JP2016165987A - Unmanned multi-rotor type helicopter airframe guard device - Google Patents

Unmanned multi-rotor type helicopter airframe guard device Download PDF

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Publication number
JP2016165987A
JP2016165987A JP2015061621A JP2015061621A JP2016165987A JP 2016165987 A JP2016165987 A JP 2016165987A JP 2015061621 A JP2015061621 A JP 2015061621A JP 2015061621 A JP2015061621 A JP 2015061621A JP 2016165987 A JP2016165987 A JP 2016165987A
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Japan
Prior art keywords
rotor type
unmanned multi
type helicopter
airframe
guard device
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Pending
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JP2015061621A
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Japanese (ja)
Inventor
幸明 十田
Yukiaki Toda
幸明 十田
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Priority to JP2015061621A priority Critical patent/JP2016165987A/en
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Abstract

PROBLEM TO BE SOLVED: To provide an unmanned multi-rotor type helicopter including a device that can reduce an impact at collision or crash to increase safety to a personnel and an objective.SOLUTION: An unmanned multi-rotor type helicopter airframe guard device has a structure that covers an airframe A with a doughnut-shaped or sphere-shaped balloon buffer device B into which a helium gas or air is filled.SELECTED DRAWING: Figure 1

Description

本発明は無人マルチローター型ヘリコプターの安全性を図ったものである。The present invention is intended for the safety of unmanned multi-rotor helicopters.

技術背景Technical background

従来のマルチローター型ヘリコプターはプロペラや機体の周りをプラスチックや金属等で囲ったものである。A conventional multi-rotor helicopter has a propeller and a fuselage surrounded by plastic or metal.

従来の機体ガードでは構造がプラスチックや金属で出来ており重量が重く強度が弱く衝撃吸収性がほとんどないので衝突や墜落時の衝撃による対人対物への安全性がほとんどないに等しい。本発明は衝突や墜落時における衝撃を弱め対人対物への安全性を高め軽量化を図る為のものである。Conventional airframe guards are made of plastic or metal, are heavy, weak and have little shock absorption, so there is almost no safety to human objectives due to impacts during collisions or crashes. The present invention is intended to reduce the impact at the time of a collision or crash, increase the safety to the human object, and reduce the weight.

課題を解決する為の手段Means to solve the problem

本発明は上記目的を達成する為にマルチローター型ヘリコプターの機体の周りをドーナツ状又は球状のバルーンにヘリウムガスか空気を封入したもので覆った構造にする。In order to achieve the above object, the present invention has a structure in which the body of a multi-rotor helicopter is covered with a donut-shaped or spherical balloon filled with helium gas or air.

発明の効果Effect of the invention

本発明は次のような効果を奏する。
本発明は機体をドーナツ状又は球状の柔らかいバルーンで覆う為軽量化と衝突時や墜落時の衝撃を大幅に減少する効果を発揮するものである。The present invention has the following effects.
Since the airframe is covered with a soft donut-shaped or spherical balloon, the present invention exhibits the effect of reducing the weight and greatly reducing the impact at the time of collision or crash.

発明を実施する為の形態BEST MODE FOR CARRYING OUT THE INVENTION

以下本発明の実施形態を図１に基ずいて説明する。Hereinafter, an embodiment of the present invention will be described with reference to FIG.

において機体（Ａ）をドーナツ状又は球状のバルーン（Ｂ）で囲った状態にする。The airframe (A) is surrounded by a donut-shaped or spherical balloon (B).

Claims (1)

無人マルチローター型ヘリコプターに取り付ける、ヘリウムガス又は空気を封入したドーナツ状又は球状のバルーン緩衝装置。A donut-shaped or spherical balloon cushioning device filled with helium gas or air, which is attached to an unmanned multi-rotor helicopter.
JP2015061621A 2015-03-09 2015-03-09 Unmanned multi-rotor type helicopter airframe guard device Pending JP2016165987A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2015061621A JP2016165987A (en) 2015-03-09 2015-03-09 Unmanned multi-rotor type helicopter airframe guard device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2015061621A JP2016165987A (en) 2015-03-09 2015-03-09 Unmanned multi-rotor type helicopter airframe guard device

Publications (1)

Publication Number Publication Date
JP2016165987A true JP2016165987A (en) 2016-09-15

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Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015061621A Pending JP2016165987A (en) 2015-03-09 2015-03-09 Unmanned multi-rotor type helicopter airframe guard device

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JP (1) JP2016165987A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017061174A (en) * 2015-09-24 2017-03-30 廣田 祐次 Drone with balloon
JP6217054B1 (en) * 2016-11-04 2017-10-25 株式会社松屋アールアンドディ Drone with airbag
WO2019142470A1 (en) 2018-01-22 2019-07-25 株式会社松屋アールアンドディ Control method for drone with airbag, and drone with airbag

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017061174A (en) * 2015-09-24 2017-03-30 廣田 祐次 Drone with balloon
JP6217054B1 (en) * 2016-11-04 2017-10-25 株式会社松屋アールアンドディ Drone with airbag
WO2018084125A1 (en) * 2016-11-04 2018-05-11 株式会社松屋アールアンドディ Drone with airbag
JP2018079911A (en) * 2016-11-04 2018-05-24 株式会社松屋アールアンドディ Drone with air bag
TWI686328B (en) * 2016-11-04 2020-03-01 日商松屋Ｒ＆Ｄ股份有限公司 UAV with airbag
US11772597B2 (en) 2016-11-04 2023-10-03 Matsuya R&D Co., Ltd. Drone with airbag
WO2019142470A1 (en) 2018-01-22 2019-07-25 株式会社松屋アールアンドディ Control method for drone with airbag, and drone with airbag
EP3744639A4 (en) * 2018-01-22 2021-11-03 Matsuya R&D Co., Ltd Control method for drone with airbag, and drone with airbag

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