JP6831756B2 - 飛行機械、輸送システム、および、輸送システムの運用方法 - Google Patents
飛行機械、輸送システム、および、輸送システムの運用方法 Download PDFInfo
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- JP6831756B2 JP6831756B2 JP2017119721A JP2017119721A JP6831756B2 JP 6831756 B2 JP6831756 B2 JP 6831756B2 JP 2017119721 A JP2017119721 A JP 2017119721A JP 2017119721 A JP2017119721 A JP 2017119721A JP 6831756 B2 JP6831756 B2 JP 6831756B2
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- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
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Description
メンテナンスのコストを抑えることができる。ただし、当然ながら、キャビンにエンジンやプロペラ等の推進装置や、最終的なキャビンを中心とした機体を制御するための動翼を供え、空中で翼のみを結合させるという構成も可能であり、運用の仕方によっては、この構成が望ましい場合もあると考えられる。
Claims (4)
- 任意の出発地点から目的地点へ、人あるいは荷物を空中輸送する飛行機械であって、
人あるいは荷物を積載するキャビンを備え、
前記キャビンは、
固定翼を分離可能に結合する固定翼結合機構と、
前記キャビンに重力に水平方向成分を持つ推力を与えるとともに前記固定翼により揚力を発生させる推進ユニットを、分離可能に結合する推進ユニット結合機構と、
前記キャビンに重力に垂直方向成分を持つ推力を与え前記固定翼による揚力がなくても前記キャビンを浮上させる浮上ユニットを、分離可能に結合する浮上ユニット結合機構と、
を備え、
前記固定翼は、自己を空中搬送するための第2の飛行機械を分離可能に結合する搬送用結合機構を備える飛行機械。 - 前記固定翼結合機構、前記推進ユニット結合機構、および、前記浮上ユニット結合機構は、飛行機械が空中にある状態で、結合および分離の少なくとも一つが可能である、
請求項1記載の飛行機械。 - 前記固定翼に前記推進ユニットが結合されており、
前記固定翼結合機構が前記推進ユニット結合機構を兼ねる、
請求項1記載の飛行機械。 - 前記固定翼、前記推進ユニット、および、前記浮上ユニットの少なくとも一つは、前記キャビンとは独立して飛行可能な構成である、
請求項1記載の飛行機械。
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JP2017119721A JP6831756B2 (ja) | 2017-06-19 | 2017-06-19 | 飛行機械、輸送システム、および、輸送システムの運用方法 |
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JP2017119721A JP6831756B2 (ja) | 2017-06-19 | 2017-06-19 | 飛行機械、輸送システム、および、輸送システムの運用方法 |
Publications (2)
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JP2019001397A JP2019001397A (ja) | 2019-01-10 |
JP6831756B2 true JP6831756B2 (ja) | 2021-02-17 |
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JP2017119721A Active JP6831756B2 (ja) | 2017-06-19 | 2017-06-19 | 飛行機械、輸送システム、および、輸送システムの運用方法 |
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JP (1) | JP6831756B2 (ja) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
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JP2022119258A (ja) * | 2021-02-04 | 2022-08-17 | Hapsモバイル株式会社 | データ処理装置、プログラム、及びデータ処理方法 |
CN113821912B (zh) * | 2021-08-25 | 2023-06-02 | 北京航空航天大学 | 一种固定翼飞机油耗模型的建模方法 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3298633A (en) * | 1965-09-10 | 1967-01-17 | Dastoli Joseph | Separable aircraft |
JPH092395A (ja) * | 1995-06-15 | 1997-01-07 | Kazuhiro Takahashi | 垂直離着陸機 |
US8950698B1 (en) * | 2012-10-26 | 2015-02-10 | The Boeing Company | Convertible compounded rotorcraft |
DE102013000409A1 (de) * | 2013-01-11 | 2014-07-17 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Flugplattform |
CN103935509B (zh) * | 2014-04-15 | 2016-06-29 | 西安交通大学 | 一种倾转四旋翼飞行器协调吊装运输装置 |
KR101614620B1 (ko) * | 2014-12-05 | 2016-04-22 | 서울대학교산학협력단 | 기계 작업이 가능한 멀티 로터 기반의 무인 비행로봇 시스템 |
US10133272B2 (en) * | 2015-05-07 | 2018-11-20 | The Boeing Company | Methods and apparatus to deploy and recover a fixed wing unmanned aerial vehicle via a non-fixed wing aircraft |
US9630712B1 (en) * | 2015-09-23 | 2017-04-25 | Amazon Technologies, Inc. | Using multirotor lifters to deploy fixed wing aircraft |
US20170144761A1 (en) * | 2015-11-19 | 2017-05-25 | A.L.D. Advanced Logistics Development Ltd. | Detachable Pilotable Capsules and Aircrafts Including Detachable Pilotable Capsules |
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