JP2020019481A5 - - Google Patents

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Publication number
JP2020019481A5
JP2020019481A5 JP2019204607A JP2019204607A JP2020019481A5 JP 2020019481 A5 JP2020019481 A5 JP 2020019481A5 JP 2019204607 A JP2019204607 A JP 2019204607A JP 2019204607 A JP2019204607 A JP 2019204607A JP 2020019481 A5 JP2020019481 A5 JP 2020019481A5
Authority
JP
Japan
Prior art keywords
main body
aircraft
flying object
peripheral portion
object according
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
JP2019204607A
Other languages
Japanese (ja)
Other versions
JP2020019481A (en
JP7038421B2 (en
Filing date
Publication date
Application filed filed Critical
Priority to JP2019204607A priority Critical patent/JP7038421B2/en
Priority claimed from JP2019204607A external-priority patent/JP7038421B2/en
Publication of JP2020019481A publication Critical patent/JP2020019481A/en
Publication of JP2020019481A5 publication Critical patent/JP2020019481A5/ja
Priority to JP2022009036A priority patent/JP7296153B2/en
Application granted granted Critical
Publication of JP7038421B2 publication Critical patent/JP7038421B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Claims (9)

外周部及び内周部を有する本体部と、
前記本体部の内部に設けられ、少なくとも前記本体部の上方から下方に向かう気流を発
生させるための揚力発生部と、
前記本体部の側面の部に、前記側面の法線方向に変位可能に設けられ、着陸状態において前記本体部を支持するフラップ部と、
前記フラップ部を変位させて前記気流の向きを変える制御を行う制御部と、を備える
飛行体。
And the body portion that having a peripheral portion and inner peripheral portion,
A lift generating portion provided inside the main body portion for generating at least an air flow from the upper side to the lower side of the main body portion.
Under end side of the body portion, displaceably mounted in a normal direction of the side, a flap portion supporting the main body portion in the landing state,
An air vehicle including a control unit that controls the displacement of the flap unit to change the direction of the air flow.
請求項1に記載の飛行体であって、
前記本体部の少なくとも上部又は下部には、全天球カメラが設けられている、
飛行体。
The flying object according to claim 1.
A spherical camera is provided at least above or below the main body.
Aircraft.
請求項2に記載の飛行体であって、
前記全天球カメラは、前記本体部の前記上部の中央又は略中央及び前記下部の中央又は略中央に設けられている、
飛行体。
The flying object according to claim 2.
The spherical camera is provided at the center or substantially the center of the upper part of the main body and at the center or substantially the center of the lower part.
Aircraft.
外周部及び内周部を有する円筒形状の本体部と、
前記本体部の内部に設けられる複数の反転プロペラと、
前記本体部の下部に変位可能に設けられたフラップ部と、
前記フラップ部を変位させて前記複数の反転プロペラにより発生した気流の向きを変える制御を行う制御部と、を備え、
前記本体部の前記外周部には、長手方向が周方向に沿うディスプレイ部が設けられる、
飛行体。
A cylindrical main body having an outer peripheral portion and an inner peripheral portion, and
A plurality of counter-rotating propellers provided inside the main body,
A flap portion displaceable at the bottom of the main body portion and
A control unit that controls the displacement of the flap unit to change the direction of the airflow generated by the plurality of counter-rotating propellers is provided.
A display portion whose longitudinal direction is along the circumferential direction is provided on the outer peripheral portion of the main body portion.
Aircraft.
請求項4に記載の飛行体であって、
前記ディスプレイ部は、前記外周部の略全面に設けられている有機ELディスプレイである、
飛行体。
The flying object according to claim 4.
The display unit is an organic EL display provided on substantially the entire surface of the outer peripheral portion.
Aircraft.
請求項4又は請求項5に記載の飛行体であって、
画像取得部を更に備えており、
前記制御部は、特定のジェスチャと特定の動作とを関連付けて管理しており、一のジェスチャに関する情報を前記ディスプレイ部に表示するとともに、前記画像取得部によって取得したユーザの行動が前記一のジェスチャと同一と判断した場合、前記特定の動作を行うように前記飛行体を制御する、
飛行体。
The flying object according to claim 4 or 5.
It also has an image acquisition unit,
The control unit manages a specific gesture in association with a specific operation, displays information about one gesture on the display unit, and the user's action acquired by the image acquisition unit is the one gesture. If it is determined to be the same as, the flying object is controlled so as to perform the specific operation.
Aircraft.
請求項1乃至請求項6のいずれかに記載の飛行体であって、
前記外周部には、一以上の深度センサが設けられている、
飛行体。
The flying object according to any one of claims 1 to 6.
One or more depth sensors are provided on the outer peripheral portion.
Aircraft.
請求項7に記載の飛行体であって、
前記深度センサは、前記外周上方から見た場合に120度間隔で設けられている、
飛行体。
The flying object according to claim 7.
The depth sensors are provided at intervals of 120 degrees when the outer peripheral portion is viewed from above.
Aircraft.
請求項1乃至請求項8のいずれかに記載の飛行体であって、
前記本体部の上面及び下面はメッシュ状に形成されている、
飛行体。
The flying object according to any one of claims 1 to 8.
The upper surface and the lower surface of the main body are formed in a mesh shape.
Aircraft.
JP2019204607A 2019-11-12 2019-11-12 Flying object Active JP7038421B2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP2019204607A JP7038421B2 (en) 2019-11-12 2019-11-12 Flying object
JP2022009036A JP7296153B2 (en) 2019-11-12 2022-01-25 flying object

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2019204607A JP7038421B2 (en) 2019-11-12 2019-11-12 Flying object

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
JP2018067403A Division JP6618564B2 (en) 2018-03-30 2018-03-30 Flying object

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2022009036A Division JP7296153B2 (en) 2019-11-12 2022-01-25 flying object

Publications (3)

Publication Number Publication Date
JP2020019481A JP2020019481A (en) 2020-02-06
JP2020019481A5 true JP2020019481A5 (en) 2021-05-13
JP7038421B2 JP7038421B2 (en) 2022-03-18

Family

ID=69588020

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2019204607A Active JP7038421B2 (en) 2019-11-12 2019-11-12 Flying object

Country Status (1)

Country Link
JP (1) JP7038421B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102462015B1 (en) * 2022-01-07 2022-11-03 조한석 Billboards using drones

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3054578A (en) * 1957-10-08 1962-09-18 Cie De Rech S Et D Etudes Aero Annular aircraft with elastic collector ring rim
JPH11115896A (en) * 1997-10-17 1999-04-27 Komatsu Ltd Unmanned and freely controlled flying body with low speed
US20040094662A1 (en) * 2002-01-07 2004-05-20 Sanders John K. Vertical tale-off landing hovercraft
AU2009243923B2 (en) * 2008-05-07 2015-04-30 Entecho Pty Ltd Fluid dynamic device with thrust control shroud
US20110147533A1 (en) * 2009-12-21 2011-06-23 Honeywell International Inc. Morphing ducted fan for vertical take-off and landing vehicle
US20130126680A1 (en) * 2011-11-17 2013-05-23 Honeywell International Inc. Unmanned air vehicle fault tolerant flight control system and method
JP2017163265A (en) * 2016-03-08 2017-09-14 株式会社リコー Controlling support system, information processing device, and program
JP6758119B2 (en) * 2016-08-24 2020-09-23 東京瓦斯株式会社 Unmanned aerial vehicle
CN106628162A (en) * 2016-12-21 2017-05-10 曹萍 Composite unmanned aerial vehicle

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