JP2020087898A - Hydrogen balloon and drone with hydrogen fuel cell - Google Patents
Hydrogen balloon and drone with hydrogen fuel cell Download PDFInfo
- Publication number
- JP2020087898A JP2020087898A JP2018232969A JP2018232969A JP2020087898A JP 2020087898 A JP2020087898 A JP 2020087898A JP 2018232969 A JP2018232969 A JP 2018232969A JP 2018232969 A JP2018232969 A JP 2018232969A JP 2020087898 A JP2020087898 A JP 2020087898A
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- Prior art keywords
- drone
- hydrogen
- fuel cell
- buoyancy
- balloon
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- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 title claims abstract description 55
- 239000001257 hydrogen Substances 0.000 title claims abstract description 39
- 229910052739 hydrogen Inorganic materials 0.000 title claims abstract description 39
- 239000000446 fuel Substances 0.000 title claims abstract description 23
- 230000005611 electricity Effects 0.000 claims abstract description 5
- 239000000463 material Substances 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells
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- Fuel Cell (AREA)
Abstract
Description
本発明は、重量物を搭載しながら飛行するための水素バルーンを搭載し、かつ水素燃料電池で発電しつつ飛行する、水素バルーンおよび水素燃料電池付きドローンに関するものである。 The present invention relates to a hydrogen balloon and a drone with a hydrogen fuel cell, which carries a hydrogen balloon for flying while carrying a heavy object, and which flies while generating power with a hydrogen fuel cell.
解決しようとする問題点は、ドローンに重量物を搭載しながら飛行する場合、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、飛行が不可能な場合の問題を解決し、かつドローンに重量物を搭載せず、ドローンが備える推進器によって得られる浮力だけで飛行可能な場合、ドローンの飛行に必要な電力をドローン自ら発電しつつ飛行する点にある。 The problem to be solved is that when flying with a heavy load on the drone, the buoyancy obtained by the drone's propulsion device is insufficient for buoyancy, and the problem when the flight is impossible is solved, and the drone If you can fly only with the buoyancy provided by the drone's propulsion device without loading heavy objects, the drone is at the point of flying while generating the power necessary for the drone to fly.
本発明は、水素ガスを格納するための水素バルーンと水素ガスを燃料に発電する水素燃料電池を搭載したドローンにおいて、重量物を搭載しながら飛行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を可能とするため、水素ガスを充填した水素バルーンにより浮力を得つつ飛行し、かつ重量物を搭載していない場合は水素バルーン内の水素ガスを燃料に水素燃料電池で発電することにより、ドローンの飛行に必要な電力をドローン自ら発電しつつ飛行を可能とすることを最も主要な特徴とする。 The present invention is a drone equipped with a hydrogen balloon for storing hydrogen gas and a hydrogen fuel cell for generating electric power using hydrogen gas as a fuel, and the buoyancy obtained by a propulsion device provided in the drone when flying while carrying a heavy object In order to enable flight even when there is a shortage, the hydrogen balloon filled with hydrogen gas flies while gaining buoyancy, and when no heavy object is loaded, the hydrogen gas in the hydrogen balloon is used as fuel The most important feature is that the drone can generate power by using the battery to generate the power necessary for the drone to fly.
本発明の水素バルーンおよび水素燃料電池付きドローンは、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、水素バルーン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が不可能な場合においても飛行が可能になり、かつドローンが備える推進器のみで十分な浮力が得られる場合においては水素バルーン内の水素ガスを燃料に水素燃料電池で発電しつつ飛行可能になることで、ドローン自体が大量のバッテリーを搭載せずに済むという利点がある。 Since the hydrogen balloon and the drone with hydrogen fuel cell of the present invention can obtain buoyancy not only by the propulsion device provided in the drone but also by the hydrogen balloon itself, flight is not possible only by the buoyancy of the propulsion device provided by the drone. If possible, it will be possible to fly, and if sufficient buoyancy can be obtained with only the propulsion device of the drone, it will be possible to fly using hydrogen gas in the hydrogen balloon as fuel and a hydrogen fuel cell to generate electricity. , There is an advantage that the drone itself does not have to be equipped with a large amount of batteries.
ドローンが浮力を必要とする場合は水素バルーンによる浮力を得つつ飛行し、浮力を必要としない場合は水素バルーン内の水素ガスをもとに水素燃料電池で発電しつつ飛行するという目的を、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。 If the drone needs buoyancy, it will fly while obtaining the buoyancy of the hydrogen balloon, and if it does not need buoyancy, the objective is to fly while generating electricity with a hydrogen fuel cell based on the hydrogen gas in the hydrogen balloon. With the number of parts, it was realized without impairing 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は水素バルーン、2はドローンの推進器、3はドローン本体および制御部、4は水素燃料電池である。 FIG. 1 is a side view of one embodiment of the device of the present invention, 1 is a hydrogen balloon, 2 is a drone propeller, 3 is a drone body and control unit, and 4 is a hydrogen fuel cell.
1の水素バルーンは水素ガス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。また1の水素バルーンと2のドローンの推進器と3のドローン本体と4の水素燃料電池の配置や連結方法については、飛行に支障がない限り自由である。 The
ドローンに重量物を搭載しながら出発地と目的地の間を飛行し、目的地に到着した際に重量物をドローンから降ろしたのち出発地に帰還するような場合、往路(重量物搭載中)において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、飛行が不可能な場合の問題を解決し、かつ復路(重量物なし)においてドローンが飛行する際に必要な電力をドローン自ら発電しつつ飛行を可能とすることで、効率的な重量物の運搬が可能となることから、運送業などの産業分野での活用が期待される。 When flying between a departure point and a destination while loading a heavy load on a drone, and when arriving at the destination, removing the heavy load from the drone and then returning to the starting place, the outbound route (while loading the heavy load) In buoyancy provided by the drone's propulsion device alone, buoyancy is not enough to solve the problem when flight is not possible, and the drone generates the power necessary for the flight on the return trip (without heavy objects) By enabling flight while enabling efficient transportation of heavy objects, it is expected to be utilized in industrial fields such as the transportation industry.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2018232969A JP2020087898A (en) | 2018-11-26 | 2018-11-26 | Hydrogen balloon and drone with hydrogen fuel cell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2018232969A JP2020087898A (en) | 2018-11-26 | 2018-11-26 | Hydrogen balloon and drone with hydrogen fuel cell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JP2020087898A true JP2020087898A (en) | 2020-06-04 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2018232969A Pending JP2020087898A (en) | 2018-11-26 | 2018-11-26 | Hydrogen balloon and drone with hydrogen fuel cell |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2020087898A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114954961A (en) * | 2022-07-13 | 2022-08-30 | 斗山创新(深圳)有限公司 | An industrial-grade VTOL fixed-wing UAV hydrogen fuel cell system |
| IT202300024318A1 (en) | 2023-11-16 | 2025-05-16 | Competence Industry Mfg 4 0 S C A R L | UNMANNED AERIAL VEHICLE SYSTEM |
-
2018
- 2018-11-26 JP JP2018232969A patent/JP2020087898A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114954961A (en) * | 2022-07-13 | 2022-08-30 | 斗山创新(深圳)有限公司 | An industrial-grade VTOL fixed-wing UAV hydrogen fuel cell system |
| IT202300024318A1 (en) | 2023-11-16 | 2025-05-16 | Competence Industry Mfg 4 0 S C A R L | UNMANNED AERIAL VEHICLE SYSTEM |
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