kgで済むことになる。
If the buoyancy that needs to be adjusted is Bc
That is, by applying a weight load of 100.7355 kg or more with the buoyancy adjuster, it is possible to avoid the possibility that the buoyancy adjuster and the drone with the gas sealer will rise without permission and become uncontrollable. Here, let Mc be the required weight load. Here, it is assumed that a cubic poly tank (capacity 1000 liters) with a side of 1 m is used as the buoyancy regulator, and water having a specific gravity of 1 is used as the weight of the buoyancy regulator. Therefore, if water of specific gravity 1 with Mc = 101 liters is injected into the plastic tank, it functions as a buoyancy regulator in the above case.
The total weight Mg 'in the above case is
The weight Md that the drone needs to lift is Bh ′ = 284.0235Kg.
In other words, in the above case, the weight that needs to be lifted by the propulsion unit included in the drone itself is only 0.2645 kg.

重量物の重さに応じて任意に決定された気体密閉器の容量に対して浮力調節器の容量を調節可能であることから、浮力調節器および気体密閉器付きドローンが制御不能となる恐れを回避しつつ、重量物を搭載した状態あるいはドローン自身の重量が重い場合であっても容易にドローンによる飛行および空中浮揚を実現できる。  Since the capacity of the buoyancy regulator can be adjusted with respect to the capacity of the gas seal that is arbitrarily determined according to the weight of the heavy object, there is a risk that the buoyancy regulator and the drone with the gas seal will be out of control. While avoiding, even when a heavy object is mounted or when the weight of the drone itself is heavy, it is possible to easily realize flying and levitation by the drone.

Claims (1)

重量物を搭載しながら、あるいはドローン自身の重量が重い状態で飛行および空中浮揚する際に、ドローンが備える推進器によって得られる浮力が不足している場合においても飛行および空中浮揚を可能とするための手段において、地球大気より比重の軽い気体を密閉した気体密閉器と、地球大気より比重が重い物質を用いて浮力を調節可能とするための浮力調節器と、を備え、飛行および空中浮揚することを特徴とする浮力調節器および気体密閉器付きドローン  To fly and levitate even when the buoyancy provided by the propulsion unit provided by the drone is insufficient when flying and levitating while carrying a heavy object or when the drone itself is heavy And a buoyancy adjuster for adjusting buoyancy using a substance having a heavier specific gravity than the earth atmosphere, and flying and levitating in the air. Drone with buoyancy regulator and gas seal
JP2017139466A 2017-06-28 2017-06-28 Buoyancy adjuster and drone with gas-closed vessel Pending JP2019006361A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7421574B2 (en) 2019-06-20 2024-01-24 ホ ワン,ソン A floating object with adjustable levitation height

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002514149A (en) * 1996-12-19 2002-05-14 エアレオン・コーポレイション Hovering vehicle
WO2014207732A1 (en) * 2013-06-28 2014-12-31 Paolo Bellezza Quater A multi-rotor aircraft
JP2017047893A (en) * 2015-07-31 2017-03-09 パナソニックIpマネジメント株式会社 Flight body

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002514149A (en) * 1996-12-19 2002-05-14 エアレオン・コーポレイション Hovering vehicle
WO2014207732A1 (en) * 2013-06-28 2014-12-31 Paolo Bellezza Quater A multi-rotor aircraft
JP2017047893A (en) * 2015-07-31 2017-03-09 パナソニックIpマネジメント株式会社 Flight body

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7421574B2 (en) 2019-06-20 2024-01-24 ホ ワン,ソン A floating object with adjustable levitation height

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