JP2013154879A - Coalesced aero-land carrier of automobile, stern of airplane and helicopter - Google Patents

Coalesced aero-land carrier of automobile, stern of airplane and helicopter Download PDF

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Publication number
JP2013154879A
JP2013154879A JP2013065067A JP2013065067A JP2013154879A JP 2013154879 A JP2013154879 A JP 2013154879A JP 2013065067 A JP2013065067 A JP 2013065067A JP 2013065067 A JP2013065067 A JP 2013065067A JP 2013154879 A JP2013154879 A JP 2013154879A
Authority
JP
Japan
Prior art keywords
helicopter
wing
aero
wings
specific
Prior art date
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Pending
Application number
JP2013065067A
Other languages
Japanese (ja)
Inventor
Jin Nakajo
仁 中城
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP2013065067A priority Critical patent/JP2013154879A/en
Publication of JP2013154879A publication Critical patent/JP2013154879A/en
Pending legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To provide an epoch-making aero-land carrier.SOLUTION: Due to a situation in which electric wires are almost distributed everywhere in a region, first of all, an aero-land carrier moves to a place where no electric wires are distributed, wings of a helicopter are extended, the right and left wings of a lateral shaft are extended during its operation and an umbrella of the helicopter is folded. Within a descending region, the wings of the helicopter are extended and the wings of the lateral shaft is folded and a descending motion is carried out only with the helicopter and then the coalesced aero-land carrier can be landed at a destination location.

Description

車窓の下部が電気自動車が一艘目、横軸が比翼で水素エンジン動力が2艘目、三艘目がヘリコプターの比翼が延び、傘の様な開き方のヘリコプター比翼、陸上部を走る時は、電気自動車(=水素での比翼時等で電力補給)、飛び立つ時には、駐車場等の電線の無い場所使用、まず、ヘリコプターの比翼を伸ばし、稼動中に横軸の比翼左右を延ばしヘリコプターの傘を畳む。下降領域では、ヘリの比翼を延ばし横軸の比翼を畳み、ヘリだけで下降、そして、目的地に着陸。そこから、さらに、電気自動車で移動する。そして、目的地に到達する。  At the bottom of the car window is the first car of the electric vehicle, the horizontal axis is the specific wing, the hydrogen engine power is the second wing, the third wing is the helicopter wing, and the helicopter wing that opens like an umbrella, , Electric vehicles (= refueling when using a specific wing with hydrogen, etc.), when flying, use a place where there is no electric wire, such as a parking lot. First, extend the specific wing of the helicopter and extend the right and left specific wings of the helicopter during operation. Fold up. In the descending area, the helicopter's specific wing is extended, the horizontal wing is folded, the helicopter descends, and then landed at the destination. From there, you can also travel by electric car. Then, the destination is reached.

新型の電気自動車や軍用機にも着目。  Focus on new electric cars and military aircraft.

プロが教える自動車のメカニズム(ナツメ社)・図解ヘリコプター(講談社)・図解・飛行機のメカニズム(講談社)  Automotive mechanisms taught by professionals (Natsume), illustrated helicopter (Kodansha), illustrated, airplane mechanism (Kodansha) 飛行機の操縦(PHP新書)・航空管制の科学(講談社)  Airplane control (PHP new book), science of air traffic control (Kodansha)

技術分野参照  Refer to technical field 技術分野参照  Refer to technical field

[実体型のモデル製造]  [Manufacture of solid model]

[水素エンジンの比翼の濃縮技術・水素ボンベ等の補助・水から水素を取り出し水槽のタンクが必要]  [Concentration technology for hydrogen engine specific blades, assistance for hydrogen cylinders, etc. ・ Hydrogen tank is required to extract hydrogen from water]

[日常生活で自動車の様な必要性の時代]  [Era of the necessity of automobiles in daily life]

[技術分野参照]
[Refer to technical field]

[日本や世界で利用可能]  [Available in Japan and the world]

[なし]  [None]

[空陸免許を取得する学校で自衛隊の元パイロットが必要]  [A former pilot of the Self-Defense Force is required at a school that obtains an air-land license]

・・・・...

・・・・...

【0004】
【非特許文献1】技術分野参照
【非特許文献2】技術分野参照
【発明の概要】
【発明が解決しようとする課題】
[実体型のモデル製造]
【課題を解決するための手段】
[水素エンジンの比翼の濃縮技術・水素ボンベ等の補助・水から水素を取り出し水槽のタンクが必要]
【発明の効果】
[日常生活で自動車の様な必要性の時代]
【図面の簡単な説明】
[技術分野参照]
【図1】空陸運搬具が地上を飛び立ち、空を旋回して、比翼も延ばしたりして地上にヘリで降り立ち目的地に向かう図面。
【図2】空陸運搬具が地上を飛び立ち、空を旋回して、比翼も延ばしたりして地上にヘリで降り立ち目的地に向かう図面。
[日本や世界で利用可能]
【実施例】
[なし]
【産業上の利用可能性】
[空陸免許を取得する学校で自衛隊の元パイロットが必要]
[0004]
[Non-patent document 1] Refer to technical field [Non-patent document 2] Refer to technical field [Summary of the Invention]
[Problems to be solved by the invention]
[Manufacture of solid model]
[Means for Solving the Problems]
[Concentration technology for hydrogen engine specific blades, assistance for hydrogen cylinders, etc. ・ Hydrogen tank is required to extract hydrogen from water]
【Effect of the invention】
[Era of the necessity of automobiles in daily life]
[Brief description of the drawings]
[Refer to technical field]
FIG. 1 is a drawing in which an air-land vehicle flies off the ground, turns in the sky, extends its specific wing, and then descends to the ground and heads for the destination.
FIG. 2 is a drawing in which an air-land vehicle flies off the ground, turns in the sky, extends its specific wing, and then descends to the ground and heads for the destination.
[Available in Japan and the world]
【Example】
[None]
[Industrial applicability]
[A former pilot of the Self-Defense Force is required at a school that obtains an air-land license]

Claims (1)

[技術分野]
車窓の下部が電気自動車が一艘目、横軸が比翼で水素エンジン動力が2艘目、三艘目がヘリコプターの比翼が延び、傘の様な開き方のヘリコプター比翼、陸上部を走る時は、電気自動車(=水素での比翼時等で電力補給)、飛び立つ時には、駐車場等の電線の無い場所使用、まず、ヘリコプターの比翼を伸ばし、稼動中に横軸の比翼左右を延ばしヘリコプターの傘を畳む。下降領域では、ヘリの比翼を延ばし横軸の比翼を畳み、ヘリだけで下降、そして、目的地に着陸。そこから、さらに、電気自動車で移動する。そして、目的地に到達する。
[Technical field]
At the bottom of the car window is the first car of the electric vehicle, the horizontal axis is the specific wing, the hydrogen engine power is the second wing, the third wing is the helicopter wing, and the helicopter wing that opens like an umbrella, , Electric vehicles (= refueling when using a specific wing with hydrogen, etc.), when flying, use a place where there is no electric wire, such as a parking lot. First, extend the specific wing of the helicopter and extend the right and left wings of the horizontal axis during operation Fold up. In the descending area, the helicopter wing is extended, the horizontal wing is folded, the helicopter descends, and then landed at the destination. From there, you can also travel by electric car. Then, the destination is reached.
JP2013065067A 2013-03-06 2013-03-06 Coalesced aero-land carrier of automobile, stern of airplane and helicopter Pending JP2013154879A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2013065067A JP2013154879A (en) 2013-03-06 2013-03-06 Coalesced aero-land carrier of automobile, stern of airplane and helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013065067A JP2013154879A (en) 2013-03-06 2013-03-06 Coalesced aero-land carrier of automobile, stern of airplane and helicopter

Publications (1)

Publication Number Publication Date
JP2013154879A true JP2013154879A (en) 2013-08-15

Family

ID=49050497

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013065067A Pending JP2013154879A (en) 2013-03-06 2013-03-06 Coalesced aero-land carrier of automobile, stern of airplane and helicopter

Country Status (1)

Country Link
JP (1) JP2013154879A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104589937A (en) * 2013-11-29 2015-05-06 仇文江 Gasoline helicopter used both in air and on ground and provided with same helicopter body
CN107038547A (en) * 2017-05-02 2017-08-11 莆田市烛火信息技术有限公司 A kind of land sky fusion logistics transporting device and method
JP2018013090A (en) * 2016-07-21 2018-01-25 海老原 雄二 Hydrogen engine device

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4017043A (en) * 1976-03-08 1977-04-12 The United States Of America As Represented By The Secretary Of The Navy Deployable rotor
JPH0686406A (en) * 1992-08-31 1994-03-25 Matsushita Electric Ind Co Ltd Charging equipment
JPH072188A (en) * 1993-04-13 1995-01-06 Toru Fujii Non-tall wing inclination jet rocket composite method
JP2009521358A (en) * 2005-12-22 2009-06-04 ジェイ ゲルビーノ アレン Retractable lift blade for aircraft

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4017043A (en) * 1976-03-08 1977-04-12 The United States Of America As Represented By The Secretary Of The Navy Deployable rotor
JPH0686406A (en) * 1992-08-31 1994-03-25 Matsushita Electric Ind Co Ltd Charging equipment
JPH072188A (en) * 1993-04-13 1995-01-06 Toru Fujii Non-tall wing inclination jet rocket composite method
JP2009521358A (en) * 2005-12-22 2009-06-04 ジェイ ゲルビーノ アレン Retractable lift blade for aircraft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104589937A (en) * 2013-11-29 2015-05-06 仇文江 Gasoline helicopter used both in air and on ground and provided with same helicopter body
JP2018013090A (en) * 2016-07-21 2018-01-25 海老原 雄二 Hydrogen engine device
CN107038547A (en) * 2017-05-02 2017-08-11 莆田市烛火信息技术有限公司 A kind of land sky fusion logistics transporting device and method
CN107038547B (en) * 2017-05-02 2021-02-23 莆田市烛火信息技术有限公司 Air-ground integrated logistics transportation device and method

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