JP2019006361A - Buoyancy adjuster and drone with gas-closed vessel - Google Patents
Buoyancy adjuster and drone with gas-closed vessel Download PDFInfo
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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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- 230000005484 gravity Effects 0.000 claims abstract description 11
- 239000000126 substance Substances 0.000 claims abstract description 4
- 238000005303 weighing Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 33
- 239000001307 helium Substances 0.000 description 9
- 229910052734 helium Inorganic materials 0.000 description 9
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 9
- 238000005339 levitation Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 239000004744 fabric Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Abstract
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.
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
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
調節する必要がある浮力をBcとすると
上記の場合の総重量Mg’は
The total weight Mg 'in the above case is
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.
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JP2017139466A JP2019006361A (en) | 2017-06-28 | 2017-06-28 | Buoyancy adjuster and drone with gas-closed vessel |
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JP2017139466A JP2019006361A (en) | 2017-06-28 | 2017-06-28 | Buoyancy adjuster and drone with gas-closed vessel |
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Cited By (1)
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)
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 |
-
2017
- 2017-06-28 JP JP2017139466A patent/JP2019006361A/en active Pending
Patent Citations (3)
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)
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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