JP2020026270A5 - - Google Patents
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- JP2020026270A5 JP2020026270A5 JP2019187099A JP2019187099A JP2020026270A5 JP 2020026270 A5 JP2020026270 A5 JP 2020026270A5 JP 2019187099 A JP2019187099 A JP 2019187099A JP 2019187099 A JP2019187099 A JP 2019187099A JP 2020026270 A5 JP2020026270 A5 JP 2020026270A5
- Authority
- JP
- Japan
- Prior art keywords
- main body
- wing aircraft
- rotary wing
- unit
- axis
- 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.)
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- 230000001174 ascending Effects 0.000 claims 1
- 230000005484 gravity Effects 0.000 claims 1
Claims (5)
前記飛行部は、複数の回転翼と、前記複数の回転翼を支持するアーム部とを備えており、
前記本体部は、上下方向に延びる部材と、当該部材の上端側及び下端側に夫々設けられた第１搭載部及び第２搭載部とを備えており、
前記接続部は、進行方向と直交する水平軸周りに前記本体部を搖動可能にする第１接続部と、前記水平軸と直交し且つ垂直上昇時に水平よりも上向きに所定の仰角をなす斜交軸周りに前記本体部を搖動可能にする第２接続部とを有している、
回転翼機。 A rotary-wing aircraft including a flight unit, a main body unit, and a connection unit for oscillatingly connecting the flight unit and the main body unit within a predetermined range.
The flight unit includes a plurality of rotor blades and an arm unit that supports the plurality of rotor blades.
The main body portion includes a member extending in the vertical direction and a first mounting portion and a second mounting portion provided on the upper end side and the lower end side of the member, respectively.
The connection portion is an oblique intersection with a first connection portion that allows the main body portion to swing around a horizontal axis orthogonal to the traveling direction, and an oblique intersection that is orthogonal to the horizontal axis and forms a predetermined elevation angle upward from the horizontal when ascending vertically. It has a second connection part around the axis that allows the main body part to swing.
Rotorcraft.
前記水平軸と前記斜交軸との交点は、前記複数の回転翼が回転することによって機体に発生する揚力の略中心位置にあることを特徴とする
回転翼機。 The rotary wing aircraft according to claim 1.
A rotary wing machine characterized in that the intersection of the horizontal axis and the oblique axis is at a substantially central position of lift generated in the airframe due to the rotation of the plurality of rotary blades.
前記水平軸と前記斜交軸との交点は、前記本体部の重心にあることを特徴とする
回転翼機。 The rotary wing aircraft according to claim 1.
A rotary wing aircraft characterized in that the intersection of the horizontal axis and the oblique axis is at the center of gravity of the main body.
前記第１搭載部の位置は、前記本体部から後方にずれており、
前記第２搭載部の位置は、前記本体部から前方にずれている、
回転翼機。 The rotary wing aircraft according to any one of claims 1 to 3.
The position of the first mounting portion is displaced rearward from the main body portion.
The position of the second mounting portion is deviated forward from the main body portion.
Rotorcraft.
前記飛行部を進行方向に傾けるようにして進行方向に移動し
前記仰角は、少なくとも進行方向への飛行時に前記斜交軸が水平となり得る角度である、
回転翼機。
The rotary wing aircraft according to any one of claims 1 to 4.
The flight portion is moved in the traveling direction so as to be tilted in the traveling direction, and the elevation angle is an angle at which the oblique axis can be horizontal at least when flying in the traveling direction.
Rotorcraft.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2019187099A JP7120645B2 (en) | 2019-10-10 | 2019-10-10 | rotorcraft |
| JP2022120658A JP7240050B2 (en) | 2019-10-10 | 2022-07-28 | rotorcraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2019187099A JP7120645B2 (en) | 2019-10-10 | 2019-10-10 | rotorcraft |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2019541468A Division JP6607480B1 (en) | 2018-08-13 | 2018-08-13 | Rotorcraft |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2022120658A Division JP7240050B2 (en) | 2019-10-10 | 2022-07-28 | rotorcraft |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2020026270A JP2020026270A (en) | 2020-02-20 |
| JP2020026270A5 true JP2020026270A5 (en) | 2021-09-30 |
| JP7120645B2 JP7120645B2 (en) | 2022-08-17 |
Family
ID=69621847
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2019187099A Active JP7120645B2 (en) | 2019-10-10 | 2019-10-10 | rotorcraft |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP7120645B2 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113581455B (en) * | 2021-08-05 | 2023-08-01 | 广东智联航空科技有限公司 | Multi-rotor aircraft with constant center of gravity |
| AU2022343911A1 (en) * | 2021-09-13 | 2024-03-28 | Orthodrone Gmbh | Aircraft |
| KR20230120915A (en) * | 2022-02-10 | 2023-08-17 | 디스이즈엔지니어링 주식회사 | Air vehicle |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6261090B2 (en) * | 2015-05-18 | 2018-01-17 | 株式会社ａｍｕｓｅ ｏｎｅｓｅｌｆ | Unmanned aerial vehicle |
| SG11201709198WA (en) * | 2015-05-19 | 2017-12-28 | Aeronext Inc | Rotary-wing aircraft |
| JP2017193208A (en) * | 2016-04-18 | 2017-10-26 | 株式会社自律制御システム研究所 | Small-sized unmanned aircraft |
| US11325696B2 (en) * | 2016-10-03 | 2022-05-10 | Aeronext Inc. | Delivery rotary-wing aircraft |
-
2019
- 2019-10-10 JP JP2019187099A patent/JP7120645B2/en active Active
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