CN117545690A - 垂直起飞的飞行器 - Google Patents
垂直起飞的飞行器 Download PDFInfo
- Publication number
- CN117545690A CN117545690A CN202280043834.3A CN202280043834A CN117545690A CN 117545690 A CN117545690 A CN 117545690A CN 202280043834 A CN202280043834 A CN 202280043834A CN 117545690 A CN117545690 A CN 117545690A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- vertical
- drive unit
- wing
- flight
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/20—Vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/296—Rotors with variable spatial positions relative to the UAV body
- B64U30/297—Tilting rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transmission Devices (AREA)
- Retarders (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Liquid Crystal Substances (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102021110634.6A DE102021110634A1 (de) | 2021-04-26 | 2021-04-26 | Senkrecht startendes Fluggerät |
| DE102021110634.6 | 2021-04-26 | ||
| PCT/EP2022/061078 WO2022229201A1 (de) | 2021-04-26 | 2022-04-26 | Senkrecht startendes fluggerät |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN117545690A true CN117545690A (zh) | 2024-02-09 |
Family
ID=81850108
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202280043834.3A Pending CN117545690A (zh) | 2021-04-26 | 2022-04-26 | 垂直起飞的飞行器 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20240217651A1 (enExample) |
| EP (1) | EP4326614A1 (enExample) |
| JP (1) | JP2024516181A (enExample) |
| CN (1) | CN117545690A (enExample) |
| AU (1) | AU2022267733A1 (enExample) |
| DE (1) | DE102021110634A1 (enExample) |
| WO (1) | WO2022229201A1 (enExample) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD1009697S1 (en) * | 2021-04-26 | 2024-01-02 | Wingcopter GmbH | Drone |
| GB2623016B (en) * | 2021-06-20 | 2024-08-21 | Norouzi Ramin | Reconfiguring vertical takeoff and landing aircraft |
| CN118651409A (zh) * | 2023-03-03 | 2024-09-17 | 成都沃飞天驭科技有限公司 | 一种垂直起降飞行器和垂直起降飞行器的控制方法 |
| WO2024183569A1 (zh) * | 2023-03-03 | 2024-09-12 | 四川沃飞长空科技发展有限公司 | 一种垂直起降飞行器和垂直起降飞行器的控制方法 |
| JP2026508675A (ja) * | 2023-05-08 | 2026-03-11 | 四川沃飛長空科技発展有限公司 | 垂直離着陸機及び垂直離着陸機の制御方法 |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103072688A (zh) * | 2013-01-22 | 2013-05-01 | 西安交通大学 | 可倾转四旋翼飞行器 |
| CN106043696A (zh) * | 2016-06-30 | 2016-10-26 | 天津曙光天成科技有限公司 | 一种无人机飞行系统 |
| US20190329882A1 (en) * | 2018-04-27 | 2019-10-31 | Aai Corporation | Variable pitch rotor assembly for electrically driven vectored thrust aircraft applications |
| WO2020105045A1 (en) * | 2018-11-25 | 2020-05-28 | Israel Aerospace Industries Ltd. | Air vehicle and method of operation of air vehicle |
| CN111216883A (zh) * | 2018-11-26 | 2020-06-02 | 空客直升机德国有限公司 | 具有至少八个推力产生单元的垂直起飞和着陆的多旋翼飞行器 |
| US20200269975A1 (en) * | 2019-02-27 | 2020-08-27 | Airbus Helicopters Deutschland GmbH | Multirotor aircraft that is adapted for vertical take-off and landing |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102012106869A1 (de) | 2012-07-27 | 2014-01-30 | Jonathan Hesselbarth | Senkrecht startendes Flugzeug |
| WO2016110756A1 (en) * | 2015-03-29 | 2016-07-14 | Milani Kazem | Vtol aircraft with tiltable propellers |
| CN205998126U (zh) * | 2016-06-30 | 2017-03-08 | 天津曙光天成科技有限公司 | 一种无人机飞行系统 |
| US10189565B2 (en) * | 2016-12-02 | 2019-01-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Modular unmanned aerial system with multi-mode propulsion |
| US10618656B2 (en) * | 2017-10-04 | 2020-04-14 | Textron Innovations Inc. | Tiltrotor aircraft having interchangeable payload modules |
| EP3704018B1 (en) * | 2017-11-03 | 2022-05-04 | Uber Technologies, Inc. | Vtol m-wing configuration |
| WO2019217920A1 (en) * | 2018-05-10 | 2019-11-14 | Joby Aero, Inc. | Electric tiltrotor aircraft |
-
2021
- 2021-04-26 DE DE102021110634.6A patent/DE102021110634A1/de active Pending
-
2022
- 2022-04-26 EP EP22725806.8A patent/EP4326614A1/de active Pending
- 2022-04-26 US US18/557,124 patent/US20240217651A1/en active Pending
- 2022-04-26 JP JP2023565224A patent/JP2024516181A/ja active Pending
- 2022-04-26 WO PCT/EP2022/061078 patent/WO2022229201A1/de not_active Ceased
- 2022-04-26 AU AU2022267733A patent/AU2022267733A1/en active Pending
- 2022-04-26 CN CN202280043834.3A patent/CN117545690A/zh active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103072688A (zh) * | 2013-01-22 | 2013-05-01 | 西安交通大学 | 可倾转四旋翼飞行器 |
| CN106043696A (zh) * | 2016-06-30 | 2016-10-26 | 天津曙光天成科技有限公司 | 一种无人机飞行系统 |
| US20190329882A1 (en) * | 2018-04-27 | 2019-10-31 | Aai Corporation | Variable pitch rotor assembly for electrically driven vectored thrust aircraft applications |
| WO2020105045A1 (en) * | 2018-11-25 | 2020-05-28 | Israel Aerospace Industries Ltd. | Air vehicle and method of operation of air vehicle |
| CN111216883A (zh) * | 2018-11-26 | 2020-06-02 | 空客直升机德国有限公司 | 具有至少八个推力产生单元的垂直起飞和着陆的多旋翼飞行器 |
| US20200269975A1 (en) * | 2019-02-27 | 2020-08-27 | Airbus Helicopters Deutschland GmbH | Multirotor aircraft that is adapted for vertical take-off and landing |
Also Published As
| Publication number | Publication date |
|---|---|
| DE102021110634A1 (de) | 2022-10-27 |
| EP4326614A1 (de) | 2024-02-28 |
| US20240217651A1 (en) | 2024-07-04 |
| WO2022229201A1 (de) | 2022-11-03 |
| AU2022267733A1 (en) | 2023-11-23 |
| JP2024516181A (ja) | 2024-04-12 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |